Started by upstream project "<a href='/csi/job/ESP_bPreBuilt/' class='jenkins-table__link model-link model-link--float'>ESP_bPreBuilt</a>" build number <a href='/csi/job/ESP_bPreBuilt/74' class='jenkins-table__link model-link model-link--float'>74</a>
originally caused by:
 Started by user <a href='/csi/user/galbramc' class='jenkins-table__link model-link model-link--float'>galbramc</a>
Running as <a href='/csi/user/galbramc' class='jenkins-table__link model-link model-link--float'>galbramc</a>
[EnvInject] - Loading node environment variables.
Building remotely on <a href='/csi/computer/macys' class='jenkins-table__link model-link model-link--float'>macys</a> in workspace /Users/jenkins/workspace/ESP_bPreBuilt
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
Checking out a fresh workspace because there's no workspace at /Users/jenkins/workspace/ESP_bPreBuilt
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-05-31T14:59:58.700 -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 2501

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 '2024-05-31T14:59:58.700 -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 863

No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
No changes for svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP since the previous build
[GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [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/jenkins16921690584623887724.sh
+ bash -ex /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/ESP_PreBuilt.sh
+ source /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ OCCTREF=7.8
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.38.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export 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
++ [[ 7.8 != '' ]]
++ [[ '' != '' ]]
++ [[ macys == *\r\e\y\n\o\l\d\s* ]]
++ [[ macys == *\m\a\c\y\s* ]]
++ export EMPnumProc=2
++ EMPnumProc=2
++ export OMP_NUM_THREADS=2
++ OMP_NUM_THREADS=2
++ source /Users/jenkins/.bash_profile
+++ export PATH=/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ export PATH=/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ export pwid_LICENSE=5053@acdl.mit.edu
+++ pwid_LICENSE=5053@acdl.mit.edu
++ [[ macys == *\m\a\c\y\s* ]]
++ export PATH=/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys == \m\a\c\y\s ]]
++ echo 'data/fighter4.csm;          ERROR:: build not completed because error -214 (did_not_create_body) was detected'
++ echo 'data/fighter4.csm;          ERROR:: build not completed because error -214 (did_not_create_body) was detected'
++ echo 'data/fighter4.csm;          ERROR:: build not completed because error -214 (did_not_create_body) was detected'
++ export CASARCH=.
++ CASARCH=.
++ '[' '!' -z '' ']'
+++ ls -d '/Users/jenkins/util/ESP/OpenCASCADE-.?'
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-3.38.0-MacOS
++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys == \m\a\c\y\s ]]
++ export SEACAS=/Users/jenkins/util/sandialabs/seacas
++ SEACAS=/Users/jenkins/util/sandialabs/seacas
++ [[ macys == \v\i\g\g\e\n ]]
++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']'
+++ perl -I/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 -Mlocal::lib=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
++ eval 'PATH="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin${PATH:+:${PATH}}"; export PATH;
PERL5LIB="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5${PERL5LIB:+:${PERL5LIB}}"; export PERL5LIB;
PERL_LOCAL_LIB_ROOT="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl${PERL_LOCAL_LIB_ROOT:+:${PERL_LOCAL_LIB_ROOT}}"; export PERL_LOCAL_LIB_ROOT;
PERL_MB_OPT="--install_base \"/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl\""; export PERL_MB_OPT;
PERL_MM_OPT="INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"; export PERL_MM_OPT;'
+++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
+++ export PATH
+++ PERL5LIB=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5
+++ export PERL5LIB
+++ PERL_LOCAL_LIB_ROOT=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
+++ export PERL_LOCAL_LIB_ROOT
+++ PERL_MB_OPT='--install_base "/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"'
+++ export PERL_MB_OPT
+++ PERL_MM_OPT=INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
+++ export PERL_MM_OPT
++ export PATH=/Users/jenkins/workspace/ESP_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 <a href='https://acdl.mit.edu/ESP/archive/ESP125-macos-x86_64.tgz'>https://acdl.mit.edu/ESP/archive/ESP125-macos-x86_64.tgz</a>
--2024-05-31 15:00:08--  <a href='https://acdl.mit.edu/ESP/archive/ESP125-macos-x86_64.tgz'>https://acdl.mit.edu/ESP/archive/ESP125-macos-x86_64.tgz</a>
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: 520633019 (497M) [application/x-gzip]
Saving to: ‘ESP125-macos-x86_64.tgz’

     0K .......... .......... .......... .......... ..........  0% 11.3M 44s
    50K .......... .......... .......... .......... ..........  0% 23.8M 32s
   100K .......... .......... .......... .......... ..........  0% 20.6M 30s
   150K .......... .......... .......... .......... ..........  0% 19.6M 29s
   200K .......... .......... .......... .......... ..........  0% 15.3M 29s
   250K .......... .......... .......... .......... ..........  0% 14.0M 30s
   300K .......... .......... .......... .......... ..........  0% 12.9M 32s
   350K .......... .......... .......... .......... ..........  0% 9.19M 34s
   400K .......... .......... .......... .......... ..........  0% 10.8M 36s
   450K .......... .......... .......... .......... ..........  0% 11.4M 36s
   500K .......... .......... .......... .......... ..........  0% 10.3M 37s
   550K .......... .......... .......... .......... ..........  0% 11.3M 38s
   600K .......... .......... .......... .......... ..........  0% 7.22M 40s
   650K .......... .......... .......... .......... ..........  0% 9.30M 41s
   700K .......... .......... .......... .......... ..........  0% 9.85M 42s
   750K .......... .......... .......... .......... ..........  0% 9.51M 43s
   800K .......... .......... .......... .......... ..........  0% 8.38M 44s
   850K .......... .......... .......... .......... ..........  0% 7.50M 45s
   900K .......... .......... .......... .......... ..........  0% 11.2M 45s
   950K .......... .......... .......... .......... ..........  0% 21.5M 44s
  1000K .......... .......... .......... .......... ..........  0% 22.8M 43s
  1050K .......... .......... .......... .......... ..........  0% 43.2M 41s
  1100K .......... .......... .......... .......... ..........  0% 23.6M 40s
  1150K .......... .......... .......... .......... ..........  0% 32.7M 39s
  1200K .......... .......... .......... .......... ..........  0% 18.4M 39s
  1250K .......... .......... .......... .......... ..........  0% 15.8M 38s
  1300K .......... .......... .......... .......... ..........  0% 10.7M 39s
  1350K .......... .......... .......... .......... ..........  0% 14.1M 39s
  1400K .......... .......... .......... .......... ..........  0% 11.0M 39s
  1450K .......... .......... .......... .......... ..........  0% 8.99M 39s
  1500K .......... .......... .......... .......... ..........  0% 11.5M 39s
  1550K .......... .......... .......... .......... ..........  0% 9.05M 40s
  1600K .......... .......... .......... .......... ..........  0% 6.41M 41s
  1650K .......... .......... .......... .......... ..........  0% 8.37M 42s
  1700K .......... .......... .......... .......... ..........  0% 6.78M 43s
  1750K .......... .......... .......... .......... ..........  0% 13.7M 42s
  1800K .......... .......... .......... .......... ..........  0% 13.2M 42s
  1850K .......... .......... .......... .......... ..........  0% 8.16M 43s
  1900K .......... .......... .......... .......... ..........  0% 10.9M 43s
  1950K .......... .......... .......... .......... ..........  0% 9.42M 43s
  2000K .......... .......... .......... .......... ..........  0% 11.0M 43s
  2050K .......... .......... .......... .......... ..........  0% 11.0M 43s
  2100K .......... .......... .......... .......... ..........  0% 7.56M 44s
  2150K .......... .......... .......... .......... ..........  0% 9.09M 44s
  2200K .......... .......... .......... .......... ..........  0% 8.08M 44s
  2250K .......... .......... .......... .......... ..........  0% 8.99M 44s
  2300K .......... .......... .......... .......... ..........  0% 9.84M 45s
  2350K .......... .......... .......... .......... ..........  0% 8.79M 45s
  2400K .......... .......... .......... .......... ..........  0% 8.66M 45s
  2450K .......... .......... .......... .......... ..........  0% 12.6M 45s
  2500K .......... .......... .......... .......... ..........  0% 22.8M 44s
  2550K .......... .......... .......... .......... ..........  0% 20.4M 44s
  2600K .......... .......... .......... .......... ..........  0% 17.1M 44s
  2650K .......... .......... .......... .......... ..........  0% 12.1M 44s
  2700K .......... .......... .......... .......... ..........  0% 9.52M 44s
  2750K .......... .......... .......... .......... ..........  0% 14.0M 44s
  2800K .......... .......... .......... .......... ..........  0% 8.42M 44s
  2850K .......... .......... .......... .......... ..........  0% 7.73M 44s
  2900K .......... .......... .......... .......... ..........  0% 10.9M 44s
  2950K .......... .......... .......... .......... ..........  0% 7.60M 45s
  3000K .......... .......... .......... .......... ..........  0% 8.72M 45s
  3050K .......... .......... .......... .......... ..........  0% 8.61M 45s
  3100K .......... .......... .......... .......... ..........  0% 6.39M 46s
  3150K .......... .......... .......... .......... ..........  0% 10.9M 46s
  3200K .......... .......... .......... .......... ..........  0% 7.77M 46s
  3250K .......... .......... .......... .......... ..........  0% 8.98M 46s
  3300K .......... .......... .......... .......... ..........  0% 6.13M 46s
  3350K .......... .......... .......... .......... ..........  0% 7.70M 47s
  3400K .......... .......... .......... .......... ..........  0% 8.37M 47s
  3450K .......... .......... .......... .......... ..........  0% 8.10M 47s
  3500K .......... .......... .......... .......... ..........  0% 8.37M 47s
  3550K .......... .......... .......... .......... ..........  0% 5.76M 48s
  3600K .......... .......... .......... .......... ..........  0% 5.26M 48s
  3650K .......... .......... .......... .......... ..........  0% 5.93M 49s
  3700K .......... .......... .......... .......... ..........  0% 5.53M 49s
  3750K .......... .......... .......... .......... ..........  0% 6.04M 50s
  3800K .......... .......... .......... .......... ..........  0% 6.01M 50s
  3850K .......... .......... .......... .......... ..........  0% 11.7M 50s
  3900K .......... .......... .......... .......... ..........  0% 13.2M 50s
  3950K .......... .......... .......... .......... ..........  0% 11.4M 50s
  4000K .......... .......... .......... .......... ..........  0% 17.0M 50s
  4050K .......... .......... .......... .......... ..........  0% 14.0M 49s
  4100K .......... .......... .......... .......... ..........  0% 14.9M 49s
  4150K .......... .......... .......... .......... ..........  0% 12.8M 49s
  4200K .......... .......... .......... .......... ..........  0% 11.4M 49s
  4250K .......... .......... .......... .......... ..........  0% 15.4M 49s
  4300K .......... .......... .......... .......... ..........  0% 12.0M 49s
  4350K .......... .......... .......... .......... ..........  0% 15.7M 48s
  4400K .......... .......... .......... .......... ..........  0% 24.1M 48s
  4450K .......... .......... .......... .......... ..........  0% 42.1M 48s
  4500K .......... .......... .......... .......... ..........  0% 71.1M 47s
  4550K .......... .......... .......... .......... ..........  0% 26.7M 47s
  4600K .......... .......... .......... .......... ..........  0% 38.9M 47s
  4650K .......... .......... .......... .......... ..........  0%  104M 46s
  4700K .......... .......... .......... .......... ..........  0% 23.7M 46s
  4750K .......... .......... .......... .......... ..........  0% 27.5M 46s
  4800K .......... .......... .......... .......... ..........  0% 11.3M 46s
  4850K .......... .......... .......... .......... ..........  0% 9.62M 46s
  4900K .......... .......... .......... .......... ..........  0% 11.5M 46s
  4950K .......... .......... .......... .......... ..........  0% 9.61M 46s
  5000K .......... .......... .......... .......... ..........  0% 13.6M 46s
  5050K .......... .......... .......... .......... ..........  1% 9.67M 46s
  5100K .......... .......... .......... .......... ..........  1% 10.2M 46s
  5150K .......... .......... .......... .......... ..........  1% 7.36M 46s
  5200K .......... .......... .......... .......... ..........  1% 8.34M 46s
  5250K .......... .......... .......... .......... ..........  1% 7.65M 46s
  5300K .......... .......... .......... .......... ..........  1% 9.31M 46s
  5350K .......... .......... .......... .......... ..........  1% 8.74M 46s
  5400K .......... .......... .......... .......... ..........  1% 8.97M 46s
  5450K .......... .......... .......... .......... ..........  1% 6.51M 47s
  5500K .......... .......... .......... .......... ..........  1% 7.14M 47s
  5550K .......... .......... .......... .......... ..........  1% 5.90M 47s
  5600K .......... .......... .......... .......... ..........  1% 5.60M 47s
  5650K .......... .......... .......... .......... ..........  1% 6.26M 48s
  5700K .......... .......... .......... .......... ..........  1% 5.92M 48s
  5750K .......... .......... .......... .......... ..........  1% 7.50M 48s
  5800K .......... .......... .......... .......... ..........  1% 10.6M 48s
  5850K .......... .......... .......... .......... ..........  1% 8.13M 48s
  5900K .......... .......... .......... .......... ..........  1% 9.70M 48s
  5950K .......... .......... .......... .......... ..........  1% 8.23M 48s
  6000K .......... .......... .......... .......... ..........  1% 5.94M 49s
  6050K .......... .......... .......... .......... ..........  1% 6.61M 49s
  6100K .......... .......... .......... .......... ..........  1% 5.05M 49s
  6150K .......... .......... .......... .......... ..........  1% 5.59M 50s
  6200K .......... .......... .......... .......... ..........  1% 3.69M 50s
  6250K .......... .......... .......... .......... ..........  1% 3.45M 51s
  6300K .......... .......... .......... .......... ..........  1% 4.62M 51s
  6350K .......... .......... .......... .......... ..........  1% 18.7M 51s
  6400K .......... .......... .......... .......... ..........  1% 20.8M 51s
  6450K .......... .......... .......... .......... ..........  1% 32.9M 51s
  6500K .......... .......... .......... .......... ..........  1% 23.9M 50s
  6550K .......... .......... .......... .......... ..........  1% 37.5M 50s
  6600K .......... .......... .......... .......... ..........  1% 18.4M 50s
  6650K .......... .......... .......... .......... ..........  1% 19.3M 50s
  6700K .......... .......... .......... .......... ..........  1% 12.0M 50s
  6750K .......... .......... .......... .......... ..........  1% 13.2M 50s
  6800K .......... .......... .......... .......... ..........  1% 11.2M 50s
  6850K .......... .......... .......... .......... ..........  1% 11.9M 49s
  6900K .......... .......... .......... .......... ..........  1% 11.8M 49s
  6950K .......... .......... .......... .......... ..........  1% 11.4M 49s
  7000K .......... .......... .......... .......... ..........  1% 12.2M 49s
  7050K .......... .......... .......... .......... ..........  1% 11.7M 49s
  7100K .......... .......... .......... .......... ..........  1% 9.92M 49s
  7150K .......... .......... .......... .......... ..........  1% 8.53M 49s
  7200K .......... .......... .......... .......... ..........  1% 8.21M 49s
  7250K .......... .......... .......... .......... ..........  1% 8.33M 49s
  7300K .......... .......... .......... .......... ..........  1% 8.07M 49s
  7350K .......... .......... .......... .......... ..........  1% 4.63M 50s
  7400K .......... .......... .......... .......... ..........  1% 6.89M 50s
  7450K .......... .......... .......... .......... ..........  1% 5.42M 50s
  7500K .......... .......... .......... .......... ..........  1% 6.62M 50s
  7550K .......... .......... .......... .......... ..........  1% 6.44M 51s
  7600K .......... .......... .......... .......... ..........  1% 5.96M 51s
  7650K .......... .......... .......... .......... ..........  1% 5.96M 51s
  7700K .......... .......... .......... .......... ..........  1% 4.94M 51s
  7750K .......... .......... .......... .......... ..........  1% 5.90M 51s
  7800K .......... .......... .......... .......... ..........  1% 5.73M 52s
  7850K .......... .......... .......... .......... ..........  1% 6.52M 52s
  7900K .......... .......... .......... .......... ..........  1% 18.5M 52s
  7950K .......... .......... .......... .......... ..........  1% 15.4M 52s
  8000K .......... .......... .......... .......... ..........  1% 12.7M 51s
  8050K .......... .......... .......... .......... ..........  1% 16.5M 51s
  8100K .......... .......... .......... .......... ..........  1% 15.6M 51s
  8150K .......... .......... .......... .......... ..........  1% 13.9M 51s
  8200K .......... .......... .......... .......... ..........  1% 14.8M 51s
  8250K .......... .......... .......... .......... ..........  1% 21.0M 51s
  8300K .......... .......... .......... .......... ..........  1% 17.1M 51s
  8350K .......... .......... .......... .......... ..........  1% 14.1M 51s
  8400K .......... .......... .......... .......... ..........  1% 23.5M 50s
  8450K .......... .......... .......... .......... ..........  1% 15.1M 50s
  8500K .......... .......... .......... .......... ..........  1% 16.7M 50s
  8550K .......... .......... .......... .......... ..........  1% 18.6M 50s
  8600K .......... .......... .......... .......... ..........  1% 25.1M 50s
  8650K .......... .......... .......... .......... ..........  1% 75.4M 50s
  8700K .......... .......... .......... .......... ..........  1% 24.4M 49s
  8750K .......... .......... .......... .......... ..........  1%  129M 49s
  8800K .......... .......... .......... .......... ..........  1% 27.3M 49s
  8850K .......... .......... .......... .......... ..........  1% 65.1M 49s
  8900K .......... .......... .......... .......... ..........  1% 23.6M 49s
  8950K .......... .......... .......... .......... ..........  1% 20.9M 48s
  9000K .......... .......... .......... .......... ..........  1% 37.4M 48s
  9050K .......... .......... .......... .......... ..........  1% 24.5M 48s
  9100K .......... .......... .......... .......... ..........  1% 21.2M 48s
  9150K .......... .......... .......... .......... ..........  1% 29.9M 48s
  9200K .......... .......... .......... .......... ..........  1% 26.0M 48s
  9250K .......... .......... .......... .......... ..........  1% 22.2M 47s
  9300K .......... .......... .......... .......... ..........  1% 27.8M 47s
  9350K .......... .......... .......... .......... ..........  1% 18.4M 47s
  9400K .......... .......... .......... .......... ..........  1% 19.1M 47s
  9450K .......... .......... .......... .......... ..........  1% 21.6M 47s
  9500K .......... .......... .......... .......... ..........  1% 23.1M 47s
  9550K .......... .......... .......... .......... ..........  1% 24.0M 47s
  9600K .......... .......... .......... .......... ..........  1% 22.5M 46s
  9650K .......... .......... .......... .......... ..........  1% 21.7M 46s
  9700K .......... .......... .......... .......... ..........  1% 19.2M 46s
  9750K .......... .......... .......... .......... ..........  1% 16.5M 46s
  9800K .......... .......... .......... .......... ..........  1% 21.2M 46s
  9850K .......... .......... .......... .......... ..........  1% 15.5M 46s
  9900K .......... .......... .......... .......... ..........  1% 15.8M 46s
  9950K .......... .......... .......... .......... ..........  1% 16.8M 46s
 10000K .......... .......... .......... .......... ..........  1% 18.5M 46s
 10050K .......... .......... .......... .......... ..........  1% 22.3M 46s
 10100K .......... .......... .......... .......... ..........  1% 13.8M 45s
 10150K .......... .......... .......... .......... ..........  2% 13.1M 45s
 10200K .......... .......... .......... .......... ..........  2% 14.5M 45s
 10250K .......... .......... .......... .......... ..........  2% 15.1M 45s
 10300K .......... .......... .......... .......... ..........  2% 18.3M 45s
 10350K .......... .......... .......... .......... ..........  2% 36.6M 45s
 10400K .......... .......... .......... .......... ..........  2% 43.6M 45s
 10450K .......... .......... .......... .......... ..........  2% 22.0M 45s
 10500K .......... .......... .......... .......... ..........  2%  172M 45s
 10550K .......... .......... .......... .......... ..........  2% 40.4M 44s
 10600K .......... .......... .......... .......... ..........  2% 45.3M 44s
 10650K .......... .......... .......... .......... ..........  2% 42.0M 44s
 10700K .......... .......... .......... .......... ..........  2% 18.9M 44s
 10750K .......... .......... .......... .......... ..........  2% 38.1M 44s
 10800K .......... .......... .......... .......... ..........  2% 25.5M 44s
 10850K .......... .......... .......... .......... ..........  2% 22.8M 44s
 10900K .......... .......... .......... .......... ..........  2% 23.4M 44s
 10950K .......... .......... .......... .......... ..........  2% 22.8M 43s
 11000K .......... .......... .......... .......... ..........  2% 24.6M 43s
 11050K .......... .......... .......... .......... ..........  2% 27.6M 43s
 11100K .......... .......... .......... .......... ..........  2% 20.6M 43s
 11150K .......... .......... .......... .......... ..........  2% 30.3M 43s
 11200K .......... .......... .......... .......... ..........  2% 19.6M 43s
 11250K .......... .......... .......... .......... ..........  2% 26.9M 43s
 11300K .......... .......... .......... .......... ..........  2% 26.5M 43s
 11350K .......... .......... .......... .......... ..........  2% 18.2M 43s
 11400K .......... .......... .......... .......... ..........  2% 39.5M 42s
 11450K .......... .......... .......... .......... ..........  2% 19.5M 42s
 11500K .......... .......... .......... .......... ..........  2% 26.4M 42s
 11550K .......... .......... .......... .......... ..........  2% 25.7M 42s
 11600K .......... .......... .......... .......... ..........  2% 12.8M 42s
 11650K .......... .......... .......... .......... ..........  2% 13.7M 42s
 11700K .......... .......... .......... .......... ..........  2% 76.1M 42s
 11750K .......... .......... .......... .......... ..........  2% 18.2M 42s
 11800K .......... .......... .......... .......... ..........  2% 21.9M 42s
 11850K .......... .......... .......... .......... ..........  2% 10.3M 42s
 11900K .......... .......... .......... .......... ..........  2% 19.5M 42s
 11950K .......... .......... .......... .......... ..........  2% 20.2M 42s
 12000K .......... .......... .......... .......... ..........  2% 15.1M 42s
 12050K .......... .......... .......... .......... ..........  2% 14.6M 42s
 12100K .......... .......... .......... .......... ..........  2% 19.9M 41s
 12150K .......... .......... .......... .......... ..........  2% 16.5M 41s
 12200K .......... .......... .......... .......... ..........  2% 19.8M 41s
 12250K .......... .......... .......... .......... ..........  2% 12.3M 41s
 12300K .......... .......... .......... .......... ..........  2% 22.7M 41s
 12350K .......... .......... .......... .......... ..........  2% 12.5M 41s
 12400K .......... .......... .......... .......... ..........  2% 13.7M 41s
 12450K .......... .......... .......... .......... ..........  2% 13.0M 41s
 12500K .......... .......... .......... .......... ..........  2% 17.5M 41s
 12550K .......... .......... .......... .......... ..........  2% 15.4M 41s
 12600K .......... .......... .......... .......... ..........  2% 10.0M 41s
 12650K .......... .......... .......... .......... ..........  2% 13.4M 41s
 12700K .......... .......... .......... .......... ..........  2% 12.1M 41s
 12750K .......... .......... .......... .......... ..........  2% 12.4M 41s
 12800K .......... .......... .......... .......... ..........  2% 12.0M 41s
 12850K .......... .......... .......... .......... ..........  2% 14.5M 41s
 12900K .......... .......... .......... .......... ..........  2% 12.0M 41s
 12950K .......... .......... .......... .......... ..........  2% 10.7M 41s
 13000K .......... .......... .......... .......... ..........  2% 14.8M 41s
 13050K .......... .......... .......... .......... ..........  2% 13.3M 41s
 13100K .......... .......... .......... .......... ..........  2% 11.3M 41s
 13150K .......... .......... .......... .......... ..........  2% 13.4M 41s
 13200K .......... .......... .......... .......... ..........  2% 10.9M 41s
 13250K .......... .......... .......... .......... ..........  2% 12.8M 41s
 13300K .......... .......... .......... .......... ..........  2% 28.4M 41s
 13350K .......... .......... .......... .......... ..........  2% 14.6M 41s
 13400K .......... .......... .......... .......... ..........  2% 15.8M 41s
 13450K .......... .......... .......... .......... ..........  2% 12.4M 41s
 13500K .......... .......... .......... .......... ..........  2% 20.7M 41s
 13550K .......... .......... .......... .......... ..........  2% 15.0M 41s
 13600K .......... .......... .......... .......... ..........  2% 9.92M 41s
 13650K .......... .......... .......... .......... ..........  2% 14.2M 41s
 13700K .......... .......... .......... .......... ..........  2% 11.6M 41s
 13750K .......... .......... .......... .......... ..........  2% 13.7M 41s
 13800K .......... .......... .......... .......... ..........  2% 13.9M 41s
 13850K .......... .......... .......... .......... ..........  2% 11.3M 41s
 13900K .......... .......... .......... .......... ..........  2% 10.0M 41s
 13950K .......... .......... .......... .......... ..........  2% 12.7M 41s
 14000K .......... .......... .......... .......... ..........  2% 16.1M 41s
 14050K .......... .......... .......... .......... ..........  2% 13.2M 41s
 14100K .......... .......... .......... .......... ..........  2% 11.7M 41s
 14150K .......... .......... .......... .......... ..........  2% 12.8M 41s
 14200K .......... .......... .......... .......... ..........  2% 10.4M 41s
 14250K .......... .......... .......... .......... ..........  2% 11.9M 41s
 14300K .......... .......... .......... .......... ..........  2% 4.28M 41s
 14350K .......... .......... .......... .......... ..........  2%  156M 41s
 14400K .......... .......... .......... .......... ..........  2% 14.7M 41s
 14450K .......... .......... .......... .......... ..........  2% 8.18M 41s
 14500K .......... .......... .......... .......... ..........  2% 8.90M 41s
 14550K .......... .......... .......... .......... ..........  2% 7.41M 41s
 14600K .......... .......... .......... .......... ..........  2% 6.03M 41s
 14650K .......... .......... .......... .......... ..........  2% 9.27M 41s
 14700K .......... .......... .......... .......... ..........  2% 6.31M 41s
 14750K .......... .......... .......... .......... ..........  2% 6.85M 41s
 14800K .......... .......... .......... .......... ..........  2% 8.35M 41s
 14850K .......... .......... .......... .......... ..........  2% 6.76M 41s
 14900K .......... .......... .......... .......... ..........  2% 7.66M 41s
 14950K .......... .......... .......... .......... ..........  2% 8.57M 41s
 15000K .......... .......... .......... .......... ..........  2% 12.6M 41s
 15050K .......... .......... .......... .......... ..........  2% 12.7M 41s
 15100K .......... .......... .......... .......... ..........  2% 9.45M 41s
 15150K .......... .......... .......... .......... ..........  2% 12.3M 41s
 15200K .......... .......... .......... .......... ..........  2% 9.85M 41s
 15250K .......... .......... .......... .......... ..........  3% 12.1M 41s
 15300K .......... .......... .......... .......... ..........  3% 11.3M 41s
 15350K .......... .......... .......... .......... ..........  3% 10.6M 41s
 15400K .......... .......... .......... .......... ..........  3% 18.4M 41s
 15450K .......... .......... .......... .......... ..........  3% 7.80M 41s
 15500K .......... .......... .......... .......... ..........  3% 22.4M 41s
 15550K .......... .......... .......... .......... ..........  3% 8.88M 41s
 15600K .......... .......... .......... .......... ..........  3% 9.22M 41s
 15650K .......... .......... .......... .......... ..........  3% 8.20M 42s
 15700K .......... .......... .......... .......... ..........  3% 6.96M 42s
 15750K .......... .......... .......... .......... ..........  3% 7.10M 42s
 15800K .......... .......... .......... .......... ..........  3% 8.67M 42s
 15850K .......... .......... .......... .......... ..........  3% 7.01M 42s
 15900K .......... .......... .......... .......... ..........  3% 7.46M 42s
 15950K .......... .......... .......... .......... ..........  3% 5.89M 42s
 16000K .......... .......... .......... .......... ..........  3% 6.59M 42s
 16050K .......... .......... .......... .......... ..........  3% 7.77M 42s
 16100K .......... .......... .......... .......... ..........  3% 5.44M 42s
 16150K .......... .......... .......... .......... ..........  3% 8.90M 42s
 16200K .......... .......... .......... .......... ..........  3% 8.39M 42s
 16250K .......... .......... .......... .......... ..........  3% 8.51M 42s
 16300K .......... .......... .......... .......... ..........  3% 8.49M 42s
 16350K .......... .......... .......... .......... ..........  3% 8.86M 42s
 16400K .......... .......... .......... .......... ..........  3% 9.13M 42s
 16450K .......... .......... .......... .......... ..........  3% 7.85M 43s
 16500K .......... .......... .......... .......... ..........  3% 12.0M 43s
 16550K .......... .......... .......... .......... ..........  3% 10.8M 43s
 16600K .......... .......... .......... .......... ..........  3% 9.43M 43s
 16650K .......... .......... .......... .......... ..........  3% 9.35M 43s
 16700K .......... .......... .......... .......... ..........  3% 6.94M 43s
 16750K .......... .......... .......... .......... ..........  3% 7.68M 43s
 16800K .......... .......... .......... .......... ..........  3% 12.0M 43s
 16850K .......... .......... .......... .......... ..........  3% 9.08M 43s
 16900K .......... .......... .......... .......... ..........  3% 11.9M 43s
 16950K .......... .......... .......... .......... ..........  3% 10.7M 43s
 17000K .......... .......... .......... .......... ..........  3% 12.4M 43s
 17050K .......... .......... .......... .......... ..........  3% 11.8M 43s
 17100K .......... .......... .......... .......... ..........  3% 9.98M 43s
 17150K .......... .......... .......... .......... ..........  3% 14.4M 43s
 17200K .......... .......... .......... .......... ..........  3% 23.7M 43s
 17250K .......... .......... .......... .......... ..........  3% 24.1M 43s
 17300K .......... .......... .......... .......... ..........  3% 15.5M 42s
 17350K .......... .......... .......... .......... ..........  3% 14.1M 42s
 17400K .......... .......... .......... .......... ..........  3% 15.2M 42s
 17450K .......... .......... .......... .......... ..........  3% 22.5M 42s
 17500K .......... .......... .......... .......... ..........  3% 21.7M 42s
 17550K .......... .......... .......... .......... ..........  3% 22.2M 42s
 17600K .......... .......... .......... .......... ..........  3% 16.9M 42s
 17650K .......... .......... .......... .......... ..........  3% 24.4M 42s
 17700K .......... .......... .......... .......... ..........  3% 22.0M 42s
 17750K .......... .......... .......... .......... ..........  3% 22.4M 42s
 17800K .......... .......... .......... .......... ..........  3% 23.6M 42s
 17850K .......... .......... .......... .......... ..........  3% 16.9M 42s
 17900K .......... .......... .......... .......... ..........  3% 15.4M 42s
 17950K .......... .......... .......... .......... ..........  3% 15.8M 42s
 18000K .......... .......... .......... .......... ..........  3% 22.6M 42s
 18050K .......... .......... .......... .......... ..........  3% 16.3M 42s
 18100K .......... .......... .......... .......... ..........  3% 16.7M 42s
 18150K .......... .......... .......... .......... ..........  3% 14.6M 42s
 18200K .......... .......... .......... .......... ..........  3% 11.0M 42s
 18250K .......... .......... .......... .......... ..........  3% 12.2M 42s
 18300K .......... .......... .......... .......... ..........  3% 13.8M 42s
 18350K .......... .......... .......... .......... ..........  3% 8.74M 42s
 18400K .......... .......... .......... .......... ..........  3% 8.68M 42s
 18450K .......... .......... .......... .......... ..........  3% 6.59M 42s
 18500K .......... .......... .......... .......... ..........  3% 8.08M 42s
 18550K .......... .......... .......... .......... ..........  3% 7.40M 42s
 18600K .......... .......... .......... .......... ..........  3% 7.29M 42s
 18650K .......... .......... .......... .......... ..........  3% 8.97M 42s
 18700K .......... .......... .......... .......... ..........  3% 8.65M 42s
 18750K .......... .......... .......... .......... ..........  3% 18.9M 42s
 18800K .......... .......... .......... .......... ..........  3% 32.0M 42s
 18850K .......... .......... .......... .......... ..........  3% 32.4M 42s
 18900K .......... .......... .......... .......... ..........  3% 31.7M 42s
 18950K .......... .......... .......... .......... ..........  3% 24.2M 42s
 19000K .......... .......... .......... .......... ..........  3% 31.1M 42s
 19050K .......... .......... .......... .......... ..........  3% 46.3M 41s
 19100K .......... .......... .......... .......... ..........  3% 23.4M 41s
 19150K .......... .......... .......... .......... ..........  3% 40.0M 41s
 19200K .......... .......... .......... .......... ..........  3% 23.0M 41s
 19250K .......... .......... .......... .......... ..........  3% 42.8M 41s
 19300K .......... .......... .......... .......... ..........  3% 24.7M 41s
 19350K .......... .......... .......... .......... ..........  3% 19.2M 41s
 19400K .......... .......... .......... .......... ..........  3% 17.6M 41s
 19450K .......... .......... .......... .......... ..........  3% 13.7M 41s
 19500K .......... .......... .......... .......... ..........  3% 15.1M 41s
 19550K .......... .......... .......... .......... ..........  3% 16.0M 41s
 19600K .......... .......... .......... .......... ..........  3% 10.3M 41s
 19650K .......... .......... .......... .......... ..........  3% 10.7M 41s
 19700K .......... .......... .......... .......... ..........  3% 7.18M 41s
 19750K .......... .......... .......... .......... ..........  3% 14.7M 41s
 19800K .......... .......... .......... .......... ..........  3% 12.3M 41s
 19850K .......... .......... .......... .......... ..........  3% 10.3M 41s
 19900K .......... .......... .......... .......... ..........  3% 12.0M 41s
 19950K .......... .......... .......... .......... ..........  3% 12.0M 41s
 20000K .......... .......... .......... .......... ..........  3% 10.0M 41s
 20050K .......... .......... .......... .......... ..........  3% 8.50M 41s
 20100K .......... .......... .......... .......... ..........  3% 9.37M 41s
 20150K .......... .......... .......... .......... ..........  3% 12.2M 41s
 20200K .......... .......... .......... .......... ..........  3% 7.90M 41s
 20250K .......... .......... .......... .......... ..........  3% 10.9M 41s
 20300K .......... .......... .......... .......... ..........  4% 10.4M 41s
 20350K .......... .......... .......... .......... ..........  4% 8.96M 41s
 20400K .......... .......... .......... .......... ..........  4% 10.9M 41s
 20450K .......... .......... .......... .......... ..........  4% 7.66M 41s
 20500K .......... .......... .......... .......... ..........  4% 11.2M 41s
 20550K .......... .......... .......... .......... ..........  4% 11.5M 41s
 20600K .......... .......... .......... .......... ..........  4% 9.33M 41s
 20650K .......... .......... .......... .......... ..........  4% 11.2M 41s
 20700K .......... .......... .......... .......... ..........  4% 10.6M 41s
 20750K .......... .......... .......... .......... ..........  4% 10.6M 41s
 20800K .......... .......... .......... .......... ..........  4% 10.1M 41s
 20850K .......... .......... .......... .......... ..........  4% 15.6M 41s
 20900K .......... .......... .......... .......... ..........  4% 39.2M 41s
 20950K .......... .......... .......... .......... ..........  4% 22.4M 41s
 21000K .......... .......... .......... .......... ..........  4% 65.7M 41s
 21050K .......... .......... .......... .......... ..........  4% 29.8M 41s
 21100K .......... .......... .......... .......... ..........  4% 27.5M 41s
 21150K .......... .......... .......... .......... ..........  4% 31.6M 41s
 21200K .......... .......... .......... .......... ..........  4% 20.3M 41s
 21250K .......... .......... .......... .......... ..........  4% 24.1M 41s
 21300K .......... .......... .......... .......... ..........  4% 13.7M 41s
 21350K .......... .......... .......... .......... ..........  4% 10.6M 41s
 21400K .......... .......... .......... .......... ..........  4% 12.6M 41s
 21450K .......... .......... .......... .......... ..........  4% 11.6M 41s
 21500K .......... .......... .......... .......... ..........  4% 15.9M 41s
 21550K .......... .......... .......... .......... ..........  4% 14.4M 41s
 21600K .......... .......... .......... .......... ..........  4% 11.6M 41s
 21650K .......... .......... .......... .......... ..........  4% 11.9M 41s
 21700K .......... .......... .......... .......... ..........  4% 12.0M 41s
 21750K .......... .......... .......... .......... ..........  4% 15.5M 41s
 21800K .......... .......... .......... .......... ..........  4% 16.7M 41s
 21850K .......... .......... .......... .......... ..........  4% 42.6M 40s
 21900K .......... .......... .......... .......... ..........  4% 44.3M 40s
 21950K .......... .......... .......... .......... ..........  4% 19.9M 40s
 22000K .......... .......... .......... .......... ..........  4%  242M 40s
 22050K .......... .......... .......... .......... ..........  4% 40.7M 40s
 22100K .......... .......... .......... .......... ..........  4% 50.3M 40s
 22150K .......... .......... .......... .......... ..........  4% 29.3M 40s
 22200K .......... .......... .......... .......... ..........  4% 31.9M 40s
 22250K .......... .......... .......... .......... ..........  4% 21.6M 40s
 22300K .......... .......... .......... .......... ..........  4% 45.6M 40s
 22350K .......... .......... .......... .......... ..........  4% 21.5M 40s
 22400K .......... .......... .......... .......... ..........  4% 21.5M 40s
 22450K .......... .......... .......... .......... ..........  4% 18.0M 40s
 22500K .......... .......... .......... .......... ..........  4% 22.1M 40s
 22550K .......... .......... .......... .......... ..........  4% 22.7M 40s
 22600K .......... .......... .......... .......... ..........  4% 13.6M 40s
 22650K .......... .......... .......... .......... ..........  4% 13.3M 40s
 22700K .......... .......... .......... .......... ..........  4% 13.3M 40s
 22750K .......... .......... .......... .......... ..........  4% 8.71M 40s
 22800K .......... .......... .......... .......... ..........  4% 11.0M 40s
 22850K .......... .......... .......... .......... ..........  4% 9.98M 40s
 22900K .......... .......... .......... .......... ..........  4% 11.3M 40s
 22950K .......... .......... .......... .......... ..........  4% 12.3M 40s
 23000K .......... .......... .......... .......... ..........  4% 13.6M 40s
 23050K .......... .......... .......... .......... ..........  4% 17.0M 40s
 23100K .......... .......... .......... .......... ..........  4% 9.69M 40s
 23150K .......... .......... .......... .......... ..........  4% 13.0M 40s
 23200K .......... .......... .......... .......... ..........  4% 14.6M 40s
 23250K .......... .......... .......... .......... ..........  4% 12.2M 40s
 23300K .......... .......... .......... .......... ..........  4% 14.0M 40s
 23350K .......... .......... .......... .......... ..........  4% 19.6M 40s
 23400K .......... .......... .......... .......... ..........  4% 39.3M 39s
 23450K .......... .......... .......... .......... ..........  4% 22.6M 39s
 23500K .......... .......... .......... .......... ..........  4% 38.0M 39s
 23550K .......... .......... .......... .......... ..........  4% 36.0M 39s
 23600K .......... .......... .......... .......... ..........  4% 37.8M 39s
 23650K .......... .......... .......... .......... ..........  4% 39.9M 39s
 23700K .......... .......... .......... .......... ..........  4% 20.1M 39s
 23750K .......... .......... .......... .......... ..........  4% 24.6M 39s
 23800K .......... .......... .......... .......... ..........  4% 22.5M 39s
 23850K .......... .......... .......... .......... ..........  4% 15.8M 39s
 23900K .......... .......... .......... .......... ..........  4% 15.6M 39s
 23950K .......... .......... .......... .......... ..........  4% 14.7M 39s
 24000K .......... .......... .......... .......... ..........  4% 16.7M 39s
 24050K .......... .......... .......... .......... ..........  4% 15.1M 39s
 24100K .......... .......... .......... .......... ..........  4% 15.0M 39s
 24150K .......... .......... .......... .......... ..........  4% 14.8M 39s
 24200K .......... .......... .......... .......... ..........  4% 9.63M 39s
 24250K .......... .......... .......... .......... ..........  4% 14.9M 39s
 24300K .......... .......... .......... .......... ..........  4% 14.4M 39s
 24350K .......... .......... .......... .......... ..........  4% 8.22M 39s
 24400K .......... .......... .......... .......... ..........  4% 7.82M 39s
 24450K .......... .......... .......... .......... ..........  4% 9.67M 39s
 24500K .......... .......... .......... .......... ..........  4% 9.83M 39s
 24550K .......... .......... .......... .......... ..........  4% 10.5M 39s
 24600K .......... .......... .......... .......... ..........  4% 8.30M 39s
 24650K .......... .......... .......... .......... ..........  4% 10.5M 39s
 24700K .......... .......... .......... .......... ..........  4% 8.08M 39s
 24750K .......... .......... .......... .......... ..........  4% 9.86M 39s
 24800K .......... .......... .......... .......... ..........  4% 19.4M 39s
 24850K .......... .......... .......... .......... ..........  4% 20.4M 39s
 24900K .......... .......... .......... .......... ..........  4% 11.4M 39s
 24950K .......... .......... .......... .......... ..........  4% 15.2M 39s
 25000K .......... .......... .......... .......... ..........  4% 13.5M 39s
 25050K .......... .......... .......... .......... ..........  4% 12.5M 39s
 25100K .......... .......... .......... .......... ..........  4% 10.9M 39s
 25150K .......... .......... .......... .......... ..........  4% 12.6M 39s
 25200K .......... .......... .......... .......... ..........  4% 11.8M 39s
 25250K .......... .......... .......... .......... ..........  4% 12.5M 39s
 25300K .......... .......... .......... .......... ..........  4% 11.8M 39s
 25350K .......... .......... .......... .......... ..........  4% 9.03M 39s
 25400K .......... .......... .......... .......... ..........  5% 14.9M 39s
 25450K .......... .......... .......... .......... ..........  5% 11.2M 39s
 25500K .......... .......... .......... .......... ..........  5% 15.2M 39s
 25550K .......... .......... .......... .......... ..........  5% 12.5M 39s
 25600K .......... .......... .......... .......... ..........  5% 11.1M 39s
 25650K .......... .......... .......... .......... ..........  5% 12.3M 39s
 25700K .......... .......... .......... .......... ..........  5% 10.8M 39s
 25750K .......... .......... .......... .......... ..........  5% 11.7M 39s
 25800K .......... .......... .......... .......... ..........  5% 16.1M 39s
 25850K .......... .......... .......... .......... ..........  5% 14.6M 39s
 25900K .......... .......... .......... .......... ..........  5% 15.6M 39s
 25950K .......... .......... .......... .......... ..........  5% 10.9M 39s
 26000K .......... .......... .......... .......... ..........  5% 15.3M 39s
 26050K .......... .......... .......... .......... ..........  5% 14.1M 39s
 26100K .......... .......... .......... .......... ..........  5% 9.99M 39s
 26150K .......... .......... .......... .......... ..........  5% 7.67M 39s
 26200K .......... .......... .......... .......... ..........  5% 7.39M 39s
 26250K .......... .......... .......... .......... ..........  5% 7.41M 39s
 26300K .......... .......... .......... .......... ..........  5% 7.92M 39s
 26350K .......... .......... .......... .......... ..........  5% 6.93M 39s
 26400K .......... .......... .......... .......... ..........  5% 10.3M 39s
 26450K .......... .......... .......... .......... ..........  5% 7.19M 39s
 26500K .......... .......... .......... .......... ..........  5% 9.72M 39s
 26550K .......... .......... .......... .......... ..........  5% 9.20M 39s
 26600K .......... .......... .......... .......... ..........  5% 5.78M 39s
 26650K .......... .......... .......... .......... ..........  5% 6.71M 39s
 26700K .......... .......... .......... .......... ..........  5% 9.13M 39s
 26750K .......... .......... .......... .......... ..........  5% 9.40M 39s
 26800K .......... .......... .......... .......... ..........  5% 11.2M 39s
 26850K .......... .......... .......... .......... ..........  5% 5.82M 39s
 26900K .......... .......... .......... .......... ..........  5% 10.2M 39s
 26950K .......... .......... .......... .......... ..........  5% 6.55M 39s
 27000K .......... .......... .......... .......... ..........  5% 8.61M 40s
 27050K .......... .......... .......... .......... ..........  5% 9.65M 40s
 27100K .......... .......... .......... .......... ..........  5% 5.64M 40s
 27150K .......... .......... .......... .......... ..........  5% 6.16M 40s
 27200K .......... .......... .......... .......... ..........  5% 5.19M 40s
 27250K .......... .......... .......... .......... ..........  5% 7.79M 40s
 27300K .......... .......... .......... .......... ..........  5% 7.08M 40s
 27350K .......... .......... .......... .......... ..........  5% 7.61M 40s
 27400K .......... .......... .......... .......... ..........  5% 9.01M 40s
 27450K .......... .......... .......... .......... ..........  5% 6.51M 40s
 27500K .......... .......... .......... .......... ..........  5% 7.00M 40s
 27550K .......... .......... .......... .......... ..........  5% 5.92M 40s
 27600K .......... .......... .......... .......... ..........  5% 4.77M 40s
 27650K .......... .......... .......... .......... ..........  5% 5.92M 40s
 27700K .......... .......... .......... .......... ..........  5% 4.65M 40s
 27750K .......... .......... .......... .......... ..........  5% 10.3M 40s
 27800K .......... .......... .......... .......... ..........  5% 21.0M 40s
 27850K .......... .......... .......... .......... ..........  5% 18.3M 40s
 27900K .......... .......... .......... .......... ..........  5% 17.1M 40s
 27950K .......... .......... .......... .......... ..........  5% 6.42M 40s
 28000K .......... .......... .......... .......... ..........  5% 5.74M 40s
 28050K .......... .......... .......... .......... ..........  5% 9.00M 40s
 28100K .......... .......... .......... .......... ..........  5% 6.84M 40s
 28150K .......... .......... .......... .......... ..........  5% 8.76M 40s
 28200K .......... .......... .......... .......... ..........  5% 6.64M 41s
 28250K .......... .......... .......... .......... ..........  5% 6.57M 41s
 28300K .......... .......... .......... .......... ..........  5% 7.48M 41s
 28350K .......... .......... .......... .......... ..........  5% 6.40M 41s
 28400K .......... .......... .......... .......... ..........  5% 20.0M 41s
 28450K .......... .......... .......... .......... ..........  5% 32.7M 41s
 28500K .......... .......... .......... .......... ..........  5% 25.7M 41s
 28550K .......... .......... .......... .......... ..........  5% 30.4M 40s
 28600K .......... .......... .......... .......... ..........  5% 18.5M 40s
 28650K .......... .......... .......... .......... ..........  5% 18.0M 40s
 28700K .......... .......... .......... .......... ..........  5% 23.2M 40s
 28750K .......... .......... .......... .......... ..........  5% 23.4M 40s
 28800K .......... .......... .......... .......... ..........  5% 17.3M 40s
 28850K .......... .......... .......... .......... ..........  5% 14.9M 40s
 28900K .......... .......... .......... .......... ..........  5% 11.7M 40s
 28950K .......... .......... .......... .......... ..........  5% 11.7M 40s
 29000K .......... .......... .......... .......... ..........  5% 15.3M 40s
 29050K .......... .......... .......... .......... ..........  5% 13.9M 40s
 29100K .......... .......... .......... .......... ..........  5% 11.7M 40s
 29150K .......... .......... .......... .......... ..........  5% 15.8M 40s
 29200K .......... .......... .......... .......... ..........  5% 12.7M 40s
 29250K .......... .......... .......... .......... ..........  5% 15.1M 40s
 29300K .......... .......... .......... .......... ..........  5% 16.4M 40s
 29350K .......... .......... .......... .......... ..........  5% 13.6M 40s
 29400K .......... .......... .......... .......... ..........  5% 18.4M 40s
 29450K .......... .......... .......... .......... ..........  5% 11.4M 40s
 29500K .......... .......... .......... .......... ..........  5% 18.1M 40s
 29550K .......... .......... .......... .......... ..........  5% 16.5M 40s
 29600K .......... .......... .......... .......... ..........  5% 35.0M 40s
 29650K .......... .......... .......... .......... ..........  5% 21.0M 40s
 29700K .......... .......... .......... .......... ..........  5% 37.6M 40s
 29750K .......... .......... .......... .......... ..........  5% 30.2M 40s
 29800K .......... .......... .......... .......... ..........  5% 79.9M 40s
 29850K .......... .......... .......... .......... ..........  5% 24.2M 40s
 29900K .......... .......... .......... .......... ..........  5% 15.7M 40s
 29950K .......... .......... .......... .......... ..........  5% 11.8M 40s
 30000K .......... .......... .......... .......... ..........  5% 22.2M 40s
 30050K .......... .......... .......... .......... ..........  5% 16.2M 40s
 30100K .......... .......... .......... .......... ..........  5% 15.4M 40s
 30150K .......... .......... .......... .......... ..........  5% 17.1M 40s
 30200K .......... .......... .......... .......... ..........  5% 11.4M 40s
 30250K .......... .......... .......... .......... ..........  5% 13.6M 40s
 30300K .......... .......... .......... .......... ..........  5% 15.2M 40s
 30350K .......... .......... .......... .......... ..........  5% 9.44M 40s
 30400K .......... .......... .......... .......... ..........  5% 16.2M 40s
 30450K .......... .......... .......... .......... ..........  5% 11.9M 40s
 30500K .......... .......... .......... .......... ..........  6% 15.9M 40s
 30550K .......... .......... .......... .......... ..........  6% 7.54M 40s
 30600K .......... .......... .......... .......... ..........  6% 5.92M 40s
 30650K .......... .......... .......... .......... ..........  6% 5.56M 40s
 30700K .......... .......... .......... .......... ..........  6% 5.54M 40s
 30750K .......... .......... .......... .......... ..........  6% 4.83M 40s
 30800K .......... .......... .......... .......... ..........  6% 4.69M 40s
 30850K .......... .......... .......... .......... ..........  6% 14.4M 40s
 30900K .......... .......... .......... .......... ..........  6% 30.4M 40s
 30950K .......... .......... .......... .......... ..........  6% 19.8M 40s
 31000K .......... .......... .......... .......... ..........  6% 23.9M 40s
 31050K .......... .......... .......... .......... ..........  6% 18.5M 40s
 31100K .......... .......... .......... .......... ..........  6% 11.6M 40s
 31150K .......... .......... .......... .......... ..........  6% 17.5M 40s
 31200K .......... .......... .......... .......... ..........  6% 12.9M 40s
 31250K .......... .......... .......... .......... ..........  6% 14.7M 40s
 31300K .......... .......... .......... .......... ..........  6% 16.3M 40s
 31350K .......... .......... .......... .......... ..........  6% 14.7M 40s
 31400K .......... .......... .......... .......... ..........  6% 12.5M 40s
 31450K .......... .......... .......... .......... ..........  6% 15.2M 40s
 31500K .......... .......... .......... .......... ..........  6% 10.8M 40s
 31550K .......... .......... .......... .......... ..........  6% 15.6M 40s
 31600K .......... .......... .......... .......... ..........  6% 11.9M 40s
 31650K .......... .......... .......... .......... ..........  6% 8.40M 40s
 31700K .......... .......... .......... .......... ..........  6% 7.69M 40s
 31750K .......... .......... .......... .......... ..........  6% 7.35M 40s
 31800K .......... .......... .......... .......... ..........  6% 6.57M 40s
 31850K .......... .......... .......... .......... ..........  6% 5.48M 40s
 31900K .......... .......... .......... .......... ..........  6% 6.66M 40s
 31950K .......... .......... .......... .......... ..........  6% 6.28M 40s
 32000K .......... .......... .......... .......... ..........  6% 7.56M 40s
 32050K .......... .......... .......... .......... ..........  6% 23.9M 40s
 32100K .......... .......... .......... .......... ..........  6% 22.7M 40s
 32150K .......... .......... .......... .......... ..........  6% 17.0M 40s
 32200K .......... .......... .......... .......... ..........  6% 25.5M 40s
 32250K .......... .......... .......... .......... ..........  6% 21.7M 40s
 32300K .......... .......... .......... .......... ..........  6% 25.2M 40s
 32350K .......... .......... .......... .......... ..........  6% 12.4M 40s
 32400K .......... .......... .......... .......... ..........  6% 23.5M 40s
 32450K .......... .......... .......... .......... ..........  6% 14.8M 40s
 32500K .......... .......... .......... .......... ..........  6% 13.1M 40s
 32550K .......... .......... .......... .......... ..........  6% 10.4M 40s
 32600K .......... .......... .......... .......... ..........  6% 7.04M 40s
 32650K .......... .......... .......... .......... ..........  6% 8.24M 40s
 32700K .......... .......... .......... .......... ..........  6% 7.63M 40s
 32750K .......... .......... .......... .......... ..........  6% 7.42M 40s
 32800K .......... .......... .......... .......... ..........  6% 9.28M 40s
 32850K .......... .......... .......... .......... ..........  6% 6.86M 40s
 32900K .......... .......... .......... .......... ..........  6% 6.20M 40s
 32950K .......... .......... .......... .......... ..........  6% 6.76M 40s
 33000K .......... .......... .......... .......... ..........  6% 8.44M 40s
 33050K .......... .......... .......... .......... ..........  6% 8.51M 40s
 33100K .......... .......... .......... .......... ..........  6% 6.96M 40s
 33150K .......... .......... .......... .......... ..........  6% 6.73M 40s
 33200K .......... .......... .......... .......... ..........  6% 5.62M 40s
 33250K .......... .......... .......... .......... ..........  6% 7.27M 40s
 33300K .......... .......... .......... .......... ..........  6% 6.05M 40s
 33350K .......... .......... .......... .......... ..........  6% 5.35M 40s
 33400K .......... .......... .......... .......... ..........  6% 4.36M 40s
 33450K .......... .......... .......... .......... ..........  6% 3.49M 41s
 33500K .......... .......... .......... .......... ..........  6% 3.60M 41s
 33550K .......... .......... .......... .......... ..........  6% 4.91M 41s
 33600K .......... .......... .......... .......... ..........  6% 10.6M 41s
 33650K .......... .......... .......... .......... ..........  6% 6.83M 41s
 33700K .......... .......... .......... .......... ..........  6% 5.08M 41s
 33750K .......... .......... .......... .......... ..........  6% 4.96M 41s
 33800K .......... .......... .......... .......... ..........  6% 11.5M 41s
 33850K .......... .......... .......... .......... ..........  6% 6.23M 41s
 33900K .......... .......... .......... .......... ..........  6% 13.3M 41s
 33950K .......... .......... .......... .......... ..........  6% 19.0M 41s
 34000K .......... .......... .......... .......... ..........  6% 21.5M 41s
 34050K .......... .......... .......... .......... ..........  6% 23.5M 41s
 34100K .......... .......... .......... .......... ..........  6% 18.3M 41s
 34150K .......... .......... .......... .......... ..........  6% 19.9M 41s
 34200K .......... .......... .......... .......... ..........  6% 15.4M 41s
 34250K .......... .......... .......... .......... ..........  6% 15.3M 41s
 34300K .......... .......... .......... .......... ..........  6% 13.8M 41s
 34350K .......... .......... .......... .......... ..........  6% 11.8M 41s
 34400K .......... .......... .......... .......... ..........  6% 10.7M 41s
 34450K .......... .......... .......... .......... ..........  6% 11.7M 41s
 34500K .......... .......... .......... .......... ..........  6% 9.04M 41s
 34550K .......... .......... .......... .......... ..........  6% 17.2M 41s
 34600K .......... .......... .......... .......... ..........  6% 10.4M 41s
 34650K .......... .......... .......... .......... ..........  6% 9.70M 41s
 34700K .......... .......... .......... .......... ..........  6% 11.0M 41s
 34750K .......... .......... .......... .......... ..........  6% 8.92M 41s
 34800K .......... .......... .......... .......... ..........  6% 10.2M 41s
 34850K .......... .......... .......... .......... ..........  6% 7.67M 41s
 34900K .......... .......... .......... .......... ..........  6% 8.78M 41s
 34950K .......... .......... .......... .......... ..........  6% 6.48M 41s
 35000K .......... .......... .......... .......... ..........  6% 8.85M 41s
 35050K .......... .......... .......... .......... ..........  6% 10.5M 41s
 35100K .......... .......... .......... .......... ..........  6% 7.41M 41s
 35150K .......... .......... .......... .......... ..........  6% 9.46M 41s
 35200K .......... .......... .......... .......... ..........  6% 14.3M 41s
 35250K .......... .......... .......... .......... ..........  6% 42.9M 41s
 35300K .......... .......... .......... .......... ..........  6% 30.8M 41s
 35350K .......... .......... .......... .......... ..........  6% 32.7M 41s
 35400K .......... .......... .......... .......... ..........  6% 21.4M 41s
 35450K .......... .......... .......... .......... ..........  6% 29.7M 41s
 35500K .......... .......... .......... .......... ..........  6% 35.0M 41s
 35550K .......... .......... .......... .......... ..........  7% 21.9M 41s
 35600K .......... .......... .......... .......... ..........  7% 19.2M 41s
 35650K .......... .......... .......... .......... ..........  7% 23.8M 40s
 35700K .......... .......... .......... .......... ..........  7% 17.0M 40s
 35750K .......... .......... .......... .......... ..........  7% 15.8M 40s
 35800K .......... .......... .......... .......... ..........  7% 17.0M 40s
 35850K .......... .......... .......... .......... ..........  7% 22.1M 40s
 35900K .......... .......... .......... .......... ..........  7% 15.6M 40s
 35950K .......... .......... .......... .......... ..........  7% 16.8M 40s
 36000K .......... .......... .......... .......... ..........  7% 15.8M 40s
 36050K .......... .......... .......... .......... ..........  7% 15.6M 40s
 36100K .......... .......... .......... .......... ..........  7% 16.2M 40s
 36150K .......... .......... .......... .......... ..........  7% 17.2M 40s
 36200K .......... .......... .......... .......... ..........  7% 16.8M 40s
 36250K .......... .......... .......... .......... ..........  7% 17.1M 40s
 36300K .......... .......... .......... .......... ..........  7% 9.46M 40s
 36350K .......... .......... .......... .......... ..........  7% 10.9M 40s
 36400K .......... .......... .......... .......... ..........  7% 11.4M 40s
 36450K .......... .......... .......... .......... ..........  7% 9.37M 40s
 36500K .......... .......... .......... .......... ..........  7% 12.7M 40s
 36550K .......... .......... .......... .......... ..........  7% 14.0M 40s
 36600K .......... .......... .......... .......... ..........  7% 10.4M 40s
 36650K .......... .......... .......... .......... ..........  7% 11.5M 40s
 36700K .......... .......... .......... .......... ..........  7% 12.4M 40s
 36750K .......... .......... .......... .......... ..........  7% 11.2M 40s
 36800K .......... .......... .......... .......... ..........  7% 13.9M 40s
 36850K .......... .......... .......... .......... ..........  7% 13.8M 40s
 36900K .......... .......... .......... .......... ..........  7% 16.8M 40s
 36950K .......... .......... .......... .......... ..........  7% 14.0M 40s
 37000K .......... .......... .......... .......... ..........  7% 17.0M 40s
 37050K .......... .......... .......... .......... ..........  7% 15.5M 40s
 37100K .......... .......... .......... .......... ..........  7% 9.03M 40s
 37150K .......... .......... .......... .......... ..........  7% 9.61M 40s
 37200K .......... .......... .......... .......... ..........  7% 8.07M 40s
 37250K .......... .......... .......... .......... ..........  7% 7.92M 40s
 37300K .......... .......... .......... .......... ..........  7% 6.16M 40s
 37350K .......... .......... .......... .......... ..........  7% 5.31M 40s
 37400K .......... .......... .......... .......... ..........  7% 5.22M 40s
 37450K .......... .......... .......... .......... ..........  7% 4.67M 40s
 37500K .......... .......... .......... .......... ..........  7% 6.18M 40s
 37550K .......... .......... .......... .......... ..........  7% 5.03M 40s
 37600K .......... .......... .......... .......... ..........  7% 8.88M 41s
 37650K .......... .......... .......... .......... ..........  7% 7.69M 41s
 37700K .......... .......... .......... .......... ..........  7% 5.00M 41s
 37750K .......... .......... .......... .......... ..........  7% 5.48M 41s
 37800K .......... .......... .......... .......... ..........  7% 5.62M 41s
 37850K .......... .......... .......... .......... ..........  7% 4.70M 41s
 37900K .......... .......... .......... .......... ..........  7% 5.97M 41s
 37950K .......... .......... .......... .......... ..........  7% 4.73M 41s
 38000K .......... .......... .......... .......... ..........  7% 4.74M 41s
 38050K .......... .......... .......... .......... ..........  7% 4.08M 41s
 38100K .......... .......... .......... .......... ..........  7% 3.53M 41s
 38150K .......... .......... .......... .......... ..........  7% 3.87M 41s
 38200K .......... .......... .......... .......... ..........  7% 5.73M 41s
 38250K .......... .......... .......... .......... ..........  7% 12.6M 41s
 38300K .......... .......... .......... .......... ..........  7% 17.3M 41s
 38350K .......... .......... .......... .......... ..........  7% 12.8M 41s
 38400K .......... .......... .......... .......... ..........  7% 14.0M 41s
 38450K .......... .......... .......... .......... ..........  7% 11.1M 41s
 38500K .......... .......... .......... .......... ..........  7% 12.4M 41s
 38550K .......... .......... .......... .......... ..........  7% 11.6M 41s
 38600K .......... .......... .......... .......... ..........  7% 9.58M 41s
 38650K .......... .......... .......... .......... ..........  7% 9.82M 41s
 38700K .......... .......... .......... .......... ..........  7% 7.05M 41s
 38750K .......... .......... .......... .......... ..........  7% 7.54M 41s
 38800K .......... .......... .......... .......... ..........  7% 12.5M 41s
 38850K .......... .......... .......... .......... ..........  7% 9.63M 41s
 38900K .......... .......... .......... .......... ..........  7% 12.1M 41s
 38950K .......... .......... .......... .......... ..........  7% 11.1M 41s
 39000K .......... .......... .......... .......... ..........  7% 9.58M 41s
 39050K .......... .......... .......... .......... ..........  7% 7.76M 41s
 39100K .......... .......... .......... .......... ..........  7% 5.85M 41s
 39150K .......... .......... .......... .......... ..........  7% 6.70M 41s
 39200K .......... .......... .......... .......... ..........  7% 5.65M 41s
 39250K .......... .......... .......... .......... ..........  7% 6.66M 41s
 39300K .......... .......... .......... .......... ..........  7% 11.1M 41s
 39350K .......... .......... .......... .......... ..........  7% 23.6M 41s
 39400K .......... .......... .......... .......... ..........  7% 39.8M 41s
 39450K .......... .......... .......... .......... ..........  7% 23.8M 41s
 39500K .......... .......... .......... .......... ..........  7% 21.7M 41s
 39550K .......... .......... .......... .......... ..........  7% 18.6M 41s
 39600K .......... .......... .......... .......... ..........  7% 15.2M 41s
 39650K .......... .......... .......... .......... ..........  7% 20.8M 41s
 39700K .......... .......... .......... .......... ..........  7% 10.9M 41s
 39750K .......... .......... .......... .......... ..........  7% 14.3M 41s
 39800K .......... .......... .......... .......... ..........  7% 15.1M 41s
 39850K .......... .......... .......... .......... ..........  7% 10.7M 41s
 39900K .......... .......... .......... .......... ..........  7% 13.9M 41s
 39950K .......... .......... .......... .......... ..........  7% 11.4M 41s
 40000K .......... .......... .......... .......... ..........  7% 13.9M 41s
 40050K .......... .......... .......... .......... ..........  7% 14.7M 41s
 40100K .......... .......... .......... .......... ..........  7% 11.2M 41s
 40150K .......... .......... .......... .......... ..........  7% 9.09M 41s
 40200K .......... .......... .......... .......... ..........  7% 23.0M 41s
 40250K .......... .......... .......... .......... ..........  7% 14.4M 41s
 40300K .......... .......... .......... .......... ..........  7% 16.2M 41s
 40350K .......... .......... .......... .......... ..........  7% 11.3M 41s
 40400K .......... .......... .......... .......... ..........  7% 11.2M 41s
 40450K .......... .......... .......... .......... ..........  7% 11.6M 41s
 40500K .......... .......... .......... .......... ..........  7% 12.6M 41s
 40550K .......... .......... .......... .......... ..........  7% 14.4M 41s
 40600K .......... .......... .......... .......... ..........  7% 10.8M 41s
 40650K .......... .......... .......... .......... ..........  8% 13.3M 41s
 40700K .......... .......... .......... .......... ..........  8% 10.7M 41s
 40750K .......... .......... .......... .......... ..........  8% 12.3M 41s
 40800K .......... .......... .......... .......... ..........  8% 17.8M 41s
 40850K .......... .......... .......... .......... ..........  8% 23.8M 41s
 40900K .......... .......... .......... .......... ..........  8% 23.4M 41s
 40950K .......... .......... .......... .......... ..........  8% 14.7M 41s
 41000K .......... .......... .......... .......... ..........  8% 23.8M 41s
 41050K .......... .......... .......... .......... ..........  8% 16.5M 41s
 41100K .......... .......... .......... .......... ..........  8% 8.59M 41s
 41150K .......... .......... .......... .......... ..........  8% 8.08M 41s
 41200K .......... .......... .......... .......... ..........  8% 10.3M 41s
 41250K .......... .......... .......... .......... ..........  8% 11.2M 41s
 41300K .......... .......... .......... .......... ..........  8% 8.73M 41s
 41350K .......... .......... .......... .......... ..........  8% 8.49M 41s
 41400K .......... .......... .......... .......... ..........  8% 7.83M 41s
 41450K .......... .......... .......... .......... ..........  8% 7.97M 41s
 41500K .......... .......... .......... .......... ..........  8% 8.42M 41s
 41550K .......... .......... .......... .......... ..........  8% 6.94M 41s
 41600K .......... .......... .......... .......... ..........  8% 4.83M 41s
 41650K .......... .......... .......... .......... ..........  8% 11.3M 41s
 41700K .......... .......... .......... .......... ..........  8% 8.32M 41s
 41750K .......... .......... .......... .......... ..........  8% 9.11M 41s
 41800K .......... .......... .......... .......... ..........  8% 7.14M 41s
 41850K .......... .......... .......... .......... ..........  8% 5.38M 41s
 41900K .......... .......... .......... .......... ..........  8% 7.71M 41s
 41950K .......... .......... .......... .......... ..........  8% 5.39M 41s
 42000K .......... .......... .......... .......... ..........  8% 6.66M 41s
 42050K .......... .......... .......... .......... ..........  8% 6.60M 41s
 42100K .......... .......... .......... .......... ..........  8% 4.93M 41s
 42150K .......... .......... .......... .......... ..........  8% 5.59M 41s
 42200K .......... .......... .......... .......... ..........  8% 5.13M 41s
 42250K .......... .......... .......... .......... ..........  8% 6.10M 41s
 42300K .......... .......... .......... .......... ..........  8% 16.6M 41s
 42350K .......... .......... .......... .......... ..........  8% 22.4M 41s
 42400K .......... .......... .......... .......... ..........  8% 32.5M 41s
 42450K .......... .......... .......... .......... ..........  8% 16.7M 41s
 42500K .......... .......... .......... .......... ..........  8% 36.3M 41s
 42550K .......... .......... .......... .......... ..........  8% 21.4M 41s
 42600K .......... .......... .......... .......... ..........  8% 11.1M 41s
 42650K .......... .......... .......... .......... ..........  8% 16.9M 41s
 42700K .......... .......... .......... .......... ..........  8% 8.84M 41s
 42750K .......... .......... .......... .......... ..........  8% 12.7M 41s
 42800K .......... .......... .......... .......... ..........  8% 9.68M 41s
 42850K .......... .......... .......... .......... ..........  8% 9.44M 41s
 42900K .......... .......... .......... .......... ..........  8% 13.1M 41s
 42950K .......... .......... .......... .......... ..........  8% 10.6M 41s
 43000K .......... .......... .......... .......... ..........  8% 9.38M 41s
 43050K .......... .......... .......... .......... ..........  8%  132M 41s
 43100K .......... .......... .......... .......... ..........  8% 28.2M 41s
 43150K .......... .......... .......... .......... ..........  8% 14.6M 41s
 43200K .......... .......... .......... .......... ..........  8%  117M 41s
 43250K .......... .......... .......... .......... ..........  8%  163M 41s
 43300K .......... .......... .......... .......... ..........  8% 39.5M 41s
 43350K .......... .......... .......... .......... ..........  8% 30.4M 41s
 43400K .......... .......... .......... .......... ..........  8% 23.4M 41s
 43450K .......... .......... .......... .......... ..........  8% 26.5M 41s
 43500K .......... .......... .......... .......... ..........  8% 21.9M 41s
 43550K .......... .......... .......... .......... ..........  8% 21.5M 41s
 43600K .......... .......... .......... .......... ..........  8% 17.8M 41s
 43650K .......... .......... .......... .......... ..........  8% 18.6M 41s
 43700K .......... .......... .......... .......... ..........  8% 16.8M 41s
 43750K .......... .......... .......... .......... ..........  8% 19.1M 41s
 43800K .......... .......... .......... .......... ..........  8% 14.9M 41s
 43850K .......... .......... .......... .......... ..........  8% 17.9M 41s
 43900K .......... .......... .......... .......... ..........  8% 20.2M 41s
 43950K .......... .......... .......... .......... ..........  8% 12.5M 41s
 44000K .......... .......... .......... .......... ..........  8% 15.6M 41s
 44050K .......... .......... .......... .......... ..........  8% 14.9M 41s
 44100K .......... .......... .......... .......... ..........  8% 12.4M 41s
 44150K .......... .......... .......... .......... ..........  8% 15.7M 41s
 44200K .......... .......... .......... .......... ..........  8% 9.24M 41s
 44250K .......... .......... .......... .......... ..........  8% 13.3M 41s
 44300K .......... .......... .......... .......... ..........  8% 13.6M 41s
 44350K .......... .......... .......... .......... ..........  8% 11.0M 41s
 44400K .......... .......... .......... .......... ..........  8% 9.32M 41s
 44450K .......... .......... .......... .......... ..........  8% 6.61M 41s
 44500K .......... .......... .......... .......... ..........  8% 8.70M 41s
 44550K .......... .......... .......... .......... ..........  8% 8.93M 41s
 44600K .......... .......... .......... .......... ..........  8% 8.05M 41s
 44650K .......... .......... .......... .......... ..........  8% 7.27M 41s
 44700K .......... .......... .......... .......... ..........  8% 7.85M 41s
 44750K .......... .......... .......... .......... ..........  8% 9.00M 41s
 44800K .......... .......... .......... .......... ..........  8% 8.23M 41s
 44850K .......... .......... .......... .......... ..........  8% 7.08M 41s
 44900K .......... .......... .......... .......... ..........  8% 11.3M 41s
 44950K .......... .......... .......... .......... ..........  8% 4.80M 41s
 45000K .......... .......... .......... .......... ..........  8% 13.5M 41s
 45050K .......... .......... .......... .......... ..........  8% 8.77M 41s
 45100K .......... .......... .......... .......... ..........  8% 10.9M 41s
 45150K .......... .......... .......... .......... ..........  8% 8.66M 41s
 45200K .......... .......... .......... .......... ..........  8% 9.30M 41s
 45250K .......... .......... .......... .......... ..........  8% 9.21M 41s
 45300K .......... .......... .......... .......... ..........  8% 15.1M 41s
 45350K .......... .......... .......... .......... ..........  8% 12.9M 41s
 45400K .......... .......... .......... .......... ..........  8% 14.5M 41s
 45450K .......... .......... .......... .......... ..........  8% 12.8M 41s
 45500K .......... .......... .......... .......... ..........  8% 18.1M 41s
 45550K .......... .......... .......... .......... ..........  8% 15.3M 41s
 45600K .......... .......... .......... .......... ..........  8% 11.5M 41s
 45650K .......... .......... .......... .......... ..........  8% 15.0M 41s
 45700K .......... .......... .......... .......... ..........  8% 16.5M 41s
 45750K .......... .......... .......... .......... ..........  9% 15.8M 41s
 45800K .......... .......... .......... .......... ..........  9% 16.0M 41s
 45850K .......... .......... .......... .......... ..........  9% 19.2M 41s
 45900K .......... .......... .......... .......... ..........  9% 15.7M 41s
 45950K .......... .......... .......... .......... ..........  9% 20.8M 41s
 46000K .......... .......... .......... .......... ..........  9% 17.1M 40s
 46050K .......... .......... .......... .......... ..........  9% 14.4M 40s
 46100K .......... .......... .......... .......... ..........  9% 12.5M 40s
 46150K .......... .......... .......... .......... ..........  9% 17.6M 40s
 46200K .......... .......... .......... .......... ..........  9% 9.47M 40s
 46250K .......... .......... .......... .......... ..........  9% 16.0M 40s
 46300K .......... .......... .......... .......... ..........  9% 12.0M 40s
 46350K .......... .......... .......... .......... ..........  9% 7.08M 40s
 46400K .......... .......... .......... .......... ..........  9% 9.38M 40s
 46450K .......... .......... .......... .......... ..........  9% 5.05M 41s
 46500K .......... .......... .......... .......... ..........  9% 6.64M 41s
 46550K .......... .......... .......... .......... ..........  9% 6.27M 41s
 46600K .......... .......... .......... .......... ..........  9% 6.45M 41s
 46650K .......... .......... .......... .......... ..........  9% 20.8M 41s
 46700K .......... .......... .......... .......... ..........  9% 15.2M 41s
 46750K .......... .......... .......... .......... ..........  9% 23.4M 41s
 46800K .......... .......... .......... .......... ..........  9% 9.26M 41s
 46850K .......... .......... .......... .......... ..........  9% 9.26M 41s
 46900K .......... .......... .......... .......... ..........  9% 11.5M 41s
 46950K .......... .......... .......... .......... ..........  9% 10.2M 41s
 47000K .......... .......... .......... .......... ..........  9% 7.26M 41s
 47050K .......... .......... .......... .......... ..........  9% 7.87M 41s
 47100K .......... .......... .......... .......... ..........  9% 7.16M 41s
 47150K .......... .......... .......... .......... ..........  9% 8.53M 41s
 47200K .......... .......... .......... .......... ..........  9% 6.79M 41s
 47250K .......... .......... .......... .......... ..........  9% 8.45M 41s
 47300K .......... .......... .......... .......... ..........  9% 9.39M 41s
 47350K .......... .......... .......... .......... ..........  9% 8.12M 41s
 47400K .......... .......... .......... .......... ..........  9% 9.01M 41s
 47450K .......... .......... .......... .......... ..........  9% 8.85M 41s
 47500K .......... .......... .......... .......... ..........  9% 7.72M 41s
 47550K .......... .......... .......... .......... ..........  9% 10.4M 41s
 47600K .......... .......... .......... .......... ..........  9% 18.7M 41s
 47650K .......... .......... .......... .......... ..........  9% 16.8M 41s
 47700K .......... .......... .......... .......... ..........  9% 11.0M 41s
 47750K .......... .......... .......... .......... ..........  9% 21.0M 41s
 47800K .......... .......... .......... .......... ..........  9% 18.3M 41s
 47850K .......... .......... .......... .......... ..........  9% 17.2M 41s
 47900K .......... .......... .......... .......... ..........  9% 17.1M 41s
 47950K .......... .......... .......... .......... ..........  9% 13.5M 41s
 48000K .......... .......... .......... .......... ..........  9% 19.0M 40s
 48050K .......... .......... .......... .......... ..........  9% 18.0M 40s
 48100K .......... .......... .......... .......... ..........  9% 16.1M 40s
 48150K .......... .......... .......... .......... ..........  9% 17.5M 40s
 48200K .......... .......... .......... .......... ..........  9% 16.1M 40s
 48250K .......... .......... .......... .......... ..........  9% 22.5M 40s
 48300K .......... .......... .......... .......... ..........  9% 23.6M 40s
 48350K .......... .......... .......... .......... ..........  9% 38.1M 40s
 48400K .......... .......... .......... .......... ..........  9% 21.5M 40s
 48450K .......... .......... .......... .......... ..........  9% 36.3M 40s
 48500K .......... .......... .......... .......... ..........  9% 37.4M 40s
 48550K .......... .......... .......... .......... ..........  9% 31.7M 40s
 48600K .......... .......... .......... .......... ..........  9% 15.5M 40s
 48650K .......... .......... .......... .......... ..........  9% 21.5M 40s
 48700K .......... .......... .......... .......... ..........  9% 11.8M 40s
 48750K .......... .......... .......... .......... ..........  9% 17.0M 40s
 48800K .......... .......... .......... .......... ..........  9% 12.0M 40s
 48850K .......... .......... .......... .......... ..........  9% 13.3M 40s
 48900K .......... .......... .......... .......... ..........  9% 13.0M 40s
 48950K .......... .......... .......... .......... ..........  9% 10.7M 40s
 49000K .......... .......... .......... .......... ..........  9% 11.7M 40s
 49050K .......... .......... .......... .......... ..........  9% 7.97M 40s
 49100K .......... .......... .......... .......... ..........  9% 6.53M 40s
 49150K .......... .......... .......... .......... ..........  9% 7.22M 40s
 49200K .......... .......... .......... .......... ..........  9% 6.96M 40s
 49250K .......... .......... .......... .......... ..........  9% 9.66M 40s
 49300K .......... .......... .......... .......... ..........  9% 11.6M 40s
 49350K .......... .......... .......... .......... ..........  9% 28.2M 40s
 49400K .......... .......... .......... .......... ..........  9% 26.0M 40s
 49450K .......... .......... .......... .......... ..........  9% 22.4M 40s
 49500K .......... .......... .......... .......... ..........  9% 11.8M 40s
 49550K .......... .......... .......... .......... ..........  9% 19.5M 40s
 49600K .......... .......... .......... .......... ..........  9% 10.4M 40s
 49650K .......... .......... .......... .......... ..........  9% 11.6M 40s
 49700K .......... .......... .......... .......... ..........  9% 10.7M 40s
 49750K .......... .......... .......... .......... ..........  9% 11.6M 40s
 49800K .......... .......... .......... .......... ..........  9% 12.0M 40s
 49850K .......... .......... .......... .......... ..........  9% 10.3M 40s
 49900K .......... .......... .......... .......... ..........  9% 12.7M 40s
 49950K .......... .......... .......... .......... ..........  9% 7.49M 40s
 50000K .......... .......... .......... .......... ..........  9% 9.09M 40s
 50050K .......... .......... .......... .......... ..........  9% 8.61M 40s
 50100K .......... .......... .......... .......... ..........  9% 7.43M 40s
 50150K .......... .......... .......... .......... ..........  9% 6.18M 40s
 50200K .......... .......... .......... .......... ..........  9% 5.36M 40s
 50250K .......... .......... .......... .......... ..........  9% 6.74M 40s
 50300K .......... .......... .......... .......... ..........  9% 5.93M 40s
 50350K .......... .......... .......... .......... ..........  9% 4.07M 40s
 50400K .......... .......... .......... .......... ..........  9% 4.60M 40s
 50450K .......... .......... .......... .......... ..........  9% 3.36M 40s
 50500K .......... .......... .......... .......... ..........  9% 8.03M 40s
 50550K .......... .......... .......... .......... ..........  9% 8.83M 40s
 50600K .......... .......... .......... .......... ..........  9% 5.08M 40s
 50650K .......... .......... .......... .......... ..........  9% 5.99M 40s
 50700K .......... .......... .......... .......... ..........  9% 7.83M 40s
 50750K .......... .......... .......... .......... ..........  9% 23.1M 40s
 50800K .......... .......... .......... .......... .......... 10% 14.5M 40s
 50850K .......... .......... .......... .......... .......... 10% 14.3M 40s
 50900K .......... .......... .......... .......... .......... 10% 15.3M 40s
 50950K .......... .......... .......... .......... .......... 10% 10.9M 40s
 51000K .......... .......... .......... .......... .......... 10% 16.2M 40s
 51050K .......... .......... .......... .......... .......... 10% 15.8M 40s
 51100K .......... .......... .......... .......... .......... 10% 12.6M 40s
 51150K .......... .......... .......... .......... .......... 10% 17.2M 40s
 51200K .......... .......... .......... .......... .......... 10% 14.2M 40s
 51250K .......... .......... .......... .......... .......... 10% 15.8M 40s
 51300K .......... .......... .......... .......... .......... 10% 11.8M 40s
 51350K .......... .......... .......... .......... .......... 10% 15.8M 40s
 51400K .......... .......... .......... .......... .......... 10% 16.5M 40s
 51450K .......... .......... .......... .......... .......... 10% 11.3M 40s
 51500K .......... .......... .......... .......... .......... 10% 14.6M 40s
 51550K .......... .......... .......... .......... .......... 10% 14.6M 40s
 51600K .......... .......... .......... .......... .......... 10% 9.94M 40s
 51650K .......... .......... .......... .......... .......... 10% 12.5M 40s
 51700K .......... .......... .......... .......... .......... 10% 9.94M 40s
 51750K .......... .......... .......... .......... .......... 10% 10.1M 40s
 51800K .......... .......... .......... .......... .......... 10% 15.0M 40s
 51850K .......... .......... .......... .......... .......... 10% 8.87M 40s
 51900K .......... .......... .......... .......... .......... 10% 10.8M 40s
 51950K .......... .......... .......... .......... .......... 10% 4.71M 40s
 52000K .......... .......... .......... .......... .......... 10% 6.35M 40s
 52050K .......... .......... .......... .......... .......... 10% 6.71M 40s
 52100K .......... .......... .......... .......... .......... 10% 5.75M 40s
 52150K .......... .......... .......... .......... .......... 10% 4.99M 40s
 52200K .......... .......... .......... .......... .......... 10% 9.58M 40s
 52250K .......... .......... .......... .......... .......... 10% 16.8M 40s
 52300K .......... .......... .......... .......... .......... 10% 21.8M 40s
 52350K .......... .......... .......... .......... .......... 10% 10.7M 40s
 52400K .......... .......... .......... .......... .......... 10% 14.3M 40s
 52450K .......... .......... .......... .......... .......... 10% 11.1M 40s
 52500K .......... .......... .......... .......... .......... 10% 13.0M 40s
 52550K .......... .......... .......... .......... .......... 10% 14.6M 40s
 52600K .......... .......... .......... .......... .......... 10% 11.4M 40s
 52650K .......... .......... .......... .......... .......... 10% 14.8M 40s
 52700K .......... .......... .......... .......... .......... 10% 11.2M 40s
 52750K .......... .......... .......... .......... .......... 10% 12.2M 40s
 52800K .......... .......... .......... .......... .......... 10% 16.9M 40s
 52850K .......... .......... .......... .......... .......... 10% 8.10M 40s
 52900K .......... .......... .......... .......... .......... 10% 6.47M 40s
 52950K .......... .......... .......... .......... .......... 10% 4.80M 40s
 53000K .......... .......... .......... .......... .......... 10% 4.04M 40s
 53050K .......... .......... .......... .......... .......... 10% 6.55M 40s
 53100K .......... .......... .......... .......... .......... 10% 11.6M 40s
 53150K .......... .......... .......... .......... .......... 10% 11.8M 40s
 53200K .......... .......... .......... .......... .......... 10% 9.46M 40s
 53250K .......... .......... .......... .......... .......... 10% 10.0M 40s
 53300K .......... .......... .......... .......... .......... 10% 16.5M 40s
 53350K .......... .......... .......... .......... .......... 10% 8.93M 40s
 53400K .......... .......... .......... .......... .......... 10% 11.4M 40s
 53450K .......... .......... .......... .......... .......... 10% 9.06M 40s
 53500K .......... .......... .......... .......... .......... 10% 11.6M 40s
 53550K .......... .......... .......... .......... .......... 10% 11.6M 40s
 53600K .......... .......... .......... .......... .......... 10% 7.93M 40s
 53650K .......... .......... .......... .......... .......... 10% 9.77M 40s
 53700K .......... .......... .......... .......... .......... 10% 17.2M 40s
 53750K .......... .......... .......... .......... .......... 10% 45.3M 40s
 53800K .......... .......... .......... .......... .......... 10% 37.9M 40s
 53850K .......... .......... .......... .......... .......... 10% 45.5M 40s
 53900K .......... .......... .......... .......... .......... 10% 26.8M 40s
 53950K .......... .......... .......... .......... .......... 10% 66.8M 40s
 54000K .......... .......... .......... .......... .......... 10% 17.3M 40s
 54050K .......... .......... .......... .......... .......... 10%  109M 40s
 54100K .......... .......... .......... .......... .......... 10% 16.1M 40s
 54150K .......... .......... .......... .......... .......... 10% 14.6M 40s
 54200K .......... .......... .......... .......... .......... 10% 13.4M 40s
 54250K .......... .......... .......... .......... .......... 10% 9.27M 40s
 54300K .......... .......... .......... .......... .......... 10% 10.2M 40s
 54350K .......... .......... .......... .......... .......... 10% 7.80M 40s
 54400K .......... .......... .......... .......... .......... 10% 8.91M 40s
 54450K .......... .......... .......... .......... .......... 10% 7.74M 40s
 54500K .......... .......... .......... .......... .......... 10% 6.43M 40s
 54550K .......... .......... .......... .......... .......... 10% 7.37M 40s
 54600K .......... .......... .......... .......... .......... 10% 4.56M 40s
 54650K .......... .......... .......... .......... .......... 10% 6.30M 40s
 54700K .......... .......... .......... .......... .......... 10% 5.08M 40s
 54750K .......... .......... .......... .......... .......... 10% 4.43M 40s
 54800K .......... .......... .......... .......... .......... 10% 9.00M 40s
 54850K .......... .......... .......... .......... .......... 10% 9.39M 40s
 54900K .......... .......... .......... .......... .......... 10% 10.5M 40s
 54950K .......... .......... .......... .......... .......... 10% 11.2M 40s
 55000K .......... .......... .......... .......... .......... 10% 11.4M 40s
 55050K .......... .......... .......... .......... .......... 10% 12.4M 40s
 55100K .......... .......... .......... .......... .......... 10% 11.9M 40s
 55150K .......... .......... .......... .......... .......... 10% 12.3M 40s
 55200K .......... .......... .......... .......... .......... 10% 17.3M 40s
 55250K .......... .......... .......... .......... .......... 10% 19.6M 40s
 55300K .......... .......... .......... .......... .......... 10% 34.4M 40s
 55350K .......... .......... .......... .......... .......... 10% 20.8M 40s
 55400K .......... .......... .......... .......... .......... 10% 15.8M 40s
 55450K .......... .......... .......... .......... .......... 10% 17.0M 40s
 55500K .......... .......... .......... .......... .......... 10% 15.5M 40s
 55550K .......... .......... .......... .......... .......... 10% 14.9M 40s
 55600K .......... .......... .......... .......... .......... 10% 15.5M 40s
 55650K .......... .......... .......... .......... .......... 10% 11.2M 40s
 55700K .......... .......... .......... .......... .......... 10% 14.5M 40s
 55750K .......... .......... .......... .......... .......... 10% 12.8M 40s
 55800K .......... .......... .......... .......... .......... 10% 10.5M 40s
 55850K .......... .......... .......... .......... .......... 10% 8.68M 40s
 55900K .......... .......... .......... .......... .......... 11% 12.4M 40s
 55950K .......... .......... .......... .......... .......... 11% 8.77M 40s
 56000K .......... .......... .......... .......... .......... 11% 9.82M 40s
 56050K .......... .......... .......... .......... .......... 11% 12.1M 40s
 56100K .......... .......... .......... .......... .......... 11% 12.0M 40s
 56150K .......... .......... .......... .......... .......... 11% 11.6M 40s
 56200K .......... .......... .......... .......... .......... 11% 9.46M 40s
 56250K .......... .......... .......... .......... .......... 11% 9.84M 40s
 56300K .......... .......... .......... .......... .......... 11% 12.3M 40s
 56350K .......... .......... .......... .......... .......... 11% 8.79M 40s
 56400K .......... .......... .......... .......... .......... 11% 15.3M 40s
 56450K .......... .......... .......... .......... .......... 11% 10.3M 40s
 56500K .......... .......... .......... .......... .......... 11% 10.2M 40s
 56550K .......... .......... .......... .......... .......... 11% 12.4M 40s
 56600K .......... .......... .......... .......... .......... 11% 11.4M 40s
 56650K .......... .......... .......... .......... .......... 11% 15.2M 40s
 56700K .......... .......... .......... .......... .......... 11% 11.4M 40s
 56750K .......... .......... .......... .......... .......... 11% 11.6M 40s
 56800K .......... .......... .......... .......... .......... 11% 15.6M 40s
 56850K .......... .......... .......... .......... .......... 11% 11.6M 40s
 56900K .......... .......... .......... .......... .......... 11% 17.1M 40s
 56950K .......... .......... .......... .......... .......... 11% 9.97M 40s
 57000K .......... .......... .......... .......... .......... 11% 26.0M 40s
 57050K .......... .......... .......... .......... .......... 11% 29.6M 40s
 57100K .......... .......... .......... .......... .......... 11% 22.1M 40s
 57150K .......... .......... .......... .......... .......... 11% 39.3M 40s
 57200K .......... .......... .......... .......... .......... 11% 36.2M 40s
 57250K .......... .......... .......... .......... .......... 11% 25.9M 40s
 57300K .......... .......... .......... .......... .......... 11% 19.4M 40s
 57350K .......... .......... .......... .......... .......... 11% 23.7M 40s
 57400K .......... .......... .......... .......... .......... 11% 25.2M 40s
 57450K .......... .......... .......... .......... .......... 11% 20.6M 40s
 57500K .......... .......... .......... .......... .......... 11% 28.0M 40s
 57550K .......... .......... .......... .......... .......... 11% 26.1M 40s
 57600K .......... .......... .......... .......... .......... 11% 23.6M 40s
 57650K .......... .......... .......... .......... .......... 11% 24.7M 40s
 57700K .......... .......... .......... .......... .......... 11% 21.8M 40s
 57750K .......... .......... .......... .......... .......... 11% 21.0M 40s
 57800K .......... .......... .......... .......... .......... 11% 30.3M 40s
 57850K .......... .......... .......... .......... .......... 11% 22.0M 40s
 57900K .......... .......... .......... .......... .......... 11% 17.6M 40s
 57950K .......... .......... .......... .......... .......... 11% 24.2M 40s
 58000K .......... .......... .......... .......... .......... 11% 15.7M 40s
 58050K .......... .......... .......... .......... .......... 11% 22.9M 39s
 58100K .......... .......... .......... .......... .......... 11% 19.2M 39s
 58150K .......... .......... .......... .......... .......... 11% 16.6M 39s
 58200K .......... .......... .......... .......... .......... 11% 21.4M 39s
 58250K .......... .......... .......... .......... .......... 11% 15.8M 39s
 58300K .......... .......... .......... .......... .......... 11% 22.4M 39s
 58350K .......... .......... .......... .......... .......... 11% 16.8M 39s
 58400K .......... .......... .......... .......... .......... 11% 16.6M 39s
 58450K .......... .......... .......... .......... .......... 11% 17.0M 39s
 58500K .......... .......... .......... .......... .......... 11% 15.0M 39s
 58550K .......... .......... .......... .......... .......... 11% 19.2M 39s
 58600K .......... .......... .......... .......... .......... 11% 17.4M 39s
 58650K .......... .......... .......... .......... .......... 11% 17.1M 39s
 58700K .......... .......... .......... .......... .......... 11% 15.9M 39s
 58750K .......... .......... .......... .......... .......... 11% 16.2M 39s
 58800K .......... .......... .......... .......... .......... 11% 18.5M 39s
 58850K .......... .......... .......... .......... .......... 11% 15.6M 39s
 58900K .......... .......... .......... .......... .......... 11% 15.3M 39s
 58950K .......... .......... .......... .......... .......... 11% 14.5M 39s
 59000K .......... .......... .......... .......... .......... 11% 29.6M 39s
 59050K .......... .......... .......... .......... .......... 11% 14.2M 39s
 59100K .......... .......... .......... .......... .......... 11% 25.1M 39s
 59150K .......... .......... .......... .......... .......... 11% 36.0M 39s
 59200K .......... .......... .......... .......... .......... 11% 13.4M 39s
 59250K .......... .......... .......... .......... .......... 11% 18.4M 39s
 59300K .......... .......... .......... .......... .......... 11% 22.5M 39s
 59350K .......... .......... .......... .......... .......... 11% 16.2M 39s
 59400K .......... .......... .......... .......... .......... 11% 17.0M 39s
 59450K .......... .......... .......... .......... .......... 11% 20.5M 39s
 59500K .......... .......... .......... .......... .......... 11% 17.6M 39s
 59550K .......... .......... .......... .......... .......... 11% 11.0M 39s
 59600K .......... .......... .......... .......... .......... 11% 12.0M 39s
 59650K .......... .......... .......... .......... .......... 11% 12.4M 39s
 59700K .......... .......... .......... .......... .......... 11% 10.2M 39s
 59750K .......... .......... .......... .......... .......... 11% 11.4M 39s
 59800K .......... .......... .......... .......... .......... 11% 12.2M 39s
 59850K .......... .......... .......... .......... .......... 11% 8.05M 39s
 59900K .......... .......... .......... .......... .......... 11% 9.04M 39s
 59950K .......... .......... .......... .......... .......... 11% 9.44M 39s
 60000K .......... .......... .......... .......... .......... 11% 7.23M 39s
 60050K .......... .......... .......... .......... .......... 11% 6.64M 39s
 60100K .......... .......... .......... .......... .......... 11% 5.31M 39s
 60150K .......... .......... .......... .......... .......... 11% 5.36M 39s
 60200K .......... .......... .......... .......... .......... 11% 5.45M 39s
 60250K .......... .......... .......... .......... .......... 11% 5.43M 39s
 60300K .......... .......... .......... .......... .......... 11% 5.43M 39s
 60350K .......... .......... .......... .......... .......... 11% 9.68M 39s
 60400K .......... .......... .......... .......... .......... 11% 35.4M 39s
 60450K .......... .......... .......... .......... .......... 11% 22.9M 39s
 60500K .......... .......... .......... .......... .......... 11% 12.8M 39s
 60550K .......... .......... .......... .......... .......... 11% 11.1M 39s
 60600K .......... .......... .......... .......... .......... 11% 12.2M 39s
 60650K .......... .......... .......... .......... .......... 11% 16.7M 39s
 60700K .......... .......... .......... .......... .......... 11% 11.8M 39s
 60750K .......... .......... .......... .......... .......... 11% 16.4M 39s
 60800K .......... .......... .......... .......... .......... 11% 12.7M 39s
 60850K .......... .......... .......... .......... .......... 11% 10.0M 39s
 60900K .......... .......... .......... .......... .......... 11% 12.2M 39s
 60950K .......... .......... .......... .......... .......... 11% 9.66M 39s
 61000K .......... .......... .......... .......... .......... 12% 9.69M 39s
 61050K .......... .......... .......... .......... .......... 12% 9.20M 39s
 61100K .......... .......... .......... .......... .......... 12% 5.93M 39s
 61150K .......... .......... .......... .......... .......... 12% 7.27M 39s
 61200K .......... .......... .......... .......... .......... 12% 5.80M 39s
 61250K .......... .......... .......... .......... .......... 12% 7.68M 39s
 61300K .......... .......... .......... .......... .......... 12% 5.44M 39s
 61350K .......... .......... .......... .......... .......... 12% 3.53M 39s
 61400K .......... .......... .......... .......... .......... 12% 3.12M 39s
 61450K .......... .......... .......... .......... .......... 12% 2.42M 39s
 61500K .......... .......... .......... .......... .......... 12% 7.01M 39s
 61550K .......... .......... .......... .......... .......... 12% 12.0M 39s
 61600K .......... .......... .......... .......... .......... 12% 11.5M 39s
 61650K .......... .......... .......... .......... .......... 12% 12.0M 39s
 61700K .......... .......... .......... .......... .......... 12% 7.59M 39s
 61750K .......... .......... .......... .......... .......... 12% 9.94M 39s
 61800K .......... .......... .......... .......... .......... 12% 10.6M 39s
 61850K .......... .......... .......... .......... .......... 12% 7.89M 39s
 61900K .......... .......... .......... .......... .......... 12% 10.2M 39s
 61950K .......... .......... .......... .......... .......... 12% 16.2M 39s
 62000K .......... .......... .......... .......... .......... 12% 25.7M 39s
 62050K .......... .......... .......... .......... .......... 12% 18.7M 39s
 62100K .......... .......... .......... .......... .......... 12% 15.1M 39s
 62150K .......... .......... .......... .......... .......... 12% 10.0M 39s
 62200K .......... .......... .......... .......... .......... 12% 8.27M 39s
 62250K .......... .......... .......... .......... .......... 12% 10.1M 39s
 62300K .......... .......... .......... .......... .......... 12% 5.64M 39s
 62350K .......... .......... .......... .......... .......... 12% 5.80M 39s
 62400K .......... .......... .......... .......... .......... 12% 6.10M 39s
 62450K .......... .......... .......... .......... .......... 12% 5.72M 39s
 62500K .......... .......... .......... .......... .......... 12% 8.53M 39s
 62550K .......... .......... .......... .......... .......... 12% 8.34M 39s
 62600K .......... .......... .......... .......... .......... 12% 35.4M 39s
 62650K .......... .......... .......... .......... .......... 12% 16.4M 39s
 62700K .......... .......... .......... .......... .......... 12% 13.6M 39s
 62750K .......... .......... .......... .......... .......... 12% 30.3M 39s
 62800K .......... .......... .......... .......... .......... 12% 13.8M 39s
 62850K .......... .......... .......... .......... .......... 12% 12.4M 39s
 62900K .......... .......... .......... .......... .......... 12% 16.0M 39s
 62950K .......... .......... .......... .......... .......... 12% 8.97M 39s
 63000K .......... .......... .......... .......... .......... 12% 6.47M 39s
 63050K .......... .......... .......... .......... .......... 12% 6.23M 39s
 63100K .......... .......... .......... .......... .......... 12% 5.10M 39s
 63150K .......... .......... .......... .......... .......... 12% 3.45M 39s
 63200K .......... .......... .......... .......... .......... 12% 3.40M 40s
 63250K .......... .......... .......... .......... .......... 12% 5.83M 40s
 63300K .......... .......... .......... .......... .......... 12% 21.4M 40s
 63350K .......... .......... .......... .......... .......... 12% 24.6M 40s
 63400K .......... .......... .......... .......... .......... 12% 50.8M 40s
 63450K .......... .......... .......... .......... .......... 12% 31.1M 39s
 63500K .......... .......... .......... .......... .......... 12% 54.7M 39s
 63550K .......... .......... .......... .......... .......... 12% 44.9M 39s
 63600K .......... .......... .......... .......... .......... 12% 27.9M 39s
 63650K .......... .......... .......... .......... .......... 12% 28.7M 39s
 63700K .......... .......... .......... .......... .......... 12% 28.5M 39s
 63750K .......... .......... .......... .......... .......... 12% 23.8M 39s
 63800K .......... .......... .......... .......... .......... 12% 22.7M 39s
 63850K .......... .......... .......... .......... .......... 12% 17.9M 39s
 63900K .......... .......... .......... .......... .......... 12% 20.6M 39s
 63950K .......... .......... .......... .......... .......... 12% 15.0M 39s
 64000K .......... .......... .......... .......... .......... 12% 12.8M 39s
 64050K .......... .......... .......... .......... .......... 12% 19.7M 39s
 64100K .......... .......... .......... .......... .......... 12% 12.9M 39s
 64150K .......... .......... .......... .......... .......... 12% 16.7M 39s
 64200K .......... .......... .......... .......... .......... 12% 13.8M 39s
 64250K .......... .......... .......... .......... .......... 12% 11.3M 39s
 64300K .......... .......... .......... .......... .......... 12% 10.1M 39s
 64350K .......... .......... .......... .......... .......... 12% 9.89M 39s
 64400K .......... .......... .......... .......... .......... 12% 11.3M 39s
 64450K .......... .......... .......... .......... .......... 12% 9.95M 39s
 64500K .......... .......... .......... .......... .......... 12% 8.58M 39s
 64550K .......... .......... .......... .......... .......... 12% 8.03M 39s
 64600K .......... .......... .......... .......... .......... 12% 7.17M 39s
 64650K .......... .......... .......... .......... .......... 12% 13.8M 39s
 64700K .......... .......... .......... .......... .......... 12% 11.3M 39s
 64750K .......... .......... .......... .......... .......... 12% 14.7M 39s
 64800K .......... .......... .......... .......... .......... 12% 15.8M 39s
 64850K .......... .......... .......... .......... .......... 12% 10.9M 39s
 64900K .......... .......... .......... .......... .......... 12% 11.6M 39s
 64950K .......... .......... .......... .......... .......... 12% 8.70M 39s
 65000K .......... .......... .......... .......... .......... 12% 10.9M 39s
 65050K .......... .......... .......... .......... .......... 12% 11.4M 39s
 65100K .......... .......... .......... .......... .......... 12% 8.94M 39s
 65150K .......... .......... .......... .......... .......... 12% 12.4M 39s
 65200K .......... .......... .......... .......... .......... 12% 7.28M 39s
 65250K .......... .......... .......... .......... .......... 12% 11.7M 39s
 65300K .......... .......... .......... .......... .......... 12% 10.3M 39s
 65350K .......... .......... .......... .......... .......... 12% 11.2M 39s
 65400K .......... .......... .......... .......... .......... 12% 10.7M 39s
 65450K .......... .......... .......... .......... .......... 12% 10.0M 39s
 65500K .......... .......... .......... .......... .......... 12% 10.1M 39s
 65550K .......... .......... .......... .......... .......... 12% 9.17M 39s
 65600K .......... .......... .......... .......... .......... 12% 10.4M 39s
 65650K .......... .......... .......... .......... .......... 12% 14.5M 39s
 65700K .......... .......... .......... .......... .......... 12% 9.89M 39s
 65750K .......... .......... .......... .......... .......... 12% 15.0M 39s
 65800K .......... .......... .......... .......... .......... 12% 9.36M 39s
 65850K .......... .......... .......... .......... .......... 12% 12.6M 39s
 65900K .......... .......... .......... .......... .......... 12% 10.6M 39s
 65950K .......... .......... .......... .......... .......... 12% 8.23M 39s
 66000K .......... .......... .......... .......... .......... 12% 8.70M 39s
 66050K .......... .......... .......... .......... .......... 13% 9.37M 39s
 66100K .......... .......... .......... .......... .......... 13% 7.29M 39s
 66150K .......... .......... .......... .......... .......... 13% 9.14M 39s
 66200K .......... .......... .......... .......... .......... 13% 5.97M 39s
 66250K .......... .......... .......... .......... .......... 13% 8.29M 39s
 66300K .......... .......... .......... .......... .......... 13% 7.77M 39s
 66350K .......... .......... .......... .......... .......... 13% 6.86M 39s
 66400K .......... .......... .......... .......... .......... 13% 9.05M 39s
 66450K .......... .......... .......... .......... .......... 13% 8.35M 39s
 66500K .......... .......... .......... .......... .......... 13% 9.99M 39s
 66550K .......... .......... .......... .......... .......... 13% 8.01M 39s
 66600K .......... .......... .......... .......... .......... 13% 5.45M 39s
 66650K .......... .......... .......... .......... .......... 13% 9.77M 39s
 66700K .......... .......... .......... .......... .......... 13% 9.57M 39s
 66750K .......... .......... .......... .......... .......... 13% 10.1M 39s
 66800K .......... .......... .......... .......... .......... 13% 12.8M 39s
 66850K .......... .......... .......... .......... .......... 13% 10.0M 39s
 66900K .......... .......... .......... .......... .......... 13% 11.0M 39s
 66950K .......... .......... .......... .......... .......... 13% 7.66M 39s
 67000K .......... .......... .......... .......... .......... 13% 8.10M 39s
 67050K .......... .......... .......... .......... .......... 13% 6.11M 39s
 67100K .......... .......... .......... .......... .......... 13% 5.05M 39s
 67150K .......... .......... .......... .......... .......... 13% 5.25M 39s
 67200K .......... .......... .......... .......... .......... 13% 9.40M 39s
 67250K .......... .......... .......... .......... .......... 13% 9.79M 39s
 67300K .......... .......... .......... .......... .......... 13% 11.0M 39s
 67350K .......... .......... .......... .......... .......... 13% 8.26M 39s
 67400K .......... .......... .......... .......... .......... 13% 9.27M 39s
 67450K .......... .......... .......... .......... .......... 13% 9.75M 39s
 67500K .......... .......... .......... .......... .......... 13% 9.54M 39s
 67550K .......... .......... .......... .......... .......... 13% 8.14M 39s
 67600K .......... .......... .......... .......... .......... 13% 8.67M 39s
 67650K .......... .......... .......... .......... .......... 13% 10.2M 39s
 67700K .......... .......... .......... .......... .......... 13% 6.28M 39s
 67750K .......... .......... .......... .......... .......... 13% 7.26M 39s
 67800K .......... .......... .......... .......... .......... 13% 7.29M 39s
 67850K .......... .......... .......... .......... .......... 13% 5.85M 39s
 67900K .......... .......... .......... .......... .......... 13% 7.01M 39s
 67950K .......... .......... .......... .......... .......... 13% 5.86M 39s
 68000K .......... .......... .......... .......... .......... 13% 10.1M 39s
 68050K .......... .......... .......... .......... .......... 13% 40.2M 39s
 68100K .......... .......... .......... .......... .......... 13% 19.4M 39s
 68150K .......... .......... .......... .......... .......... 13% 21.2M 39s
 68200K .......... .......... .......... .......... .......... 13% 24.0M 39s
 68250K .......... .......... .......... .......... .......... 13% 15.6M 39s
 68300K .......... .......... .......... .......... .......... 13% 9.77M 39s
 68350K .......... .......... .......... .......... .......... 13% 10.6M 39s
 68400K .......... .......... .......... .......... .......... 13% 11.5M 39s
 68450K .......... .......... .......... .......... .......... 13% 9.24M 39s
 68500K .......... .......... .......... .......... .......... 13% 9.63M 39s
 68550K .......... .......... .......... .......... .......... 13% 11.9M 39s
 68600K .......... .......... .......... .......... .......... 13% 9.17M 39s
 68650K .......... .......... .......... .......... .......... 13% 10.5M 39s
 68700K .......... .......... .......... .......... .......... 13% 5.80M 39s
 68750K .......... .......... .......... .......... .......... 13% 8.75M 39s
 68800K .......... .......... .......... .......... .......... 13% 8.84M 39s
 68850K .......... .......... .......... .......... .......... 13% 6.57M 39s
 68900K .......... .......... .......... .......... .......... 13% 8.81M 39s
 68950K .......... .......... .......... .......... .......... 13% 4.75M 39s
 69000K .......... .......... .......... .......... .......... 13% 5.84M 39s
 69050K .......... .......... .......... .......... .......... 13% 4.91M 39s
 69100K .......... .......... .......... .......... .......... 13% 4.91M 39s
 69150K .......... .......... .......... .......... .......... 13% 5.15M 39s
 69200K .......... .......... .......... .......... .......... 13% 5.13M 39s
 69250K .......... .......... .......... .......... .......... 13% 10.0M 39s
 69300K .......... .......... .......... .......... .......... 13% 8.05M 39s
 69350K .......... .......... .......... .......... .......... 13% 6.55M 40s
 69400K .......... .......... .......... .......... .......... 13% 7.48M 40s
 69450K .......... .......... .......... .......... .......... 13% 6.50M 40s
 69500K .......... .......... .......... .......... .......... 13% 6.50M 40s
 69550K .......... .......... .......... .......... .......... 13% 7.48M 40s
 69600K .......... .......... .......... .......... .......... 13% 9.66M 40s
 69650K .......... .......... .......... .......... .......... 13% 10.6M 40s
 69700K .......... .......... .......... .......... .......... 13% 9.54M 40s
 69750K .......... .......... .......... .......... .......... 13% 12.1M 40s
 69800K .......... .......... .......... .......... .......... 13% 7.77M 40s
 69850K .......... .......... .......... .......... .......... 13% 7.79M 40s
 69900K .......... .......... .......... .......... .......... 13% 6.59M 40s
 69950K .......... .......... .......... .......... .......... 13% 7.39M 40s
 70000K .......... .......... .......... .......... .......... 13% 8.81M 40s
 70050K .......... .......... .......... .......... .......... 13% 6.06M 40s
 70100K .......... .......... .......... .......... .......... 13% 5.73M 40s
 70150K .......... .......... .......... .......... .......... 13% 5.40M 40s
 70200K .......... .......... .......... .......... .......... 13% 7.89M 40s
 70250K .......... .......... .......... .......... .......... 13% 11.2M 40s
 70300K .......... .......... .......... .......... .......... 13% 10.3M 40s
 70350K .......... .......... .......... .......... .......... 13% 11.5M 40s
 70400K .......... .......... .......... .......... .......... 13% 12.9M 40s
 70450K .......... .......... .......... .......... .......... 13% 11.1M 40s
 70500K .......... .......... .......... .......... .......... 13% 12.5M 40s
 70550K .......... .......... .......... .......... .......... 13% 8.13M 40s
 70600K .......... .......... .......... .......... .......... 13% 6.16M 40s
 70650K .......... .......... .......... .......... .......... 13% 10.6M 40s
 70700K .......... .......... .......... .......... .......... 13% 8.77M 40s
 70750K .......... .......... .......... .......... .......... 13% 9.79M 40s
 70800K .......... .......... .......... .......... .......... 13% 10.1M 40s
 70850K .......... .......... .......... .......... .......... 13% 11.5M 40s
 70900K .......... .......... .......... .......... .......... 13% 11.2M 40s
 70950K .......... .......... .......... .......... .......... 13% 10.2M 40s
 71000K .......... .......... .......... .......... .......... 13% 12.5M 40s
 71050K .......... .......... .......... .......... .......... 13% 14.4M 40s
 71100K .......... .......... .......... .......... .......... 13% 8.90M 40s
 71150K .......... .......... .......... .......... .......... 14% 12.9M 40s
 71200K .......... .......... .......... .......... .......... 14% 8.07M 40s
 71250K .......... .......... .......... .......... .......... 14% 20.7M 40s
 71300K .......... .......... .......... .......... .......... 14% 48.2M 40s
 71350K .......... .......... .......... .......... .......... 14% 19.7M 40s
 71400K .......... .......... .......... .......... .......... 14% 27.9M 40s
 71450K .......... .......... .......... .......... .......... 14% 21.7M 39s
 71500K .......... .......... .......... .......... .......... 14% 13.6M 39s
 71550K .......... .......... .......... .......... .......... 14% 14.0M 39s
 71600K .......... .......... .......... .......... .......... 14% 11.9M 39s
 71650K .......... .......... .......... .......... .......... 14% 12.2M 39s
 71700K .......... .......... .......... .......... .......... 14% 11.9M 39s
 71750K .......... .......... .......... .......... .......... 14% 11.3M 39s
 71800K .......... .......... .......... .......... .......... 14% 12.9M 39s
 71850K .......... .......... .......... .......... .......... 14% 11.1M 39s
 71900K .......... .......... .......... .......... .......... 14% 13.0M 39s
 71950K .......... .......... .......... .......... .......... 14% 10.7M 39s
 72000K .......... .......... .......... .......... .......... 14% 9.50M 39s
 72050K .......... .......... .......... .......... .......... 14% 12.2M 39s
 72100K .......... .......... .......... .......... .......... 14% 8.20M 39s
 72150K .......... .......... .......... .......... .......... 14% 9.34M 39s
 72200K .......... .......... .......... .......... .......... 14% 6.01M 39s
 72250K .......... .......... .......... .......... .......... 14% 6.81M 39s
 72300K .......... .......... .......... .......... .......... 14% 6.38M 39s
 72350K .......... .......... .......... .......... .......... 14% 4.83M 39s
 72400K .......... .......... .......... .......... .......... 14% 9.05M 39s
 72450K .......... .......... .......... .......... .......... 14% 9.34M 39s
 72500K .......... .......... .......... .......... .......... 14% 9.11M 39s
 72550K .......... .......... .......... .......... .......... 14% 9.54M 39s
 72600K .......... .......... .......... .......... .......... 14% 11.1M 39s
 72650K .......... .......... .......... .......... .......... 14% 11.8M 39s
 72700K .......... .......... .......... .......... .......... 14% 10.8M 39s
 72750K .......... .......... .......... .......... .......... 14% 14.2M 39s
 72800K .......... .......... .......... .......... .......... 14% 23.8M 39s
 72850K .......... .......... .......... .......... .......... 14% 49.6M 39s
 72900K .......... .......... .......... .......... .......... 14% 25.1M 39s
 72950K .......... .......... .......... .......... .......... 14% 74.8M 39s
 73000K .......... .......... .......... .......... .......... 14% 26.3M 39s
 73050K .......... .......... .......... .......... .......... 14% 38.7M 39s
 73100K .......... .......... .......... .......... .......... 14% 22.4M 39s
 73150K .......... .......... .......... .......... .......... 14% 39.3M 39s
 73200K .......... .......... .......... .......... .......... 14% 14.5M 39s
 73250K .......... .......... .......... .......... .......... 14% 42.2M 39s
 73300K .......... .......... .......... .......... .......... 14% 22.4M 39s
 73350K .......... .......... .......... .......... .......... 14% 15.1M 39s
 73400K .......... .......... .......... .......... .......... 14% 15.2M 39s
 73450K .......... .......... .......... .......... .......... 14% 15.0M 39s
 73500K .......... .......... .......... .......... .......... 14% 20.7M 39s
 73550K .......... .......... .......... .......... .......... 14% 12.5M 39s
 73600K .......... .......... .......... .......... .......... 14% 16.1M 39s
 73650K .......... .......... .......... .......... .......... 14% 15.1M 39s
 73700K .......... .......... .......... .......... .......... 14% 13.9M 39s
 73750K .......... .......... .......... .......... .......... 14% 13.6M 39s
 73800K .......... .......... .......... .......... .......... 14% 11.1M 39s
 73850K .......... .......... .......... .......... .......... 14% 9.66M 39s
 73900K .......... .......... .......... .......... .......... 14% 9.21M 39s
 73950K .......... .......... .......... .......... .......... 14% 11.6M 39s
 74000K .......... .......... .......... .......... .......... 14% 9.33M 39s
 74050K .......... .......... .......... .......... .......... 14% 7.54M 39s
 74100K .......... .......... .......... .......... .......... 14% 6.78M 39s
 74150K .......... .......... .......... .......... .......... 14% 6.88M 39s
 74200K .......... .......... .......... .......... .......... 14% 8.19M 39s
 74250K .......... .......... .......... .......... .......... 14% 9.78M 39s
 74300K .......... .......... .......... .......... .......... 14% 8.70M 39s
 74350K .......... .......... .......... .......... .......... 14% 8.82M 39s
 74400K .......... .......... .......... .......... .......... 14% 8.86M 39s
 74450K .......... .......... .......... .......... .......... 14% 8.67M 39s
 74500K .......... .......... .......... .......... .......... 14% 9.45M 39s
 74550K .......... .......... .......... .......... .......... 14% 32.1M 39s
 74600K .......... .......... .......... .......... .......... 14% 23.7M 39s
 74650K .......... .......... .......... .......... .......... 14% 42.8M 39s
 74700K .......... .......... .......... .......... .......... 14% 26.3M 39s
 74750K .......... .......... .......... .......... .......... 14% 32.2M 39s
 74800K .......... .......... .......... .......... .......... 14% 26.9M 39s
 74850K .......... .......... .......... .......... .......... 14% 17.2M 39s
 74900K .......... .......... .......... .......... .......... 14% 31.6M 39s
 74950K .......... .......... .......... .......... .......... 14% 15.6M 39s
 75000K .......... .......... .......... .......... .......... 14% 15.3M 39s
 75050K .......... .......... .......... .......... .......... 14% 13.8M 39s
 75100K .......... .......... .......... .......... .......... 14% 11.2M 39s
 75150K .......... .......... .......... .......... .......... 14% 12.3M 39s
 75200K .......... .......... .......... .......... .......... 14% 11.4M 39s
 75250K .......... .......... .......... .......... .......... 14% 12.2M 39s
 75300K .......... .......... .......... .......... .......... 14% 12.6M 39s
 75350K .......... .......... .......... .......... .......... 14% 10.7M 39s
 75400K .......... .......... .......... .......... .......... 14% 9.43M 39s
 75450K .......... .......... .......... .......... .......... 14% 9.65M 39s
 75500K .......... .......... .......... .......... .......... 14% 20.5M 39s
 75550K .......... .......... .......... .......... .......... 14% 21.4M 39s
 75600K .......... .......... .......... .......... .......... 14% 25.7M 39s
 75650K .......... .......... .......... .......... .......... 14% 50.6M 39s
 75700K .......... .......... .......... .......... .......... 14% 20.2M 39s
 75750K .......... .......... .......... .......... .......... 14% 31.3M 39s
 75800K .......... .......... .......... .......... .......... 14% 23.2M 39s
 75850K .......... .......... .......... .......... .......... 14% 12.5M 39s
 75900K .......... .......... .......... .......... .......... 14% 12.2M 39s
 75950K .......... .......... .......... .......... .......... 14% 9.28M 39s
 76000K .......... .......... .......... .......... .......... 14% 12.3M 39s
 76050K .......... .......... .......... .......... .......... 14% 10.3M 39s
 76100K .......... .......... .......... .......... .......... 14% 9.90M 39s
 76150K .......... .......... .......... .......... .......... 14% 11.8M 39s
 76200K .......... .......... .......... .......... .......... 14% 7.07M 39s
 76250K .......... .......... .......... .......... .......... 15% 8.05M 39s
 76300K .......... .......... .......... .......... .......... 15% 6.42M 39s
 76350K .......... .......... .......... .......... .......... 15% 6.15M 39s
 76400K .......... .......... .......... .......... .......... 15% 7.00M 39s
 76450K .......... .......... .......... .......... .......... 15% 6.45M 39s
 76500K .......... .......... .......... .......... .......... 15% 8.97M 39s
 76550K .......... .......... .......... .......... .......... 15% 20.9M 39s
 76600K .......... .......... .......... .......... .......... 15% 27.6M 39s
 76650K .......... .......... .......... .......... .......... 15% 34.3M 39s
 76700K .......... .......... .......... .......... .......... 15% 25.5M 39s
 76750K .......... .......... .......... .......... .......... 15% 32.7M 39s
 76800K .......... .......... .......... .......... .......... 15% 23.9M 39s
 76850K .......... .......... .......... .......... .......... 15% 15.2M 39s
 76900K .......... .......... .......... .......... .......... 15% 18.2M 39s
 76950K .......... .......... .......... .......... .......... 15% 16.0M 39s
 77000K .......... .......... .......... .......... .......... 15% 14.8M 39s
 77050K .......... .......... .......... .......... .......... 15% 16.1M 39s
 77100K .......... .......... .......... .......... .......... 15% 9.91M 39s
 77150K .......... .......... .......... .......... .......... 15% 15.5M 39s
 77200K .......... .......... .......... .......... .......... 15% 11.2M 39s
 77250K .......... .......... .......... .......... .......... 15% 16.5M 39s
 77300K .......... .......... .......... .......... .......... 15% 13.2M 39s
 77350K .......... .......... .......... .......... .......... 15% 9.35M 39s
 77400K .......... .......... .......... .......... .......... 15% 14.7M 39s
 77450K .......... .......... .......... .......... .......... 15% 10.8M 39s
 77500K .......... .......... .......... .......... .......... 15% 9.98M 39s
 77550K .......... .......... .......... .......... .......... 15% 11.4M 39s
 77600K .......... .......... .......... .......... .......... 15% 10.3M 39s
 77650K .......... .......... .......... .......... .......... 15% 11.3M 39s
 77700K .......... .......... .......... .......... .......... 15% 11.6M 39s
 77750K .......... .......... .......... .......... .......... 15% 12.1M 39s
 77800K .......... .......... .......... .......... .......... 15% 19.6M 39s
 77850K .......... .......... .......... .......... .......... 15% 16.6M 39s
 77900K .......... .......... .......... .......... .......... 15%  140M 38s
 77950K .......... .......... .......... .......... .......... 15% 25.1M 38s
 78000K .......... .......... .......... .......... .......... 15% 21.2M 38s
 78050K .......... .......... .......... .......... .......... 15% 22.5M 38s
 78100K .......... .......... .......... .......... .......... 15% 15.7M 38s
 78150K .......... .......... .......... .......... .......... 15% 23.2M 38s
 78200K .......... .......... .......... .......... .......... 15% 16.7M 38s
 78250K .......... .......... .......... .......... .......... 15% 16.1M 38s
 78300K .......... .......... .......... .......... .......... 15% 19.1M 38s
 78350K .......... .......... .......... .......... .......... 15% 12.0M 38s
 78400K .......... .......... .......... .......... .......... 15% 16.2M 38s
 78450K .......... .......... .......... .......... .......... 15% 16.9M 38s
 78500K .......... .......... .......... .......... .......... 15% 14.6M 38s
 78550K .......... .......... .......... .......... .......... 15% 16.0M 38s
 78600K .......... .......... .......... .......... .......... 15% 10.6M 38s
 78650K .......... .......... .......... .......... .......... 15% 15.6M 38s
 78700K .......... .......... .......... .......... .......... 15% 12.4M 38s
 78750K .......... .......... .......... .......... .......... 15% 10.1M 38s
 78800K .......... .......... .......... .......... .......... 15% 11.5M 38s
 78850K .......... .......... .......... .......... .......... 15% 11.4M 38s
 78900K .......... .......... .......... .......... .......... 15% 13.7M 38s
 78950K .......... .......... .......... .......... .......... 15% 12.4M 38s
 79000K .......... .......... .......... .......... .......... 15% 10.3M 38s
 79050K .......... .......... .......... .......... .......... 15% 11.8M 38s
 79100K .......... .......... .......... .......... .......... 15% 8.77M 38s
 79150K .......... .......... .......... .......... .......... 15% 10.7M 38s
 79200K .......... .......... .......... .......... .......... 15% 8.15M 38s
 79250K .......... .......... .......... .......... .......... 15% 8.17M 38s
 79300K .......... .......... .......... .......... .......... 15% 6.12M 38s
 79350K .......... .......... .......... .......... .......... 15% 8.64M 38s
 79400K .......... .......... .......... .......... .......... 15% 7.40M 38s
 79450K .......... .......... .......... .......... .......... 15% 6.20M 38s
 79500K .......... .......... .......... .......... .......... 15% 9.77M 38s
 79550K .......... .......... .......... .......... .......... 15% 10.8M 38s
 79600K .......... .......... .......... .......... .......... 15% 6.51M 38s
 79650K .......... .......... .......... .......... .......... 15% 6.66M 38s
 79700K .......... .......... .......... .......... .......... 15% 5.88M 38s
 79750K .......... .......... .......... .......... .......... 15% 13.0M 38s
 79800K .......... .......... .......... .......... .......... 15% 9.06M 38s
 79850K .......... .......... .......... .......... .......... 15% 8.79M 38s
 79900K .......... .......... .......... .......... .......... 15% 11.0M 38s
 79950K .......... .......... .......... .......... .......... 15% 8.18M 38s
 80000K .......... .......... .......... .......... .......... 15% 14.8M 38s
 80050K .......... .......... .......... .......... .......... 15% 14.3M 38s
 80100K .......... .......... .......... .......... .......... 15% 11.2M 38s
 80150K .......... .......... .......... .......... .......... 15% 12.2M 38s
 80200K .......... .......... .......... .......... .......... 15% 13.4M 38s
 80250K .......... .......... .......... .......... .......... 15% 11.1M 38s
 80300K .......... .......... .......... .......... .......... 15% 10.4M 38s
 80350K .......... .......... .......... .......... .......... 15% 7.52M 38s
 80400K .......... .......... .......... .......... .......... 15% 9.91M 38s
 80450K .......... .......... .......... .......... .......... 15% 9.64M 38s
 80500K .......... .......... .......... .......... .......... 15% 10.0M 38s
 80550K .......... .......... .......... .......... .......... 15% 11.0M 38s
 80600K .......... .......... .......... .......... .......... 15% 7.19M 38s
 80650K .......... .......... .......... .......... .......... 15% 10.8M 38s
 80700K .......... .......... .......... .......... .......... 15% 7.83M 38s
 80750K .......... .......... .......... .......... .......... 15% 8.21M 38s
 80800K .......... .......... .......... .......... .......... 15% 7.12M 38s
 80850K .......... .......... .......... .......... .......... 15% 4.85M 38s
 80900K .......... .......... .......... .......... .......... 15% 5.15M 38s
 80950K .......... .......... .......... .......... .......... 15% 3.84M 38s
 81000K .......... .......... .......... .......... .......... 15% 3.89M 38s
 81050K .......... .......... .......... .......... .......... 15% 4.20M 38s
 81100K .......... .......... .......... .......... .......... 15% 4.57M 38s
 81150K .......... .......... .......... .......... .......... 15% 19.7M 38s
 81200K .......... .......... .......... .......... .......... 15% 11.8M 38s
 81250K .......... .......... .......... .......... .......... 15% 12.4M 38s
 81300K .......... .......... .......... .......... .......... 16% 12.5M 38s
 81350K .......... .......... .......... .......... .......... 16% 9.71M 38s
 81400K .......... .......... .......... .......... .......... 16% 14.1M 38s
 81450K .......... .......... .......... .......... .......... 16% 9.31M 38s
 81500K .......... .......... .......... .......... .......... 16% 12.5M 38s
 81550K .......... .......... .......... .......... .......... 16% 10.5M 38s
 81600K .......... .......... .......... .......... .......... 16% 11.5M 38s
 81650K .......... .......... .......... .......... .......... 16% 21.0M 38s
 81700K .......... .......... .......... .......... .......... 16% 18.7M 38s
 81750K .......... .......... .......... .......... .......... 16% 17.0M 38s
 81800K .......... .......... .......... .......... .......... 16% 22.4M 38s
 81850K .......... .......... .......... .......... .......... 16% 17.1M 38s
 81900K .......... .......... .......... .......... .......... 16% 16.9M 38s
 81950K .......... .......... .......... .......... .......... 16% 15.6M 38s
 82000K .......... .......... .......... .......... .......... 16% 16.1M 38s
 82050K .......... .......... .......... .......... .......... 16% 15.6M 38s
 82100K .......... .......... .......... .......... .......... 16% 13.5M 38s
 82150K .......... .......... .......... .......... .......... 16% 16.2M 38s
 82200K .......... .......... .......... .......... .......... 16% 13.4M 38s
 82250K .......... .......... .......... .......... .......... 16% 14.4M 38s
 82300K .......... .......... .......... .......... .......... 16% 13.9M 38s
 82350K .......... .......... .......... .......... .......... 16% 12.3M 38s
 82400K .......... .......... .......... .......... .......... 16% 11.3M 38s
 82450K .......... .......... .......... .......... .......... 16% 13.8M 38s
 82500K .......... .......... .......... .......... .......... 16% 13.6M 38s
 82550K .......... .......... .......... .......... .......... 16% 9.94M 38s
 82600K .......... .......... .......... .......... .......... 16% 10.6M 38s
 82650K .......... .......... .......... .......... .......... 16% 14.3M 38s
 82700K .......... .......... .......... .......... .......... 16% 11.5M 38s
 82750K .......... .......... .......... .......... .......... 16% 13.1M 38s
 82800K .......... .......... .......... .......... .......... 16% 12.1M 38s
 82850K .......... .......... .......... .......... .......... 16% 10.8M 38s
 82900K .......... .......... .......... .......... .......... 16% 10.8M 38s
 82950K .......... .......... .......... .......... .......... 16% 9.82M 38s
 83000K .......... .......... .......... .......... .......... 16% 9.67M 38s
 83050K .......... .......... .......... .......... .......... 16% 12.3M 38s
 83100K .......... .......... .......... .......... .......... 16% 6.07M 38s
 83150K .......... .......... .......... .......... .......... 16% 6.83M 38s
 83200K .......... .......... .......... .......... .......... 16% 5.99M 38s
 83250K .......... .......... .......... .......... .......... 16% 6.51M 38s
 83300K .......... .......... .......... .......... .......... 16% 6.91M 38s
 83350K .......... .......... .......... .......... .......... 16% 5.50M 38s
 83400K .......... .......... .......... .......... .......... 16% 5.95M 38s
 83450K .......... .......... .......... .......... .......... 16% 7.24M 38s
 83500K .......... .......... .......... .......... .......... 16% 8.75M 38s
 83550K .......... .......... .......... .......... .......... 16% 7.12M 38s
 83600K .......... .......... .......... .......... .......... 16% 5.28M 38s
 83650K .......... .......... .......... .......... .......... 16% 8.51M 38s
 83700K .......... .......... .......... .......... .......... 16% 4.93M 38s
 83750K .......... .......... .......... .......... .......... 16% 6.42M 38s
 83800K .......... .......... .......... .......... .......... 16% 5.18M 38s
 83850K .......... .......... .......... .......... .......... 16% 5.25M 38s
 83900K .......... .......... .......... .......... .......... 16% 6.36M 38s
 83950K .......... .......... .......... .......... .......... 16% 6.78M 38s
 84000K .......... .......... .......... .......... .......... 16%  188M 38s
 84050K .......... .......... .......... .......... .......... 16% 13.9M 38s
 84100K .......... .......... .......... .......... .......... 16% 10.4M 38s
 84150K .......... .......... .......... .......... .......... 16% 12.0M 38s
 84200K .......... .......... .......... .......... .......... 16% 15.2M 38s
 84250K .......... .......... .......... .......... .......... 16% 15.5M 38s
 84300K .......... .......... .......... .......... .......... 16% 12.1M 38s
 84350K .......... .......... .......... .......... .......... 16% 9.54M 38s
 84400K .......... .......... .......... .......... .......... 16% 9.69M 38s
 84450K .......... .......... .......... .......... .......... 16% 9.83M 38s
 84500K .......... .......... .......... .......... .......... 16% 10.3M 38s
 84550K .......... .......... .......... .......... .......... 16% 12.1M 38s
 84600K .......... .......... .......... .......... .......... 16% 9.05M 38s
 84650K .......... .......... .......... .......... .......... 16% 11.1M 38s
 84700K .......... .......... .......... .......... .......... 16% 9.40M 38s
 84750K .......... .......... .......... .......... .......... 16% 8.84M 38s
 84800K .......... .......... .......... .......... .......... 16% 9.23M 38s
 84850K .......... .......... .......... .......... .......... 16% 6.56M 38s
 84900K .......... .......... .......... .......... .......... 16% 6.50M 38s
 84950K .......... .......... .......... .......... .......... 16% 5.89M 38s
 85000K .......... .......... .......... .......... .......... 16% 7.05M 38s
 85050K .......... .......... .......... .......... .......... 16% 5.95M 38s
 85100K .......... .......... .......... .......... .......... 16% 9.76M 38s
 85150K .......... .......... .......... .......... .......... 16% 10.5M 38s
 85200K .......... .......... .......... .......... .......... 16% 6.41M 38s
 85250K .......... .......... .......... .......... .......... 16% 7.28M 38s
 85300K .......... .......... .......... .......... .......... 16% 10.8M 38s
 85350K .......... .......... .......... .......... .......... 16% 11.6M 38s
 85400K .......... .......... .......... .......... .......... 16% 9.36M 38s
 85450K .......... .......... .......... .......... .......... 16% 9.73M 38s
 85500K .......... .......... .......... .......... .......... 16% 12.4M 38s
 85550K .......... .......... .......... .......... .......... 16% 12.0M 38s
 85600K .......... .......... .......... .......... .......... 16% 9.41M 38s
 85650K .......... .......... .......... .......... .......... 16% 9.17M 38s
 85700K .......... .......... .......... .......... .......... 16% 10.7M 38s
 85750K .......... .......... .......... .......... .......... 16% 10.2M 38s
 85800K .......... .......... .......... .......... .......... 16% 15.2M 38s
 85850K .......... .......... .......... .......... .......... 16% 16.8M 38s
 85900K .......... .......... .......... .......... .......... 16% 45.2M 38s
 85950K .......... .......... .......... .......... .......... 16%  151M 38s
 86000K .......... .......... .......... .......... .......... 16% 24.8M 38s
 86050K .......... .......... .......... .......... .......... 16% 23.2M 38s
 86100K .......... .......... .......... .......... .......... 16% 12.8M 38s
 86150K .......... .......... .......... .......... .......... 16% 15.4M 38s
 86200K .......... .......... .......... .......... .......... 16% 11.5M 38s
 86250K .......... .......... .......... .......... .......... 16% 14.5M 38s
 86300K .......... .......... .......... .......... .......... 16% 12.6M 38s
 86350K .......... .......... .......... .......... .......... 16% 10.5M 38s
 86400K .......... .......... .......... .......... .......... 17% 13.7M 38s
 86450K .......... .......... .......... .......... .......... 17% 12.1M 38s
 86500K .......... .......... .......... .......... .......... 17% 13.4M 38s
 86550K .......... .......... .......... .......... .......... 17% 14.8M 38s
 86600K .......... .......... .......... .......... .......... 17% 13.1M 38s
 86650K .......... .......... .......... .......... .......... 17% 11.9M 38s
 86700K .......... .......... .......... .......... .......... 17% 7.38M 38s
 86750K .......... .......... .......... .......... .......... 17% 7.37M 38s
 86800K .......... .......... .......... .......... .......... 17% 6.75M 38s
 86850K .......... .......... .......... .......... .......... 17% 9.36M 38s
 86900K .......... .......... .......... .......... .......... 17% 11.9M 38s
 86950K .......... .......... .......... .......... .......... 17% 7.05M 38s
 87000K .......... .......... .......... .......... .......... 17% 9.24M 38s
 87050K .......... .......... .......... .......... .......... 17% 9.58M 38s
 87100K .......... .......... .......... .......... .......... 17% 7.53M 38s
 87150K .......... .......... .......... .......... .......... 17% 9.96M 38s
 87200K .......... .......... .......... .......... .......... 17% 7.39M 38s
 87250K .......... .......... .......... .......... .......... 17% 18.9M 38s
 87300K .......... .......... .......... .......... .......... 17% 17.1M 38s
 87350K .......... .......... .......... .......... .......... 17% 13.8M 38s
 87400K .......... .......... .......... .......... .......... 17% 11.0M 38s
 87450K .......... .......... .......... .......... .......... 17% 8.50M 38s
 87500K .......... .......... .......... .......... .......... 17% 13.6M 38s
 87550K .......... .......... .......... .......... .......... 17% 13.4M 38s
 87600K .......... .......... .......... .......... .......... 17% 11.4M 38s
 87650K .......... .......... .......... .......... .......... 17% 9.51M 38s
 87700K .......... .......... .......... .......... .......... 17% 6.81M 38s
 87750K .......... .......... .......... .......... .......... 17% 6.92M 38s
 87800K .......... .......... .......... .......... .......... 17% 7.83M 38s
 87850K .......... .......... .......... .......... .......... 17% 7.35M 38s
 87900K .......... .......... .......... .......... .......... 17% 6.95M 38s
 87950K .......... .......... .......... .......... .......... 17% 5.98M 38s
 88000K .......... .......... .......... .......... .......... 17% 8.31M 38s
 88050K .......... .......... .......... .......... .......... 17% 6.84M 38s
 88100K .......... .......... .......... .......... .......... 17% 5.64M 38s
 88150K .......... .......... .......... .......... .......... 17% 9.93M 38s
 88200K .......... .......... .......... .......... .......... 17% 22.4M 38s
 88250K .......... .......... .......... .......... .......... 17% 22.5M 38s
 88300K .......... .......... .......... .......... .......... 17% 28.1M 38s
 88350K .......... .......... .......... .......... .......... 17% 18.6M 38s
 88400K .......... .......... .......... .......... .......... 17% 18.0M 38s
 88450K .......... .......... .......... .......... .......... 17% 12.7M 38s
 88500K .......... .......... .......... .......... .......... 17% 16.8M 38s
 88550K .......... .......... .......... .......... .......... 17% 12.1M 38s
 88600K .......... .......... .......... .......... .......... 17% 9.60M 38s
 88650K .......... .......... .......... .......... .......... 17% 11.9M 38s
 88700K .......... .......... .......... .......... .......... 17% 9.34M 38s
 88750K .......... .......... .......... .......... .......... 17% 10.6M 38s
 88800K .......... .......... .......... .......... .......... 17% 11.8M 38s
 88850K .......... .......... .......... .......... .......... 17% 9.71M 38s
 88900K .......... .......... .......... .......... .......... 17% 7.57M 38s
 88950K .......... .......... .......... .......... .......... 17% 6.48M 38s
 89000K .......... .......... .......... .......... .......... 17% 9.73M 38s
 89050K .......... .......... .......... .......... .......... 17% 7.39M 38s
 89100K .......... .......... .......... .......... .......... 17% 7.07M 38s
 89150K .......... .......... .......... .......... .......... 17% 7.84M 38s
 89200K .......... .......... .......... .......... .......... 17% 8.05M 38s
 89250K .......... .......... .......... .......... .......... 17% 9.01M 38s
 89300K .......... .......... .......... .......... .......... 17% 4.98M 38s
 89350K .......... .......... .......... .......... .......... 17% 4.46M 38s
 89400K .......... .......... .......... .......... .......... 17% 3.44M 38s
 89450K .......... .......... .......... .......... .......... 17% 2.78M 38s
 89500K .......... .......... .......... .......... .......... 17% 3.33M 38s
 89550K .......... .......... .......... .......... .......... 17% 11.0M 38s
 89600K .......... .......... .......... .......... .......... 17% 9.72M 38s
 89650K .......... .......... .......... .......... .......... 17% 10.8M 38s
 89700K .......... .......... .......... .......... .......... 17% 7.38M 38s
 89750K .......... .......... .......... .......... .......... 17% 7.54M 38s
 89800K .......... .......... .......... .......... .......... 17% 9.64M 38s
 89850K .......... .......... .......... .......... .......... 17% 5.43M 38s
 89900K .......... .......... .......... .......... .......... 17% 9.10M 38s
 89950K .......... .......... .......... .......... .......... 17% 8.74M 38s
 90000K .......... .......... .......... .......... .......... 17% 7.35M 38s
 90050K .......... .......... .......... .......... .......... 17% 6.87M 38s
 90100K .......... .......... .......... .......... .......... 17% 5.63M 38s
 90150K .......... .......... .......... .......... .......... 17% 7.89M 38s
 90200K .......... .......... .......... .......... .......... 17% 6.62M 38s
 90250K .......... .......... .......... .......... .......... 17% 14.1M 38s
 90300K .......... .......... .......... .......... .......... 17% 7.44M 38s
 90350K .......... .......... .......... .......... .......... 17% 16.5M 38s
 90400K .......... .......... .......... .......... .......... 17% 14.2M 38s
 90450K .......... .......... .......... .......... .......... 17% 11.1M 38s
 90500K .......... .......... .......... .......... .......... 17% 10.7M 38s
 90550K .......... .......... .......... .......... .......... 17% 12.6M 38s
 90600K .......... .......... .......... .......... .......... 17% 12.8M 38s
 90650K .......... .......... .......... .......... .......... 17% 11.9M 38s
 90700K .......... .......... .......... .......... .......... 17% 10.7M 38s
 90750K .......... .......... .......... .......... .......... 17% 12.5M 38s
 90800K .......... .......... .......... .......... .......... 17% 13.8M 38s
 90850K .......... .......... .......... .......... .......... 17% 8.42M 38s
 90900K .......... .......... .......... .......... .......... 17% 9.27M 38s
 90950K .......... .......... .......... .......... .......... 17% 11.4M 38s
 91000K .......... .......... .......... .......... .......... 17% 11.6M 38s
 91050K .......... .......... .......... .......... .......... 17% 13.0M 38s
 91100K .......... .......... .......... .......... .......... 17% 7.40M 38s
 91150K .......... .......... .......... .......... .......... 17% 10.0M 38s
 91200K .......... .......... .......... .......... .......... 17% 9.72M 38s
 91250K .......... .......... .......... .......... .......... 17% 7.73M 38s
 91300K .......... .......... .......... .......... .......... 17% 9.51M 38s
 91350K .......... .......... .......... .......... .......... 17% 8.03M 38s
 91400K .......... .......... .......... .......... .......... 17% 8.85M 38s
 91450K .......... .......... .......... .......... .......... 17% 5.82M 38s
 91500K .......... .......... .......... .......... .......... 18% 7.10M 38s
 91550K .......... .......... .......... .......... .......... 18% 6.16M 38s
 91600K .......... .......... .......... .......... .......... 18% 5.99M 38s
 91650K .......... .......... .......... .......... .......... 18% 7.57M 38s
 91700K .......... .......... .......... .......... .......... 18% 5.90M 38s
 91750K .......... .......... .......... .......... .......... 18% 15.5M 38s
 91800K .......... .......... .......... .......... .......... 18% 23.6M 38s
 91850K .......... .......... .......... .......... .......... 18% 15.4M 38s
 91900K .......... .......... .......... .......... .......... 18% 14.9M 38s
 91950K .......... .......... .......... .......... .......... 18% 16.1M 38s
 92000K .......... .......... .......... .......... .......... 18% 13.5M 38s
 92050K .......... .......... .......... .......... .......... 18% 15.5M 38s
 92100K .......... .......... .......... .......... .......... 18% 8.24M 38s
 92150K .......... .......... .......... .......... .......... 18% 9.43M 38s
 92200K .......... .......... .......... .......... .......... 18% 8.61M 38s
 92250K .......... .......... .......... .......... .......... 18% 11.8M 38s
 92300K .......... .......... .......... .......... .......... 18% 10.9M 38s
 92350K .......... .......... .......... .......... .......... 18% 9.04M 38s
 92400K .......... .......... .......... .......... .......... 18% 6.14M 38s
 92450K .......... .......... .......... .......... .......... 18% 6.25M 38s
 92500K .......... .......... .......... .......... .......... 18% 9.23M 38s
 92550K .......... .......... .......... .......... .......... 18% 16.7M 38s
 92600K .......... .......... .......... .......... .......... 18% 9.83M 38s
 92650K .......... .......... .......... .......... .......... 18% 9.14M 38s
 92700K .......... .......... .......... .......... .......... 18% 8.28M 38s
 92750K .......... .......... .......... .......... .......... 18% 7.90M 38s
 92800K .......... .......... .......... .......... .......... 18% 12.4M 38s
 92850K .......... .......... .......... .......... .......... 18% 10.8M 38s
 92900K .......... .......... .......... .......... .......... 18% 11.5M 38s
 92950K .......... .......... .......... .......... .......... 18% 10.0M 38s
 93000K .......... .......... .......... .......... .......... 18% 9.80M 38s
 93050K .......... .......... .......... .......... .......... 18% 9.08M 38s
 93100K .......... .......... .......... .......... .......... 18% 8.26M 38s
 93150K .......... .......... .......... .......... .......... 18% 10.3M 38s
 93200K .......... .......... .......... .......... .......... 18% 5.13M 38s
 93250K .......... .......... .......... .......... .......... 18% 7.73M 38s
 93300K .......... .......... .......... .......... .......... 18% 6.55M 38s
 93350K .......... .......... .......... .......... .......... 18% 7.95M 38s
 93400K .......... .......... .......... .......... .......... 18% 6.19M 38s
 93450K .......... .......... .......... .......... .......... 18% 7.10M 38s
 93500K .......... .......... .......... .......... .......... 18% 9.76M 38s
 93550K .......... .......... .......... .......... .......... 18% 10.7M 38s
 93600K .......... .......... .......... .......... .......... 18% 7.93M 38s
 93650K .......... .......... .......... .......... .......... 18% 13.0M 38s
 93700K .......... .......... .......... .......... .......... 18% 11.5M 38s
 93750K .......... .......... .......... .......... .......... 18% 13.5M 38s
 93800K .......... .......... .......... .......... .......... 18% 12.3M 38s
 93850K .......... .......... .......... .......... .......... 18% 10.9M 38s
 93900K .......... .......... .......... .......... .......... 18% 13.1M 38s
 93950K .......... .......... .......... .......... .......... 18% 10.7M 38s
 94000K .......... .......... .......... .......... .......... 18% 8.35M 38s
 94050K .......... .......... .......... .......... .......... 18% 29.1M 38s
 94100K .......... .......... .......... .......... .......... 18% 27.7M 38s
 94150K .......... .......... .......... .......... .......... 18% 22.4M 38s
 94200K .......... .......... .......... .......... .......... 18% 9.78M 38s
 94250K .......... .......... .......... .......... .......... 18%  203M 38s
 94300K .......... .......... .......... .......... .......... 18%  191M 38s
 94350K .......... .......... .......... .......... .......... 18% 18.9M 38s
 94400K .......... .......... .......... .......... .......... 18% 40.5M 38s
 94450K .......... .......... .......... .......... .......... 18% 15.2M 38s
 94500K .......... .......... .......... .......... .......... 18% 16.9M 38s
 94550K .......... .......... .......... .......... .......... 18% 20.7M 38s
 94600K .......... .......... .......... .......... .......... 18% 14.2M 38s
 94650K .......... .......... .......... .......... .......... 18% 15.9M 38s
 94700K .......... .......... .......... .......... .......... 18% 15.8M 38s
 94750K .......... .......... .......... .......... .......... 18% 16.2M 38s
 94800K .......... .......... .......... .......... .......... 18% 13.0M 38s
 94850K .......... .......... .......... .......... .......... 18% 10.2M 38s
 94900K .......... .......... .......... .......... .......... 18% 9.05M 38s
 94950K .......... .......... .......... .......... .......... 18% 7.00M 38s
 95000K .......... .......... .......... .......... .......... 18% 8.22M 38s
 95050K .......... .......... .......... .......... .......... 18% 8.94M 38s
 95100K .......... .......... .......... .......... .......... 18% 8.30M 38s
 95150K .......... .......... .......... .......... .......... 18% 7.57M 38s
 95200K .......... .......... .......... .......... .......... 18% 5.76M 38s
 95250K .......... .......... .......... .......... .......... 18% 7.52M 38s
 95300K .......... .......... .......... .......... .......... 18% 6.02M 38s
 95350K .......... .......... .......... .......... .......... 18% 5.56M 38s
 95400K .......... .......... .......... .......... .......... 18% 6.55M 38s
 95450K .......... .......... .......... .......... .......... 18% 8.69M 38s
 95500K .......... .......... .......... .......... .......... 18% 14.9M 38s
 95550K .......... .......... .......... .......... .......... 18% 12.7M 38s
 95600K .......... .......... .......... .......... .......... 18% 12.2M 38s
 95650K .......... .......... .......... .......... .......... 18% 12.2M 38s
 95700K .......... .......... .......... .......... .......... 18% 11.6M 38s
 95750K .......... .......... .......... .......... .......... 18% 10.4M 38s
 95800K .......... .......... .......... .......... .......... 18% 12.3M 38s
 95850K .......... .......... .......... .......... .......... 18% 15.6M 38s
 95900K .......... .......... .......... .......... .......... 18% 44.7M 38s
 95950K .......... .......... .......... .......... .......... 18% 23.6M 38s
 96000K .......... .......... .......... .......... .......... 18% 22.2M 38s
 96050K .......... .......... .......... .......... .......... 18% 22.8M 38s
 96100K .......... .......... .......... .......... .......... 18% 21.7M 38s
 96150K .......... .......... .......... .......... .......... 18% 24.7M 38s
 96200K .......... .......... .......... .......... .......... 18% 20.4M 38s
 96250K .......... .......... .......... .......... .......... 18% 25.1M 38s
 96300K .......... .......... .......... .......... .......... 18% 18.8M 38s
 96350K .......... .......... .......... .......... .......... 18% 12.8M 38s
 96400K .......... .......... .......... .......... .......... 18% 18.7M 38s
 96450K .......... .......... .......... .......... .......... 18% 13.7M 38s
 96500K .......... .......... .......... .......... .......... 18% 16.1M 38s
 96550K .......... .......... .......... .......... .......... 18% 14.7M 38s
 96600K .......... .......... .......... .......... .......... 19% 11.5M 38s
 96650K .......... .......... .......... .......... .......... 19% 10.1M 38s
 96700K .......... .......... .......... .......... .......... 19% 13.0M 38s
 96750K .......... .......... .......... .......... .......... 19% 8.60M 38s
 96800K .......... .......... .......... .......... .......... 19% 9.52M 38s
 96850K .......... .......... .......... .......... .......... 19% 10.0M 38s
 96900K .......... .......... .......... .......... .......... 19% 12.1M 38s
 96950K .......... .......... .......... .......... .......... 19% 9.96M 38s
 97000K .......... .......... .......... .......... .......... 19% 9.75M 38s
 97050K .......... .......... .......... .......... .......... 19% 9.33M 38s
 97100K .......... .......... .......... .......... .......... 19% 7.27M 38s
 97150K .......... .......... .......... .......... .......... 19% 6.23M 38s
 97200K .......... .......... .......... .......... .......... 19% 4.61M 38s
 97250K .......... .......... .......... .......... .......... 19% 5.04M 38s
 97300K .......... .......... .......... .......... .......... 19% 5.67M 38s
 97350K .......... .......... .......... .......... .......... 19% 19.2M 38s
 97400K .......... .......... .......... .......... .......... 19% 31.9M 38s
 97450K .......... .......... .......... .......... .......... 19% 25.0M 38s
 97500K .......... .......... .......... .......... .......... 19% 30.8M 38s
 97550K .......... .......... .......... .......... .......... 19% 26.8M 38s
 97600K .......... .......... .......... .......... .......... 19% 16.8M 38s
 97650K .......... .......... .......... .......... .......... 19% 22.5M 38s
 97700K .......... .......... .......... .......... .......... 19% 15.2M 38s
 97750K .......... .......... .......... .......... .......... 19% 17.2M 38s
 97800K .......... .......... .......... .......... .......... 19% 15.1M 38s
 97850K .......... .......... .......... .......... .......... 19% 13.8M 38s
 97900K .......... .......... .......... .......... .......... 19% 17.1M 38s
 97950K .......... .......... .......... .......... .......... 19% 17.0M 38s
 98000K .......... .......... .......... .......... .......... 19% 17.4M 38s
 98050K .......... .......... .......... .......... .......... 19% 13.1M 38s
 98100K .......... .......... .......... .......... .......... 19% 11.3M 38s
 98150K .......... .......... .......... .......... .......... 19% 16.5M 37s
 98200K .......... .......... .......... .......... .......... 19% 11.3M 37s
 98250K .......... .......... .......... .......... .......... 19% 12.0M 37s
 98300K .......... .......... .......... .......... .......... 19% 8.97M 37s
 98350K .......... .......... .......... .......... .......... 19% 7.93M 37s
 98400K .......... .......... .......... .......... .......... 19% 7.24M 37s
 98450K .......... .......... .......... .......... .......... 19% 6.13M 37s
 98500K .......... .......... .......... .......... .......... 19% 9.59M 37s
 98550K .......... .......... .......... .......... .......... 19% 14.2M 37s
 98600K .......... .......... .......... .......... .......... 19% 9.65M 37s
 98650K .......... .......... .......... .......... .......... 19% 12.6M 37s
 98700K .......... .......... .......... .......... .......... 19% 11.5M 37s
 98750K .......... .......... .......... .......... .......... 19% 12.7M 37s
 98800K .......... .......... .......... .......... .......... 19% 11.5M 37s
 98850K .......... .......... .......... .......... .......... 19% 12.2M 37s
 98900K .......... .......... .......... .......... .......... 19% 8.66M 37s
 98950K .......... .......... .......... .......... .......... 19% 12.1M 37s
 99000K .......... .......... .......... .......... .......... 19% 11.0M 37s
 99050K .......... .......... .......... .......... .......... 19% 9.06M 37s
 99100K .......... .......... .......... .......... .......... 19% 10.3M 37s
 99150K .......... .......... .......... .......... .......... 19% 8.28M 37s
 99200K .......... .......... .......... .......... .......... 19% 7.81M 37s
 99250K .......... .......... .......... .......... .......... 19% 6.37M 37s
 99300K .......... .......... .......... .......... .......... 19% 7.05M 37s
 99350K .......... .......... .......... .......... .......... 19% 6.92M 37s
 99400K .......... .......... .......... .......... .......... 19% 7.42M 37s
 99450K .......... .......... .......... .......... .......... 19% 5.86M 37s
 99500K .......... .......... .......... .......... .......... 19% 9.80M 37s
 99550K .......... .......... .......... .......... .......... 19% 34.6M 37s
 99600K .......... .......... .......... .......... .......... 19% 22.2M 37s
 99650K .......... .......... .......... .......... .......... 19% 13.8M 37s
 99700K .......... .......... .......... .......... .......... 19% 27.8M 37s
 99750K .......... .......... .......... .......... .......... 19% 11.0M 37s
 99800K .......... .......... .......... .......... .......... 19% 18.9M 37s
 99850K .......... .......... .......... .......... .......... 19% 12.5M 37s
 99900K .......... .......... .......... .......... .......... 19% 16.2M 37s
 99950K .......... .......... .......... .......... .......... 19% 8.77M 37s
100000K .......... .......... .......... .......... .......... 19% 11.3M 37s
100050K .......... .......... .......... .......... .......... 19% 15.0M 37s
100100K .......... .......... .......... .......... .......... 19% 5.86M 37s
100150K .......... .......... .......... .......... .......... 19% 8.14M 37s
100200K .......... .......... .......... .......... .......... 19% 8.89M 37s
100250K .......... .......... .......... .......... .......... 19% 8.54M 37s
100300K .......... .......... .......... .......... .......... 19% 9.55M 37s
100350K .......... .......... .......... .......... .......... 19% 7.90M 37s
100400K .......... .......... .......... .......... .......... 19% 9.27M 37s
100450K .......... .......... .......... .......... .......... 19% 19.3M 37s
100500K .......... .......... .......... .......... .......... 19% 14.8M 37s
100550K .......... .......... .......... .......... .......... 19% 20.5M 37s
100600K .......... .......... .......... .......... .......... 19% 13.6M 37s
100650K .......... .......... .......... .......... .......... 19% 8.57M 37s
100700K .......... .......... .......... .......... .......... 19% 11.1M 37s
100750K .......... .......... .......... .......... .......... 19% 13.2M 37s
100800K .......... .......... .......... .......... .......... 19% 15.0M 37s
100850K .......... .......... .......... .......... .......... 19% 13.2M 37s
100900K .......... .......... .......... .......... .......... 19% 15.6M 37s
100950K .......... .......... .......... .......... .......... 19% 11.9M 37s
101000K .......... .......... .......... .......... .......... 19% 12.1M 37s
101050K .......... .......... .......... .......... .......... 19% 16.2M 37s
101100K .......... .......... .......... .......... .......... 19% 10.5M 37s
101150K .......... .......... .......... .......... .......... 19% 13.4M 37s
101200K .......... .......... .......... .......... .......... 19% 17.9M 37s
101250K .......... .......... .......... .......... .......... 19% 39.2M 37s
101300K .......... .......... .......... .......... .......... 19% 42.5M 37s
101350K .......... .......... .......... .......... .......... 19% 21.8M 37s
101400K .......... .......... .......... .......... .......... 19% 27.7M 37s
101450K .......... .......... .......... .......... .......... 19% 24.4M 37s
101500K .......... .......... .......... .......... .......... 19% 12.0M 37s
101550K .......... .......... .......... .......... .......... 19% 12.4M 37s
101600K .......... .......... .......... .......... .......... 19% 11.9M 37s
101650K .......... .......... .......... .......... .......... 20% 13.4M 37s
101700K .......... .......... .......... .......... .......... 20% 11.1M 37s
101750K .......... .......... .......... .......... .......... 20% 13.5M 37s
101800K .......... .......... .......... .......... .......... 20% 8.81M 37s
101850K .......... .......... .......... .......... .......... 20% 11.5M 37s
101900K .......... .......... .......... .......... .......... 20% 10.5M 37s
101950K .......... .......... .......... .......... .......... 20% 6.84M 37s
102000K .......... .......... .......... .......... .......... 20% 6.61M 37s
102050K .......... .......... .......... .......... .......... 20% 7.15M 37s
102100K .......... .......... .......... .......... .......... 20% 5.61M 37s
102150K .......... .......... .......... .......... .......... 20% 6.48M 37s
102200K .......... .......... .......... .......... .......... 20% 5.94M 37s
102250K .......... .......... .......... .......... .......... 20% 7.90M 37s
102300K .......... .......... .......... .......... .......... 20% 6.75M 37s
102350K .......... .......... .......... .......... .......... 20% 6.78M 37s
102400K .......... .......... .......... .......... .......... 20% 7.75M 37s
102450K .......... .......... .......... .......... .......... 20% 5.96M 37s
102500K .......... .......... .......... .......... .......... 20% 8.67M 37s
102550K .......... .......... .......... .......... .......... 20% 15.6M 37s
102600K .......... .......... .......... .......... .......... 20% 34.6M 37s
102650K .......... .......... .......... .......... .......... 20% 16.3M 37s
102700K .......... .......... .......... .......... .......... 20% 42.5M 37s
102750K .......... .......... .......... .......... .......... 20% 15.9M 37s
102800K .......... .......... .......... .......... .......... 20% 19.6M 37s
102850K .......... .......... .......... .......... .......... 20% 10.1M 37s
102900K .......... .......... .......... .......... .......... 20% 13.7M 37s
102950K .......... .......... .......... .......... .......... 20% 9.07M 37s
103000K .......... .......... .......... .......... .......... 20% 9.44M 37s
103050K .......... .......... .......... .......... .......... 20% 9.47M 37s
103100K .......... .......... .......... .......... .......... 20% 8.57M 37s
103150K .......... .......... .......... .......... .......... 20% 8.65M 37s
103200K .......... .......... .......... .......... .......... 20% 7.23M 37s
103250K .......... .......... .......... .......... .......... 20% 5.98M 37s
103300K .......... .......... .......... .......... .......... 20% 6.84M 37s
103350K .......... .......... .......... .......... .......... 20% 8.57M 37s
103400K .......... .......... .......... .......... .......... 20% 12.3M 37s
103450K .......... .......... .......... .......... .......... 20% 9.80M 37s
103500K .......... .......... .......... .......... .......... 20% 9.40M 37s
103550K .......... .......... .......... .......... .......... 20% 9.10M 37s
103600K .......... .......... .......... .......... .......... 20% 7.73M 37s
103650K .......... .......... .......... .......... .......... 20% 10.1M 37s
103700K .......... .......... .......... .......... .......... 20% 9.12M 37s
103750K .......... .......... .......... .......... .......... 20% 7.81M 37s
103800K .......... .......... .......... .......... .......... 20% 6.81M 37s
103850K .......... .......... .......... .......... .......... 20% 4.61M 37s
103900K .......... .......... .......... .......... .......... 20% 7.24M 37s
103950K .......... .......... .......... .......... .......... 20% 5.52M 37s
104000K .......... .......... .......... .......... .......... 20% 7.99M 37s
104050K .......... .......... .......... .......... .......... 20% 9.33M 37s
104100K .......... .......... .......... .......... .......... 20% 8.46M 37s
104150K .......... .......... .......... .......... .......... 20% 7.12M 37s
104200K .......... .......... .......... .......... .......... 20% 5.30M 37s
104250K .......... .......... .......... .......... .......... 20% 4.09M 37s
104300K .......... .......... .......... .......... .......... 20% 3.91M 37s
104350K .......... .......... .......... .......... .......... 20% 3.30M 37s
104400K .......... .......... .......... .......... .......... 20% 9.02M 37s
104450K .......... .......... .......... .......... .......... 20% 10.6M 37s
104500K .......... .......... .......... .......... .......... 20% 14.5M 37s
104550K .......... .......... .......... .......... .......... 20% 12.2M 37s
104600K .......... .......... .......... .......... .......... 20% 10.3M 37s
104650K .......... .......... .......... .......... .......... 20% 9.37M 37s
104700K .......... .......... .......... .......... .......... 20% 6.87M 37s
104750K .......... .......... .......... .......... .......... 20% 8.97M 37s
104800K .......... .......... .......... .......... .......... 20% 7.58M 37s
104850K .......... .......... .......... .......... .......... 20% 6.37M 37s
104900K .......... .......... .......... .......... .......... 20% 6.91M 37s
104950K .......... .......... .......... .......... .......... 20% 5.47M 37s
105000K .......... .......... .......... .......... .......... 20% 6.77M 37s
105050K .......... .......... .......... .......... .......... 20% 10.5M 37s
105100K .......... .......... .......... .......... .......... 20% 13.1M 37s
105150K .......... .......... .......... .......... .......... 20% 16.9M 37s
105200K .......... .......... .......... .......... .......... 20% 5.39M 37s
105250K .......... .......... .......... .......... .......... 20% 5.11M 37s
105300K .......... .......... .......... .......... .......... 20% 6.45M 37s
105350K .......... .......... .......... .......... .......... 20% 4.71M 37s
105400K .......... .......... .......... .......... .......... 20% 4.76M 37s
105450K .......... .......... .......... .......... .......... 20% 4.04M 37s
105500K .......... .......... .......... .......... .......... 20% 3.95M 37s
105550K .......... .......... .......... .......... .......... 20% 3.64M 37s
105600K .......... .......... .......... .......... .......... 20% 5.30M 37s
105650K .......... .......... .......... .......... .......... 20% 21.2M 37s
105700K .......... .......... .......... .......... .......... 20% 15.5M 37s
105750K .......... .......... .......... .......... .......... 20% 15.8M 37s
105800K .......... .......... .......... .......... .......... 20% 13.7M 37s
105850K .......... .......... .......... .......... .......... 20% 9.05M 37s
105900K .......... .......... .......... .......... .......... 20% 11.5M 37s
105950K .......... .......... .......... .......... .......... 20% 8.07M 37s
106000K .......... .......... .......... .......... .......... 20% 9.63M 37s
106050K .......... .......... .......... .......... .......... 20% 10.8M 37s
106100K .......... .......... .......... .......... .......... 20% 9.05M 37s
106150K .......... .......... .......... .......... .......... 20% 11.9M 37s
106200K .......... .......... .......... .......... .......... 20% 7.49M 37s
106250K .......... .......... .......... .......... .......... 20% 13.8M 37s
106300K .......... .......... .......... .......... .......... 20% 10.4M 37s
106350K .......... .......... .......... .......... .......... 20% 10.0M 37s
106400K .......... .......... .......... .......... .......... 20% 13.7M 37s
106450K .......... .......... .......... .......... .......... 20% 11.8M 37s
106500K .......... .......... .......... .......... .......... 20% 13.2M 37s
106550K .......... .......... .......... .......... .......... 20% 16.2M 37s
106600K .......... .......... .......... .......... .......... 20% 11.5M 37s
106650K .......... .......... .......... .......... .......... 20% 15.7M 37s
106700K .......... .......... .......... .......... .......... 20% 26.2M 37s
106750K .......... .......... .......... .......... .......... 21% 43.2M 37s
106800K .......... .......... .......... .......... .......... 21% 25.5M 37s
106850K .......... .......... .......... .......... .......... 21% 23.7M 37s
106900K .......... .......... .......... .......... .......... 21%  245M 37s
106950K .......... .......... .......... .......... .......... 21% 25.8M 37s
107000K .......... .......... .......... .......... .......... 21% 18.9M 37s
107050K .......... .......... .......... .......... .......... 21% 15.1M 37s
107100K .......... .......... .......... .......... .......... 21% 6.73M 37s
107150K .......... .......... .......... .......... .......... 21% 7.10M 37s
107200K .......... .......... .......... .......... .......... 21% 6.28M 37s
107250K .......... .......... .......... .......... .......... 21% 5.38M 37s
107300K .......... .......... .......... .......... .......... 21% 5.98M 37s
107350K .......... .......... .......... .......... .......... 21% 4.94M 37s
107400K .......... .......... .......... .......... .......... 21% 5.55M 37s
107450K .......... .......... .......... .......... .......... 21% 7.80M 37s
107500K .......... .......... .......... .......... .......... 21% 7.26M 37s
107550K .......... .......... .......... .......... .......... 21%  236M 37s
107600K .......... .......... .......... .......... .......... 21% 30.2M 37s
107650K .......... .......... .......... .......... .......... 21% 22.1M 37s
107700K .......... .......... .......... .......... .......... 21% 8.65M 37s
107750K .......... .......... .......... .......... .......... 21% 15.3M 37s
107800K .......... .......... .......... .......... .......... 21% 22.4M 37s
107850K .......... .......... .......... .......... .......... 21% 10.5M 37s
107900K .......... .......... .......... .......... .......... 21% 18.7M 37s
107950K .......... .......... .......... .......... .......... 21% 10.5M 37s
108000K .......... .......... .......... .......... .......... 21% 13.0M 37s
108050K .......... .......... .......... .......... .......... 21% 9.78M 37s
108100K .......... .......... .......... .......... .......... 21% 8.70M 37s
108150K .......... .......... .......... .......... .......... 21% 8.65M 37s
108200K .......... .......... .......... .......... .......... 21% 7.83M 37s
108250K .......... .......... .......... .......... .......... 21% 8.38M 37s
108300K .......... .......... .......... .......... .......... 21% 7.42M 37s
108350K .......... .......... .......... .......... .......... 21% 6.51M 37s
108400K .......... .......... .......... .......... .......... 21% 6.83M 37s
108450K .......... .......... .......... .......... .......... 21% 5.16M 37s
108500K .......... .......... .......... .......... .......... 21% 14.1M 37s
108550K .......... .......... .......... .......... .......... 21% 19.3M 37s
108600K .......... .......... .......... .......... .......... 21% 14.0M 37s
108650K .......... .......... .......... .......... .......... 21% 13.2M 37s
108700K .......... .......... .......... .......... .......... 21% 10.8M 37s
108750K .......... .......... .......... .......... .......... 21% 9.06M 37s
108800K .......... .......... .......... .......... .......... 21% 8.06M 37s
108850K .......... .......... .......... .......... .......... 21% 11.0M 37s
108900K .......... .......... .......... .......... .......... 21% 12.3M 37s
108950K .......... .......... .......... .......... .......... 21% 10.2M 37s
109000K .......... .......... .......... .......... .......... 21% 11.6M 37s
109050K .......... .......... .......... .......... .......... 21% 15.4M 37s
109100K .......... .......... .......... .......... .......... 21% 7.84M 37s
109150K .......... .......... .......... .......... .......... 21% 8.94M 37s
109200K .......... .......... .......... .......... .......... 21% 7.35M 37s
109250K .......... .......... .......... .......... .......... 21% 7.00M 37s
109300K .......... .......... .......... .......... .......... 21% 6.93M 37s
109350K .......... .......... .......... .......... .......... 21% 7.16M 37s
109400K .......... .......... .......... .......... .......... 21% 7.88M 37s
109450K .......... .......... .......... .......... .......... 21% 7.06M 37s
109500K .......... .......... .......... .......... .......... 21% 6.67M 37s
109550K .......... .......... .......... .......... .......... 21% 8.88M 37s
109600K .......... .......... .......... .......... .......... 21% 6.92M 37s
109650K .......... .......... .......... .......... .......... 21% 8.42M 37s
109700K .......... .......... .......... .......... .......... 21% 6.26M 37s
109750K .......... .......... .......... .......... .......... 21% 8.11M 37s
109800K .......... .......... .......... .......... .......... 21% 9.00M 37s
109850K .......... .......... .......... .......... .......... 21% 6.68M 37s
109900K .......... .......... .......... .......... .......... 21% 8.04M 37s
109950K .......... .......... .......... .......... .......... 21% 5.18M 37s
110000K .......... .......... .......... .......... .......... 21% 6.30M 37s
110050K .......... .......... .......... .......... .......... 21% 7.04M 37s
110100K .......... .......... .......... .......... .......... 21% 5.87M 37s
110150K .......... .......... .......... .......... .......... 21% 8.51M 37s
110200K .......... .......... .......... .......... .......... 21% 15.0M 37s
110250K .......... .......... .......... .......... .......... 21% 13.4M 37s
110300K .......... .......... .......... .......... .......... 21% 16.3M 37s
110350K .......... .......... .......... .......... .......... 21% 11.1M 37s
110400K .......... .......... .......... .......... .......... 21% 9.66M 37s
110450K .......... .......... .......... .......... .......... 21% 8.25M 37s
110500K .......... .......... .......... .......... .......... 21% 9.46M 37s
110550K .......... .......... .......... .......... .......... 21% 9.09M 37s
110600K .......... .......... .......... .......... .......... 21% 7.96M 37s
110650K .......... .......... .......... .......... .......... 21% 8.23M 37s
110700K .......... .......... .......... .......... .......... 21% 11.0M 37s
110750K .......... .......... .......... .......... .......... 21% 22.1M 37s
110800K .......... .......... .......... .......... .......... 21% 27.9M 37s
110850K .......... .......... .......... .......... .......... 21% 23.4M 37s
110900K .......... .......... .......... .......... .......... 21% 45.7M 37s
110950K .......... .......... .......... .......... .......... 21% 21.3M 37s
111000K .......... .......... .......... .......... .......... 21% 25.5M 37s
111050K .......... .......... .......... .......... .......... 21% 14.1M 37s
111100K .......... .......... .......... .......... .......... 21% 20.4M 37s
111150K .......... .......... .......... .......... .......... 21% 20.6M 37s
111200K .......... .......... .......... .......... .......... 21% 14.3M 37s
111250K .......... .......... .......... .......... .......... 21% 18.2M 37s
111300K .......... .......... .......... .......... .......... 21% 19.9M 37s
111350K .......... .......... .......... .......... .......... 21% 13.4M 37s
111400K .......... .......... .......... .......... .......... 21% 21.3M 37s
111450K .......... .......... .......... .......... .......... 21% 15.4M 37s
111500K .......... .......... .......... .......... .......... 21% 19.4M 37s
111550K .......... .......... .......... .......... .......... 21% 14.6M 37s
111600K .......... .......... .......... .......... .......... 21% 12.2M 37s
111650K .......... .......... .......... .......... .......... 21% 11.8M 37s
111700K .......... .......... .......... .......... .......... 21% 12.0M 37s
111750K .......... .......... .......... .......... .......... 21% 11.5M 37s
111800K .......... .......... .......... .......... .......... 21% 11.4M 37s
111850K .......... .......... .......... .......... .......... 22% 10.2M 37s
111900K .......... .......... .......... .......... .......... 22% 10.0M 37s
111950K .......... .......... .......... .......... .......... 22% 8.67M 37s
112000K .......... .......... .......... .......... .......... 22% 9.81M 37s
112050K .......... .......... .......... .......... .......... 22% 10.7M 37s
112100K .......... .......... .......... .......... .......... 22% 9.10M 37s
112150K .......... .......... .......... .......... .......... 22% 10.5M 37s
112200K .......... .......... .......... .......... .......... 22% 8.48M 37s
112250K .......... .......... .......... .......... .......... 22% 15.8M 37s
112300K .......... .......... .......... .......... .......... 22% 22.4M 37s
112350K .......... .......... .......... .......... .......... 22% 32.1M 37s
112400K .......... .......... .......... .......... .......... 22% 27.9M 37s
112450K .......... .......... .......... .......... .......... 22% 55.7M 37s
112500K .......... .......... .......... .......... .......... 22% 22.6M 37s
112550K .......... .......... .......... .......... .......... 22% 15.8M 37s
112600K .......... .......... .......... .......... .......... 22% 14.1M 37s
112650K .......... .......... .......... .......... .......... 22% 12.6M 37s
112700K .......... .......... .......... .......... .......... 22% 9.36M 37s
112750K .......... .......... .......... .......... .......... 22% 10.1M 37s
112800K .......... .......... .......... .......... .......... 22% 12.1M 37s
112850K .......... .......... .......... .......... .......... 22% 9.08M 37s
112900K .......... .......... .......... .......... .......... 22% 11.6M 37s
112950K .......... .......... .......... .......... .......... 22% 7.72M 37s
113000K .......... .......... .......... .......... .......... 22% 10.2M 37s
113050K .......... .......... .......... .......... .......... 22% 8.73M 37s
113100K .......... .......... .......... .......... .......... 22% 6.93M 37s
113150K .......... .......... .......... .......... .......... 22% 8.98M 37s
113200K .......... .......... .......... .......... .......... 22% 7.29M 37s
113250K .......... .......... .......... .......... .......... 22% 19.6M 37s
113300K .......... .......... .......... .......... .......... 22% 34.3M 37s
113350K .......... .......... .......... .......... .......... 22% 24.1M 37s
113400K .......... .......... .......... .......... .......... 22% 26.2M 37s
113450K .......... .......... .......... .......... .......... 22% 17.9M 37s
113500K .......... .......... .......... .......... .......... 22% 16.8M 37s
113550K .......... .......... .......... .......... .......... 22% 17.3M 37s
113600K .......... .......... .......... .......... .......... 22% 16.0M 37s
113650K .......... .......... .......... .......... .......... 22% 16.9M 37s
113700K .......... .......... .......... .......... .......... 22% 15.3M 37s
113750K .......... .......... .......... .......... .......... 22% 17.1M 37s
113800K .......... .......... .......... .......... .......... 22% 15.6M 36s
113850K .......... .......... .......... .......... .......... 22% 14.5M 36s
113900K .......... .......... .......... .......... .......... 22% 16.6M 36s
113950K .......... .......... .......... .......... .......... 22% 13.8M 36s
114000K .......... .......... .......... .......... .......... 22% 13.8M 36s
114050K .......... .......... .......... .......... .......... 22% 33.0M 36s
114100K .......... .......... .......... .......... .......... 22% 20.2M 36s
114150K .......... .......... .......... .......... .......... 22%  161M 36s
114200K .......... .......... .......... .......... .......... 22% 27.9M 36s
114250K .......... .......... .......... .......... .......... 22% 22.7M 36s
114300K .......... .......... .......... .......... .......... 22% 29.4M 36s
114350K .......... .......... .......... .......... .......... 22% 10.4M 36s
114400K .......... .......... .......... .......... .......... 22% 13.3M 36s
114450K .......... .......... .......... .......... .......... 22% 15.0M 36s
114500K .......... .......... .......... .......... .......... 22% 14.5M 36s
114550K .......... .......... .......... .......... .......... 22% 13.5M 36s
114600K .......... .......... .......... .......... .......... 22% 8.38M 36s
114650K .......... .......... .......... .......... .......... 22% 7.55M 36s
114700K .......... .......... .......... .......... .......... 22% 10.2M 36s
114750K .......... .......... .......... .......... .......... 22% 9.80M 36s
114800K .......... .......... .......... .......... .......... 22% 9.68M 36s
114850K .......... .......... .......... .......... .......... 22% 8.24M 36s
114900K .......... .......... .......... .......... .......... 22% 11.0M 36s
114950K .......... .......... .......... .......... .......... 22% 6.91M 36s
115000K .......... .......... .......... .......... .......... 22% 13.5M 36s
115050K .......... .......... .......... .......... .......... 22% 17.4M 36s
115100K .......... .......... .......... .......... .......... 22% 11.5M 36s
115150K .......... .......... .......... .......... .......... 22% 8.47M 36s
115200K .......... .......... .......... .......... .......... 22% 7.36M 36s
115250K .......... .......... .......... .......... .......... 22% 8.54M 36s
115300K .......... .......... .......... .......... .......... 22% 9.55M 36s
115350K .......... .......... .......... .......... .......... 22% 9.03M 36s
115400K .......... .......... .......... .......... .......... 22% 8.87M 36s
115450K .......... .......... .......... .......... .......... 22% 7.85M 36s
115500K .......... .......... .......... .......... .......... 22% 16.1M 36s
115550K .......... .......... .......... .......... .......... 22% 29.0M 36s
115600K .......... .......... .......... .......... .......... 22% 12.9M 36s
115650K .......... .......... .......... .......... .......... 22% 39.7M 36s
115700K .......... .......... .......... .......... .......... 22% 21.5M 36s
115750K .......... .......... .......... .......... .......... 22% 20.1M 36s
115800K .......... .......... .......... .......... .......... 22% 15.3M 36s
115850K .......... .......... .......... .......... .......... 22% 13.4M 36s
115900K .......... .......... .......... .......... .......... 22% 16.2M 36s
115950K .......... .......... .......... .......... .......... 22% 12.0M 36s
116000K .......... .......... .......... .......... .......... 22% 13.5M 36s
116050K .......... .......... .......... .......... .......... 22% 11.1M 36s
116100K .......... .......... .......... .......... .......... 22% 7.48M 36s
116150K .......... .......... .......... .......... .......... 22% 9.28M 36s
116200K .......... .......... .......... .......... .......... 22% 6.20M 36s
116250K .......... .......... .......... .......... .......... 22% 9.17M 36s
116300K .......... .......... .......... .......... .......... 22% 8.76M 36s
116350K .......... .......... .......... .......... .......... 22% 6.52M 36s
116400K .......... .......... .......... .......... .......... 22% 8.46M 36s
116450K .......... .......... .......... .......... .......... 22% 9.18M 36s
116500K .......... .......... .......... .......... .......... 22% 7.38M 36s
116550K .......... .......... .......... .......... .......... 22% 8.02M 36s
116600K .......... .......... .......... .......... .......... 22% 6.71M 36s
116650K .......... .......... .......... .......... .......... 22% 6.80M 36s
116700K .......... .......... .......... .......... .......... 22% 4.22M 36s
116750K .......... .......... .......... .......... .......... 22% 5.89M 36s
116800K .......... .......... .......... .......... .......... 22% 4.77M 36s
116850K .......... .......... .......... .......... .......... 22% 4.38M 36s
116900K .......... .......... .......... .......... .......... 23% 5.10M 36s
116950K .......... .......... .......... .......... .......... 23% 4.22M 36s
117000K .......... .......... .......... .......... .......... 23% 4.82M 36s
117050K .......... .......... .......... .......... .......... 23% 5.61M 36s
117100K .......... .......... .......... .......... .......... 23% 5.10M 36s
117150K .......... .......... .......... .......... .......... 23% 6.19M 36s
117200K .......... .......... .......... .......... .......... 23% 6.18M 36s
117250K .......... .......... .......... .......... .......... 23% 12.4M 36s
117300K .......... .......... .......... .......... .......... 23% 10.4M 36s
117350K .......... .......... .......... .......... .......... 23% 9.13M 36s
117400K .......... .......... .......... .......... .......... 23% 9.83M 36s
117450K .......... .......... .......... .......... .......... 23% 9.05M 36s
117500K .......... .......... .......... .......... .......... 23% 6.71M 36s
117550K .......... .......... .......... .......... .......... 23% 9.49M 36s
117600K .......... .......... .......... .......... .......... 23% 11.3M 36s
117650K .......... .......... .......... .......... .......... 23% 10.7M 36s
117700K .......... .......... .......... .......... .......... 23% 11.1M 36s
117750K .......... .......... .......... .......... .......... 23% 15.4M 36s
117800K .......... .......... .......... .......... .......... 23% 13.1M 36s
117850K .......... .......... .......... .......... .......... 23% 11.2M 36s
117900K .......... .......... .......... .......... .......... 23% 12.5M 36s
117950K .......... .......... .......... .......... .......... 23% 13.2M 36s
118000K .......... .......... .......... .......... .......... 23% 15.4M 36s
118050K .......... .......... .......... .......... .......... 23% 20.9M 36s
118100K .......... .......... .......... .......... .......... 23% 46.5M 36s
118150K .......... .......... .......... .......... .......... 23% 50.4M 36s
118200K .......... .......... .......... .......... .......... 23% 47.2M 36s
118250K .......... .......... .......... .......... .......... 23% 25.4M 36s
118300K .......... .......... .......... .......... .......... 23% 50.8M 36s
118350K .......... .......... .......... .......... .......... 23% 57.0M 36s
118400K .......... .......... .......... .......... .......... 23% 44.4M 36s
118450K .......... .......... .......... .......... .......... 23% 20.3M 36s
118500K .......... .......... .......... .......... .......... 23% 20.0M 36s
118550K .......... .......... .......... .......... .......... 23% 17.6M 36s
118600K .......... .......... .......... .......... .......... 23% 17.5M 36s
118650K .......... .......... .......... .......... .......... 23% 22.1M 36s
118700K .......... .......... .......... .......... .......... 23% 18.4M 36s
118750K .......... .......... .......... .......... .......... 23% 21.4M 36s
118800K .......... .......... .......... .......... .......... 23% 20.3M 36s
118850K .......... .......... .......... .......... .......... 23% 19.1M 36s
118900K .......... .......... .......... .......... .......... 23% 19.7M 36s
118950K .......... .......... .......... .......... .......... 23% 15.8M 36s
119000K .......... .......... .......... .......... .......... 23% 21.8M 36s
119050K .......... .......... .......... .......... .......... 23% 11.7M 36s
119100K .......... .......... .......... .......... .......... 23% 10.4M 36s
119150K .......... .......... .......... .......... .......... 23% 13.1M 36s
119200K .......... .......... .......... .......... .......... 23% 8.17M 36s
119250K .......... .......... .......... .......... .......... 23% 11.0M 36s
119300K .......... .......... .......... .......... .......... 23% 12.3M 36s
119350K .......... .......... .......... .......... .......... 23% 11.4M 36s
119400K .......... .......... .......... .......... .......... 23% 8.95M 36s
119450K .......... .......... .......... .......... .......... 23% 6.44M 36s
119500K .......... .......... .......... .......... .......... 23% 10.5M 36s
119550K .......... .......... .......... .......... .......... 23% 9.10M 36s
119600K .......... .......... .......... .......... .......... 23% 7.80M 36s
119650K .......... .......... .......... .......... .......... 23% 8.56M 36s
119700K .......... .......... .......... .......... .......... 23% 8.14M 36s
119750K .......... .......... .......... .......... .......... 23% 11.0M 36s
119800K .......... .......... .......... .......... .......... 23% 19.4M 36s
119850K .......... .......... .......... .......... .......... 23% 13.9M 36s
119900K .......... .......... .......... .......... .......... 23% 7.58M 36s
119950K .......... .......... .......... .......... .......... 23% 8.48M 36s
120000K .......... .......... .......... .......... .......... 23% 7.87M 36s
120050K .......... .......... .......... .......... .......... 23% 5.23M 36s
120100K .......... .......... .......... .......... .......... 23% 7.27M 36s
120150K .......... .......... .......... .......... .......... 23% 14.7M 36s
120200K .......... .......... .......... .......... .......... 23% 9.90M 36s
120250K .......... .......... .......... .......... .......... 23% 12.0M 36s
120300K .......... .......... .......... .......... .......... 23% 9.41M 36s
120350K .......... .......... .......... .......... .......... 23% 10.6M 36s
120400K .......... .......... .......... .......... .......... 23% 10.5M 36s
120450K .......... .......... .......... .......... .......... 23% 11.5M 36s
120500K .......... .......... .......... .......... .......... 23% 9.88M 36s
120550K .......... .......... .......... .......... .......... 23% 11.5M 36s
120600K .......... .......... .......... .......... .......... 23% 10.1M 36s
120650K .......... .......... .......... .......... .......... 23% 15.5M 36s
120700K .......... .......... .......... .......... .......... 23% 44.1M 36s
120750K .......... .......... .......... .......... .......... 23% 24.9M 36s
120800K .......... .......... .......... .......... .......... 23%  132M 36s
120850K .......... .......... .......... .......... .......... 23% 27.7M 36s
120900K .......... .......... .......... .......... .......... 23% 26.8M 36s
120950K .......... .......... .......... .......... .......... 23% 22.1M 36s
121000K .......... .......... .......... .......... .......... 23% 18.8M 36s
121050K .......... .......... .......... .......... .......... 23% 20.1M 36s
121100K .......... .......... .......... .......... .......... 23% 11.8M 36s
121150K .......... .......... .......... .......... .......... 23% 15.8M 36s
121200K .......... .......... .......... .......... .......... 23% 14.2M 36s
121250K .......... .......... .......... .......... .......... 23% 18.0M 36s
121300K .......... .......... .......... .......... .......... 23% 15.1M 36s
121350K .......... .......... .......... .......... .......... 23% 13.3M 36s
121400K .......... .......... .......... .......... .......... 23% 12.3M 36s
121450K .......... .......... .......... .......... .......... 23% 11.7M 36s
121500K .......... .......... .......... .......... .......... 23% 12.1M 36s
121550K .......... .......... .......... .......... .......... 23% 12.1M 36s
121600K .......... .......... .......... .......... .......... 23% 9.57M 36s
121650K .......... .......... .......... .......... .......... 23% 10.2M 36s
121700K .......... .......... .......... .......... .......... 23% 8.33M 36s
121750K .......... .......... .......... .......... .......... 23% 10.3M 36s
121800K .......... .......... .......... .......... .......... 23% 9.75M 36s
121850K .......... .......... .......... .......... .......... 23% 7.96M 36s
121900K .......... .......... .......... .......... .......... 23% 7.56M 36s
121950K .......... .......... .......... .......... .......... 23% 20.3M 36s
122000K .......... .......... .......... .......... .......... 24% 11.3M 36s
122050K .......... .......... .......... .......... .......... 24% 20.9M 36s
122100K .......... .......... .......... .......... .......... 24% 9.23M 36s
122150K .......... .......... .......... .......... .......... 24% 13.7M 36s
122200K .......... .......... .......... .......... .......... 24% 11.4M 36s
122250K .......... .......... .......... .......... .......... 24% 10.8M 36s
122300K .......... .......... .......... .......... .......... 24% 12.1M 36s
122350K .......... .......... .......... .......... .......... 24% 9.33M 36s
122400K .......... .......... .......... .......... .......... 24% 8.01M 36s
122450K .......... .......... .......... .......... .......... 24% 8.83M 36s
122500K .......... .......... .......... .......... .......... 24% 13.0M 36s
122550K .......... .......... .......... .......... .......... 24% 12.8M 36s
122600K .......... .......... .......... .......... .......... 24% 9.94M 36s
122650K .......... .......... .......... .......... .......... 24% 8.25M 36s
122700K .......... .......... .......... .......... .......... 24% 6.45M 36s
122750K .......... .......... .......... .......... .......... 24% 7.35M 36s
122800K .......... .......... .......... .......... .......... 24% 9.40M 36s
122850K .......... .......... .......... .......... .......... 24% 7.49M 36s
122900K .......... .......... .......... .......... .......... 24% 9.42M 36s
122950K .......... .......... .......... .......... .......... 24% 6.39M 36s
123000K .......... .......... .......... .......... .......... 24% 5.26M 36s
123050K .......... .......... .......... .......... .......... 24% 4.95M 36s
123100K .......... .......... .......... .......... .......... 24% 4.81M 36s
123150K .......... .......... .......... .......... .......... 24% 11.5M 36s
123200K .......... .......... .......... .......... .......... 24% 8.01M 36s
123250K .......... .......... .......... .......... .......... 24% 9.58M 36s
123300K .......... .......... .......... .......... .......... 24% 7.76M 36s
123350K .......... .......... .......... .......... .......... 24% 6.27M 36s
123400K .......... .......... .......... .......... .......... 24% 6.46M 36s
123450K .......... .......... .......... .......... .......... 24% 5.42M 36s
123500K .......... .......... .......... .......... .......... 24% 8.31M 36s
123550K .......... .......... .......... .......... .......... 24% 21.8M 36s
123600K .......... .......... .......... .......... .......... 24% 37.2M 36s
123650K .......... .......... .......... .......... .......... 24% 30.8M 36s
123700K .......... .......... .......... .......... .......... 24% 23.7M 36s
123750K .......... .......... .......... .......... .......... 24% 22.6M 36s
123800K .......... .......... .......... .......... .......... 24% 43.4M 36s
123850K .......... .......... .......... .......... .......... 24% 22.9M 36s
123900K .......... .......... .......... .......... .......... 24% 25.8M 36s
123950K .......... .......... .......... .......... .......... 24% 27.9M 36s
124000K .......... .......... .......... .......... .......... 24% 33.2M 36s
124050K .......... .......... .......... .......... .......... 24% 27.7M 35s
124100K .......... .......... .......... .......... .......... 24% 23.1M 35s
124150K .......... .......... .......... .......... .......... 24% 32.7M 35s
124200K .......... .......... .......... .......... .......... 24% 21.0M 35s
124250K .......... .......... .......... .......... .......... 24% 29.9M 35s
124300K .......... .......... .......... .......... .......... 24% 32.9M 35s
124350K .......... .......... .......... .......... .......... 24% 19.9M 35s
124400K .......... .......... .......... .......... .......... 24% 35.7M 35s
124450K .......... .......... .......... .......... .......... 24% 19.8M 35s
124500K .......... .......... .......... .......... .......... 24% 34.3M 35s
124550K .......... .......... .......... .......... .......... 24% 27.3M 35s
124600K .......... .......... .......... .......... .......... 24% 14.1M 35s
124650K .......... .......... .......... .......... .......... 24% 35.7M 35s
124700K .......... .......... .......... .......... .......... 24% 12.4M 35s
124750K .......... .......... .......... .......... .......... 24% 13.8M 35s
124800K .......... .......... .......... .......... .......... 24% 9.42M 35s
124850K .......... .......... .......... .......... .......... 24% 9.71M 35s
124900K .......... .......... .......... .......... .......... 24% 11.7M 35s
124950K .......... .......... .......... .......... .......... 24% 10.1M 35s
125000K .......... .......... .......... .......... .......... 24% 11.9M 35s
125050K .......... .......... .......... .......... .......... 24% 9.88M 35s
125100K .......... .......... .......... .......... .......... 24% 11.2M 35s
125150K .......... .......... .......... .......... .......... 24% 12.3M 35s
125200K .......... .......... .......... .......... .......... 24% 20.2M 35s
125250K .......... .......... .......... .......... .......... 24% 25.4M 35s
125300K .......... .......... .......... .......... .......... 24% 27.4M 35s
125350K .......... .......... .......... .......... .......... 24% 32.8M 35s
125400K .......... .......... .......... .......... .......... 24% 19.7M 35s
125450K .......... .......... .......... .......... .......... 24% 11.6M 35s
125500K .......... .......... .......... .......... .......... 24% 13.3M 35s
125550K .......... .......... .......... .......... .......... 24% 13.7M 35s
125600K .......... .......... .......... .......... .......... 24% 10.7M 35s
125650K .......... .......... .......... .......... .......... 24% 9.05M 35s
125700K .......... .......... .......... .......... .......... 24% 11.4M 35s
125750K .......... .......... .......... .......... .......... 24% 7.96M 35s
125800K .......... .......... .......... .......... .......... 24% 8.34M 35s
125850K .......... .......... .......... .......... .......... 24% 7.29M 35s
125900K .......... .......... .......... .......... .......... 24% 8.53M 35s
125950K .......... .......... .......... .......... .......... 24% 7.96M 35s
126000K .......... .......... .......... .......... .......... 24% 8.33M 35s
126050K .......... .......... .......... .......... .......... 24% 16.3M 35s
126100K .......... .......... .......... .......... .......... 24% 16.4M 35s
126150K .......... .......... .......... .......... .......... 24% 52.3M 35s
126200K .......... .......... .......... .......... .......... 24% 24.5M 35s
126250K .......... .......... .......... .......... .......... 24% 25.7M 35s
126300K .......... .......... .......... .......... .......... 24% 20.1M 35s
126350K .......... .......... .......... .......... .......... 24% 15.5M 35s
126400K .......... .......... .......... .......... .......... 24% 17.3M 35s
126450K .......... .......... .......... .......... .......... 24% 16.8M 35s
126500K .......... .......... .......... .......... .......... 24% 14.4M 35s
126550K .......... .......... .......... .......... .......... 24% 10.8M 35s
126600K .......... .......... .......... .......... .......... 24% 14.5M 35s
126650K .......... .......... .......... .......... .......... 24% 11.7M 35s
126700K .......... .......... .......... .......... .......... 24% 9.61M 35s
126750K .......... .......... .......... .......... .......... 24% 11.3M 35s
126800K .......... .......... .......... .......... .......... 24% 11.8M 35s
126850K .......... .......... .......... .......... .......... 24% 9.07M 35s
126900K .......... .......... .......... .......... .......... 24% 10.2M 35s
126950K .......... .......... .......... .......... .......... 24% 10.4M 35s
127000K .......... .......... .......... .......... .......... 24% 11.0M 35s
127050K .......... .......... .......... .......... .......... 24% 11.4M 35s
127100K .......... .......... .......... .......... .......... 25% 9.37M 35s
127150K .......... .......... .......... .......... .......... 25% 7.62M 35s
127200K .......... .......... .......... .......... .......... 25% 9.19M 35s
127250K .......... .......... .......... .......... .......... 25% 9.83M 35s
127300K .......... .......... .......... .......... .......... 25% 8.69M 35s
127350K .......... .......... .......... .......... .......... 25% 9.77M 35s
127400K .......... .......... .......... .......... .......... 25% 8.26M 35s
127450K .......... .......... .......... .......... .......... 25% 9.52M 35s
127500K .......... .......... .......... .......... .......... 25% 9.22M 35s
127550K .......... .......... .......... .......... .......... 25% 9.49M 35s
127600K .......... .......... .......... .......... .......... 25% 7.70M 35s
127650K .......... .......... .......... .......... .......... 25% 19.4M 35s
127700K .......... .......... .......... .......... .......... 25% 16.4M 35s
127750K .......... .......... .......... .......... .......... 25% 94.3M 35s
127800K .......... .......... .......... .......... .......... 25% 82.6M 35s
127850K .......... .......... .......... .......... .......... 25% 17.8M 35s
127900K .......... .......... .......... .......... .......... 25%  182M 35s
127950K .......... .......... .......... .......... .......... 25% 24.8M 35s
128000K .......... .......... .......... .......... .......... 25% 34.0M 35s
128050K .......... .......... .......... .......... .......... 25% 29.8M 35s
128100K .......... .......... .......... .......... .......... 25% 26.8M 35s
128150K .......... .......... .......... .......... .......... 25% 25.2M 35s
128200K .......... .......... .......... .......... .......... 25% 25.3M 35s
128250K .......... .......... .......... .......... .......... 25% 27.1M 35s
128300K .......... .......... .......... .......... .......... 25% 23.2M 35s
128350K .......... .......... .......... .......... .......... 25% 21.6M 35s
128400K .......... .......... .......... .......... .......... 25% 25.7M 35s
128450K .......... .......... .......... .......... .......... 25% 20.3M 35s
128500K .......... .......... .......... .......... .......... 25% 24.5M 35s
128550K .......... .......... .......... .......... .......... 25% 25.1M 35s
128600K .......... .......... .......... .......... .......... 25% 18.4M 35s
128650K .......... .......... .......... .......... .......... 25% 20.4M 35s
128700K .......... .......... .......... .......... .......... 25% 15.4M 35s
128750K .......... .......... .......... .......... .......... 25% 16.0M 35s
128800K .......... .......... .......... .......... .......... 25% 23.4M 35s
128850K .......... .......... .......... .......... .......... 25% 15.8M 35s
128900K .......... .......... .......... .......... .......... 25% 15.2M 35s
128950K .......... .......... .......... .......... .......... 25% 14.9M 35s
129000K .......... .......... .......... .......... .......... 25% 13.1M 35s
129050K .......... .......... .......... .......... .......... 25% 23.3M 35s
129100K .......... .......... .......... .......... .......... 25% 14.9M 35s
129150K .......... .......... .......... .......... .......... 25% 13.7M 35s
129200K .......... .......... .......... .......... .......... 25% 16.0M 35s
129250K .......... .......... .......... .......... .......... 25% 41.2M 35s
129300K .......... .......... .......... .......... .......... 25% 33.2M 35s
129350K .......... .......... .......... .......... .......... 25% 22.3M 35s
129400K .......... .......... .......... .......... .......... 25% 48.5M 35s
129450K .......... .......... .......... .......... .......... 25% 48.9M 35s
129500K .......... .......... .......... .......... .......... 25% 22.4M 35s
129550K .......... .......... .......... .......... .......... 25% 31.2M 35s
129600K .......... .......... .......... .......... .......... 25% 18.7M 35s
129650K .......... .......... .......... .......... .......... 25% 13.9M 35s
129700K .......... .......... .......... .......... .......... 25% 10.9M 35s
129750K .......... .......... .......... .......... .......... 25% 12.2M 35s
129800K .......... .......... .......... .......... .......... 25% 8.76M 35s
129850K .......... .......... .......... .......... .......... 25% 7.60M 35s
129900K .......... .......... .......... .......... .......... 25% 8.16M 35s
129950K .......... .......... .......... .......... .......... 25% 7.97M 35s
130000K .......... .......... .......... .......... .......... 25% 9.89M 35s
130050K .......... .......... .......... .......... .......... 25% 9.32M 35s
130100K .......... .......... .......... .......... .......... 25% 6.53M 35s
130150K .......... .......... .......... .......... .......... 25% 8.41M 35s
130200K .......... .......... .......... .......... .......... 25% 8.09M 35s
130250K .......... .......... .......... .......... .......... 25% 9.30M 35s
130300K .......... .......... .......... .......... .......... 25% 9.14M 35s
130350K .......... .......... .......... .......... .......... 25% 7.23M 35s
130400K .......... .......... .......... .......... .......... 25% 10.6M 35s
130450K .......... .......... .......... .......... .......... 25% 11.7M 34s
130500K .......... .......... .......... .......... .......... 25% 14.1M 34s
130550K .......... .......... .......... .......... .......... 25% 15.3M 34s
130600K .......... .......... .......... .......... .......... 25% 7.13M 34s
130650K .......... .......... .......... .......... .......... 25% 7.56M 34s
130700K .......... .......... .......... .......... .......... 25% 5.89M 34s
130750K .......... .......... .......... .......... .......... 25% 6.59M 34s
130800K .......... .......... .......... .......... .......... 25% 7.30M 34s
130850K .......... .......... .......... .......... .......... 25% 7.07M 34s
130900K .......... .......... .......... .......... .......... 25% 19.9M 34s
130950K .......... .......... .......... .......... .......... 25% 23.0M 34s
131000K .......... .......... .......... .......... .......... 25% 18.7M 34s
131050K .......... .......... .......... .......... .......... 25% 27.3M 34s
131100K .......... .......... .......... .......... .......... 25% 17.3M 34s
131150K .......... .......... .......... .......... .......... 25% 20.1M 34s
131200K .......... .......... .......... .......... .......... 25% 16.8M 34s
131250K .......... .......... .......... .......... .......... 25% 17.1M 34s
131300K .......... .......... .......... .......... .......... 25% 23.5M 34s
131350K .......... .......... .......... .......... .......... 25% 17.0M 34s
131400K .......... .......... .......... .......... .......... 25% 14.9M 34s
131450K .......... .......... .......... .......... .......... 25% 15.5M 34s
131500K .......... .......... .......... .......... .......... 25% 16.5M 34s
131550K .......... .......... .......... .......... .......... 25% 17.1M 34s
131600K .......... .......... .......... .......... .......... 25% 12.9M 34s
131650K .......... .......... .......... .......... .......... 25% 18.6M 34s
131700K .......... .......... .......... .......... .......... 25% 13.0M 34s
131750K .......... .......... .......... .......... .......... 25% 16.3M 34s
131800K .......... .......... .......... .......... .......... 25% 17.4M 34s
131850K .......... .......... .......... .......... .......... 25% 12.2M 34s
131900K .......... .......... .......... .......... .......... 25% 12.5M 34s
131950K .......... .......... .......... .......... .......... 25% 5.63M 34s
132000K .......... .......... .......... .......... .......... 25% 7.43M 34s
132050K .......... .......... .......... .......... .......... 25% 7.07M 34s
132100K .......... .......... .......... .......... .......... 25% 6.34M 34s
132150K .......... .......... .......... .......... .......... 26% 7.24M 34s
132200K .......... .......... .......... .......... .......... 26% 4.94M 34s
132250K .......... .......... .......... .......... .......... 26% 6.34M 34s
132300K .......... .......... .......... .......... .......... 26% 5.43M 34s
132350K .......... .......... .......... .......... .......... 26% 4.35M 34s
132400K .......... .......... .......... .......... .......... 26% 5.92M 34s
132450K .......... .......... .......... .......... .......... 26% 4.49M 34s
132500K .......... .......... .......... .......... .......... 26% 11.7M 34s
132550K .......... .......... .......... .......... .......... 26% 12.1M 34s
132600K .......... .......... .......... .......... .......... 26% 10.7M 34s
132650K .......... .......... .......... .......... .......... 26% 11.4M 34s
132700K .......... .......... .......... .......... .......... 26% 11.0M 34s
132750K .......... .......... .......... .......... .......... 26% 11.8M 34s
132800K .......... .......... .......... .......... .......... 26% 10.7M 34s
132850K .......... .......... .......... .......... .......... 26% 8.07M 34s
132900K .......... .......... .......... .......... .......... 26% 8.33M 34s
132950K .......... .......... .......... .......... .......... 26% 6.35M 34s
133000K .......... .......... .......... .......... .......... 26% 6.74M 34s
133050K .......... .......... .......... .......... .......... 26% 7.82M 34s
133100K .......... .......... .......... .......... .......... 26% 6.30M 34s
133150K .......... .......... .......... .......... .......... 26% 5.64M 34s
133200K .......... .......... .......... .......... .......... 26% 4.82M 34s
133250K .......... .......... .......... .......... .......... 26% 3.94M 34s
133300K .......... .......... .......... .......... .......... 26% 3.65M 34s
133350K .......... .......... .......... .......... .......... 26% 4.37M 34s
133400K .......... .......... .......... .......... .......... 26% 4.51M 34s
133450K .......... .......... .......... .......... .......... 26% 5.90M 34s
133500K .......... .......... .......... .......... .......... 26% 7.38M 34s
133550K .......... .......... .......... .......... .......... 26% 7.64M 34s
133600K .......... .......... .......... .......... .......... 26% 8.11M 34s
133650K .......... .......... .......... .......... .......... 26% 8.43M 34s
133700K .......... .......... .......... .......... .......... 26% 8.03M 34s
133750K .......... .......... .......... .......... .......... 26% 7.73M 34s
133800K .......... .......... .......... .......... .......... 26% 9.96M 34s
133850K .......... .......... .......... .......... .......... 26% 6.32M 34s
133900K .......... .......... .......... .......... .......... 26% 6.18M 34s
133950K .......... .......... .......... .......... .......... 26% 8.17M 34s
134000K .......... .......... .......... .......... .......... 26% 9.93M 34s
134050K .......... .......... .......... .......... .......... 26% 9.62M 34s
134100K .......... .......... .......... .......... .......... 26% 6.52M 34s
134150K .......... .......... .......... .......... .......... 26% 6.89M 34s
134200K .......... .......... .......... .......... .......... 26% 5.79M 34s
134250K .......... .......... .......... .......... .......... 26% 6.25M 34s
134300K .......... .......... .......... .......... .......... 26% 6.16M 34s
134350K .......... .......... .......... .......... .......... 26% 8.71M 34s
134400K .......... .......... .......... .......... .......... 26% 11.6M 34s
134450K .......... .......... .......... .......... .......... 26% 11.8M 34s
134500K .......... .......... .......... .......... .......... 26% 13.4M 34s
134550K .......... .......... .......... .......... .......... 26% 12.2M 34s
134600K .......... .......... .......... .......... .......... 26% 11.3M 34s
134650K .......... .......... .......... .......... .......... 26% 14.1M 34s
134700K .......... .......... .......... .......... .......... 26% 12.7M 34s
134750K .......... .......... .......... .......... .......... 26% 13.1M 34s
134800K .......... .......... .......... .......... .......... 26% 29.0M 34s
134850K .......... .......... .......... .......... .......... 26% 26.0M 34s
134900K .......... .......... .......... .......... .......... 26% 23.1M 34s
134950K .......... .......... .......... .......... .......... 26% 60.4M 34s
135000K .......... .......... .......... .......... .......... 26%  128M 34s
135050K .......... .......... .......... .......... .......... 26% 22.5M 34s
135100K .......... .......... .......... .......... .......... 26% 15.4M 34s
135150K .......... .......... .......... .......... .......... 26% 15.7M 34s
135200K .......... .......... .......... .......... .......... 26% 20.9M 34s
135250K .......... .......... .......... .......... .......... 26% 17.0M 34s
135300K .......... .......... .......... .......... .......... 26% 15.5M 34s
135350K .......... .......... .......... .......... .......... 26% 15.7M 34s
135400K .......... .......... .......... .......... .......... 26% 17.0M 34s
135450K .......... .......... .......... .......... .......... 26% 14.6M 34s
135500K .......... .......... .......... .......... .......... 26% 13.5M 34s
135550K .......... .......... .......... .......... .......... 26% 18.1M 34s
135600K .......... .......... .......... .......... .......... 26% 12.7M 34s
135650K .......... .......... .......... .......... .......... 26% 12.1M 34s
135700K .......... .......... .......... .......... .......... 26% 16.8M 34s
135750K .......... .......... .......... .......... .......... 26% 14.8M 34s
135800K .......... .......... .......... .......... .......... 26% 11.4M 34s
135850K .......... .......... .......... .......... .......... 26% 14.5M 34s
135900K .......... .......... .......... .......... .......... 26% 14.8M 34s
135950K .......... .......... .......... .......... .......... 26% 11.4M 34s
136000K .......... .......... .......... .......... .......... 26% 14.8M 34s
136050K .......... .......... .......... .......... .......... 26% 15.6M 34s
136100K .......... .......... .......... .......... .......... 26% 10.1M 34s
136150K .......... .......... .......... .......... .......... 26% 14.5M 34s
136200K .......... .......... .......... .......... .......... 26% 23.1M 34s
136250K .......... .......... .......... .......... .......... 26% 35.3M 34s
136300K .......... .......... .......... .......... .......... 26% 36.0M 34s
136350K .......... .......... .......... .......... .......... 26% 22.7M 34s
136400K .......... .......... .......... .......... .......... 26% 23.7M 34s
136450K .......... .......... .......... .......... .......... 26% 26.0M 34s
136500K .......... .......... .......... .......... .......... 26% 28.8M 34s
136550K .......... .......... .......... .......... .......... 26% 22.3M 34s
136600K .......... .......... .......... .......... .......... 26% 11.5M 34s
136650K .......... .......... .......... .......... .......... 26% 22.1M 34s
136700K .......... .......... .......... .......... .......... 26% 12.4M 34s
136750K .......... .......... .......... .......... .......... 26% 13.2M 34s
136800K .......... .......... .......... .......... .......... 26% 14.9M 34s
136850K .......... .......... .......... .......... .......... 26% 13.3M 34s
136900K .......... .......... .......... .......... .......... 26% 12.6M 34s
136950K .......... .......... .......... .......... .......... 26% 10.2M 34s
137000K .......... .......... .......... .......... .......... 26% 13.1M 34s
137050K .......... .......... .......... .......... .......... 26% 11.2M 34s
137100K .......... .......... .......... .......... .......... 26% 13.4M 34s
137150K .......... .......... .......... .......... .......... 26% 10.7M 34s
137200K .......... .......... .......... .......... .......... 26% 11.2M 34s
137250K .......... .......... .......... .......... .......... 27% 12.8M 34s
137300K .......... .......... .......... .......... .......... 27% 11.8M 34s
137350K .......... .......... .......... .......... .......... 27% 12.4M 34s
137400K .......... .......... .......... .......... .......... 27% 11.1M 34s
137450K .......... .......... .......... .......... .......... 27% 16.9M 34s
137500K .......... .......... .......... .......... .......... 27% 13.2M 34s
137550K .......... .......... .......... .......... .......... 27% 17.3M 34s
137600K .......... .......... .......... .......... .......... 27% 9.62M 34s
137650K .......... .......... .......... .......... .......... 27% 16.9M 34s
137700K .......... .......... .......... .......... .......... 27% 11.9M 34s
137750K .......... .......... .......... .......... .......... 27% 14.4M 34s
137800K .......... .......... .......... .......... .......... 27% 17.2M 34s
137850K .......... .......... .......... .......... .......... 27% 11.0M 34s
137900K .......... .......... .......... .......... .......... 27% 15.5M 34s
137950K .......... .......... .......... .......... .......... 27% 12.5M 34s
138000K .......... .......... .......... .......... .......... 27% 14.2M 34s
138050K .......... .......... .......... .......... .......... 27% 17.1M 34s
138100K .......... .......... .......... .......... .......... 27% 13.2M 34s
138150K .......... .......... .......... .......... .......... 27% 16.1M 34s
138200K .......... .......... .......... .......... .......... 27% 21.4M 34s
138250K .......... .......... .......... .......... .......... 27% 15.4M 34s
138300K .......... .......... .......... .......... .......... 27% 21.1M 34s
138350K .......... .......... .......... .......... .......... 27% 15.3M 34s
138400K .......... .......... .......... .......... .......... 27% 15.4M 34s
138450K .......... .......... .......... .......... .......... 27% 13.2M 34s
138500K .......... .......... .......... .......... .......... 27% 10.7M 34s
138550K .......... .......... .......... .......... .......... 27% 15.7M 34s
138600K .......... .......... .......... .......... .......... 27% 11.6M 34s
138650K .......... .......... .......... .......... .......... 27% 14.5M 34s
138700K .......... .......... .......... .......... .......... 27% 12.4M 34s
138750K .......... .......... .......... .......... .......... 27% 10.9M 34s
138800K .......... .......... .......... .......... .......... 27% 11.4M 34s
138850K .......... .......... .......... .......... .......... 27% 9.25M 34s
138900K .......... .......... .......... .......... .......... 27% 8.52M 34s
138950K .......... .......... .......... .......... .......... 27% 6.36M 34s
139000K .......... .......... .......... .......... .......... 27% 8.55M 34s
139050K .......... .......... .......... .......... .......... 27% 8.87M 34s
139100K .......... .......... .......... .......... .......... 27% 8.23M 34s
139150K .......... .......... .......... .......... .......... 27% 8.61M 34s
139200K .......... .......... .......... .......... .......... 27% 6.95M 34s
139250K .......... .......... .......... .......... .......... 27% 14.7M 34s
139300K .......... .......... .......... .......... .......... 27% 14.5M 34s
139350K .......... .......... .......... .......... .......... 27% 11.3M 34s
139400K .......... .......... .......... .......... .......... 27% 10.8M 34s
139450K .......... .......... .......... .......... .......... 27% 9.67M 34s
139500K .......... .......... .......... .......... .......... 27% 14.6M 34s
139550K .......... .......... .......... .......... .......... 27% 9.40M 34s
139600K .......... .......... .......... .......... .......... 27% 13.9M 34s
139650K .......... .......... .......... .......... .......... 27% 11.6M 34s
139700K .......... .......... .......... .......... .......... 27% 8.86M 34s
139750K .......... .......... .......... .......... .......... 27% 8.84M 34s
139800K .......... .......... .......... .......... .......... 27% 9.10M 34s
139850K .......... .......... .......... .......... .......... 27% 9.24M 34s
139900K .......... .......... .......... .......... .......... 27% 7.53M 34s
139950K .......... .......... .......... .......... .......... 27% 7.63M 34s
140000K .......... .......... .......... .......... .......... 27% 8.26M 34s
140050K .......... .......... .......... .......... .......... 27% 9.07M 34s
140100K .......... .......... .......... .......... .......... 27% 8.00M 34s
140150K .......... .......... .......... .......... .......... 27% 8.69M 34s
140200K .......... .......... .......... .......... .......... 27% 6.80M 34s
140250K .......... .......... .......... .......... .......... 27% 5.03M 34s
140300K .......... .......... .......... .......... .......... 27% 6.43M 34s
140350K .......... .......... .......... .......... .......... 27% 5.49M 34s
140400K .......... .......... .......... .......... .......... 27% 8.89M 34s
140450K .......... .......... .......... .......... .......... 27% 16.2M 34s
140500K .......... .......... .......... .......... .......... 27% 26.5M 34s
140550K .......... .......... .......... .......... .......... 27% 19.5M 34s
140600K .......... .......... .......... .......... .......... 27% 17.0M 34s
140650K .......... .......... .......... .......... .......... 27% 13.6M 34s
140700K .......... .......... .......... .......... .......... 27% 9.12M 34s
140750K .......... .......... .......... .......... .......... 27% 11.4M 34s
140800K .......... .......... .......... .......... .......... 27% 9.40M 34s
140850K .......... .......... .......... .......... .......... 27% 7.35M 34s
140900K .......... .......... .......... .......... .......... 27% 9.37M 34s
140950K .......... .......... .......... .......... .......... 27% 8.03M 34s
141000K .......... .......... .......... .......... .......... 27% 10.9M 34s
141050K .......... .......... .......... .......... .......... 27% 23.1M 34s
141100K .......... .......... .......... .......... .......... 27% 26.9M 34s
141150K .......... .......... .......... .......... .......... 27% 29.9M 34s
141200K .......... .......... .......... .......... .......... 27% 29.3M 34s
141250K .......... .......... .......... .......... .......... 27% 19.0M 34s
141300K .......... .......... .......... .......... .......... 27%  131M 34s
141350K .......... .......... .......... .......... .......... 27% 17.1M 34s
141400K .......... .......... .......... .......... .......... 27% 17.8M 34s
141450K .......... .......... .......... .......... .......... 27% 9.76M 34s
141500K .......... .......... .......... .......... .......... 27% 12.5M 34s
141550K .......... .......... .......... .......... .......... 27% 8.05M 34s
141600K .......... .......... .......... .......... .......... 27% 5.43M 34s
141650K .......... .......... .......... .......... .......... 27% 6.15M 34s
141700K .......... .......... .......... .......... .......... 27% 5.11M 34s
141750K .......... .......... .......... .......... .......... 27% 9.35M 34s
141800K .......... .......... .......... .......... .......... 27% 9.34M 34s
141850K .......... .......... .......... .......... .......... 27% 9.64M 34s
141900K .......... .......... .......... .......... .......... 27% 9.67M 34s
141950K .......... .......... .......... .......... .......... 27% 7.83M 34s
142000K .......... .......... .......... .......... .......... 27% 9.96M 34s
142050K .......... .......... .......... .......... .......... 27% 11.8M 34s
142100K .......... .......... .......... .......... .......... 27% 22.6M 34s
142150K .......... .......... .......... .......... .......... 27% 90.1M 33s
142200K .......... .......... .......... .......... .......... 27% 21.3M 33s
142250K .......... .......... .......... .......... .......... 27% 24.4M 33s
142300K .......... .......... .......... .......... .......... 27% 24.1M 33s
142350K .......... .......... .......... .......... .......... 28% 21.8M 33s
142400K .......... .......... .......... .......... .......... 28% 21.7M 33s
142450K .......... .......... .......... .......... .......... 28% 12.8M 33s
142500K .......... .......... .......... .......... .......... 28% 18.4M 33s
142550K .......... .......... .......... .......... .......... 28% 12.0M 33s
142600K .......... .......... .......... .......... .......... 28% 11.0M 33s
142650K .......... .......... .......... .......... .......... 28% 14.0M 33s
142700K .......... .......... .......... .......... .......... 28% 8.92M 33s
142750K .......... .......... .......... .......... .......... 28% 9.02M 33s
142800K .......... .......... .......... .......... .......... 28% 8.83M 33s
142850K .......... .......... .......... .......... .......... 28% 7.18M 33s
142900K .......... .......... .......... .......... .......... 28% 6.63M 33s
142950K .......... .......... .......... .......... .......... 28% 4.51M 33s
143000K .......... .......... .......... .......... .......... 28% 10.2M 33s
143050K .......... .......... .......... .......... .......... 28% 8.84M 33s
143100K .......... .......... .......... .......... .......... 28% 9.59M 33s
143150K .......... .......... .......... .......... .......... 28% 10.7M 33s
143200K .......... .......... .......... .......... .......... 28% 11.2M 33s
143250K .......... .......... .......... .......... .......... 28% 8.67M 33s
143300K .......... .......... .......... .......... .......... 28% 12.2M 33s
143350K .......... .......... .......... .......... .......... 28% 9.58M 33s
143400K .......... .......... .......... .......... .......... 28% 10.8M 33s
143450K .......... .......... .......... .......... .......... 28% 7.85M 33s
143500K .......... .......... .......... .......... .......... 28% 10.1M 33s
143550K .......... .......... .......... .......... .......... 28% 8.47M 33s
143600K .......... .......... .......... .......... .......... 28% 8.69M 33s
143650K .......... .......... .......... .......... .......... 28% 9.27M 33s
143700K .......... .......... .......... .......... .......... 28% 7.25M 33s
143750K .......... .......... .......... .......... .......... 28% 8.65M 33s
143800K .......... .......... .......... .......... .......... 28% 26.3M 33s
143850K .......... .......... .......... .......... .......... 28% 13.8M 33s
143900K .......... .......... .......... .......... .......... 28% 16.4M 33s
143950K .......... .......... .......... .......... .......... 28% 11.7M 33s
144000K .......... .......... .......... .......... .......... 28% 12.6M 33s
144050K .......... .......... .......... .......... .......... 28% 11.2M 33s
144100K .......... .......... .......... .......... .......... 28% 9.49M 33s
144150K .......... .......... .......... .......... .......... 28% 11.4M 33s
144200K .......... .......... .......... .......... .......... 28% 11.4M 33s
144250K .......... .......... .......... .......... .......... 28% 15.3M 33s
144300K .......... .......... .......... .......... .......... 28% 11.1M 33s
144350K .......... .......... .......... .......... .......... 28% 11.7M 33s
144400K .......... .......... .......... .......... .......... 28% 11.7M 33s
144450K .......... .......... .......... .......... .......... 28% 12.4M 33s
144500K .......... .......... .......... .......... .......... 28% 12.2M 33s
144550K .......... .......... .......... .......... .......... 28% 8.38M 33s
144600K .......... .......... .......... .......... .......... 28% 10.0M 33s
144650K .......... .......... .......... .......... .......... 28% 9.62M 33s
144700K .......... .......... .......... .......... .......... 28% 9.88M 33s
144750K .......... .......... .......... .......... .......... 28% 8.84M 33s
144800K .......... .......... .......... .......... .......... 28% 6.40M 33s
144850K .......... .......... .......... .......... .......... 28% 5.65M 33s
144900K .......... .......... .......... .......... .......... 28% 7.04M 33s
144950K .......... .......... .......... .......... .......... 28% 5.10M 33s
145000K .......... .......... .......... .......... .......... 28% 6.24M 33s
145050K .......... .......... .......... .......... .......... 28% 7.54M 33s
145100K .......... .......... .......... .......... .......... 28% 6.85M 33s
145150K .......... .......... .......... .......... .......... 28% 7.63M 33s
145200K .......... .......... .......... .......... .......... 28% 6.18M 33s
145250K .......... .......... .......... .......... .......... 28% 10.7M 33s
145300K .......... .......... .......... .......... .......... 28% 10.6M 33s
145350K .......... .......... .......... .......... .......... 28% 17.3M 33s
145400K .......... .......... .......... .......... .......... 28% 14.2M 33s
145450K .......... .......... .......... .......... .......... 28% 15.6M 33s
145500K .......... .......... .......... .......... .......... 28% 12.7M 33s
145550K .......... .......... .......... .......... .......... 28% 10.4M 33s
145600K .......... .......... .......... .......... .......... 28% 7.26M 33s
145650K .......... .......... .......... .......... .......... 28% 9.37M 33s
145700K .......... .......... .......... .......... .......... 28% 9.05M 33s
145750K .......... .......... .......... .......... .......... 28% 10.4M 33s
145800K .......... .......... .......... .......... .......... 28% 11.9M 33s
145850K .......... .......... .......... .......... .......... 28% 8.30M 33s
145900K .......... .......... .......... .......... .......... 28% 15.7M 33s
145950K .......... .......... .......... .......... .......... 28% 22.2M 33s
146000K .......... .......... .......... .......... .......... 28% 42.5M 33s
146050K .......... .......... .......... .......... .......... 28% 34.8M 33s
146100K .......... .......... .......... .......... .......... 28% 31.0M 33s
146150K .......... .......... .......... .......... .......... 28% 32.9M 33s
146200K .......... .......... .......... .......... .......... 28% 17.3M 33s
146250K .......... .......... .......... .......... .......... 28% 13.4M 33s
146300K .......... .......... .......... .......... .......... 28% 27.1M 33s
146350K .......... .......... .......... .......... .......... 28% 14.0M 33s
146400K .......... .......... .......... .......... .......... 28% 15.3M 33s
146450K .......... .......... .......... .......... .......... 28% 11.1M 33s
146500K .......... .......... .......... .......... .......... 28% 16.1M 33s
146550K .......... .......... .......... .......... .......... 28% 12.6M 33s
146600K .......... .......... .......... .......... .......... 28% 12.7M 33s
146650K .......... .......... .......... .......... .......... 28% 11.8M 33s
146700K .......... .......... .......... .......... .......... 28% 10.6M 33s
146750K .......... .......... .......... .......... .......... 28% 10.8M 33s
146800K .......... .......... .......... .......... .......... 28% 10.2M 33s
146850K .......... .......... .......... .......... .......... 28% 8.76M 33s
146900K .......... .......... .......... .......... .......... 28% 7.02M 33s
146950K .......... .......... .......... .......... .......... 28% 5.63M 33s
147000K .......... .......... .......... .......... .......... 28% 10.4M 33s
147050K .......... .......... .......... .......... .......... 28% 9.60M 33s
147100K .......... .......... .......... .......... .......... 28% 9.42M 33s
147150K .......... .......... .......... .......... .......... 28% 7.84M 33s
147200K .......... .......... .......... .......... .......... 28% 4.82M 33s
147250K .......... .......... .......... .......... .......... 28% 5.68M 33s
147300K .......... .......... .......... .......... .......... 28% 6.27M 33s
147350K .......... .......... .......... .......... .......... 28% 5.13M 33s
147400K .......... .......... .......... .......... .......... 29% 16.4M 33s
147450K .......... .......... .......... .......... .......... 29% 31.9M 33s
147500K .......... .......... .......... .......... .......... 29% 21.4M 33s
147550K .......... .......... .......... .......... .......... 29% 18.1M 33s
147600K .......... .......... .......... .......... .......... 29% 13.4M 33s
147650K .......... .......... .......... .......... .......... 29% 12.2M 33s
147700K .......... .......... .......... .......... .......... 29% 13.2M 33s
147750K .......... .......... .......... .......... .......... 29% 13.8M 33s
147800K .......... .......... .......... .......... .......... 29% 15.1M 33s
147850K .......... .......... .......... .......... .......... 29% 13.1M 33s
147900K .......... .......... .......... .......... .......... 29% 12.2M 33s
147950K .......... .......... .......... .......... .......... 29% 9.56M 33s
148000K .......... .......... .......... .......... .......... 29% 12.9M 33s
148050K .......... .......... .......... .......... .......... 29% 9.44M 33s
148100K .......... .......... .......... .......... .......... 29% 15.4M 33s
148150K .......... .......... .......... .......... .......... 29% 13.3M 33s
148200K .......... .......... .......... .......... .......... 29% 11.1M 33s
148250K .......... .......... .......... .......... .......... 29% 15.8M 33s
148300K .......... .......... .......... .......... .......... 29% 13.0M 33s
148350K .......... .......... .......... .......... .......... 29% 12.2M 33s
148400K .......... .......... .......... .......... .......... 29% 15.6M 33s
148450K .......... .......... .......... .......... .......... 29% 15.5M 33s
148500K .......... .......... .......... .......... .......... 29% 38.7M 33s
148550K .......... .......... .......... .......... .......... 29% 40.9M 33s
148600K .......... .......... .......... .......... .......... 29% 33.3M 33s
148650K .......... .......... .......... .......... .......... 29% 38.2M 33s
148700K .......... .......... .......... .......... .......... 29% 59.4M 33s
148750K .......... .......... .......... .......... .......... 29% 31.7M 33s
148800K .......... .......... .......... .......... .......... 29% 29.6M 33s
148850K .......... .......... .......... .......... .......... 29% 28.3M 33s
148900K .......... .......... .......... .......... .......... 29% 25.3M 33s
148950K .......... .......... .......... .......... .......... 29% 24.6M 33s
149000K .......... .......... .......... .......... .......... 29% 33.7M 33s
149050K .......... .......... .......... .......... .......... 29% 26.9M 33s
149100K .......... .......... .......... .......... .......... 29% 19.6M 33s
149150K .......... .......... .......... .......... .......... 29% 23.4M 33s
149200K .......... .......... .......... .......... .......... 29% 16.6M 33s
149250K .......... .......... .......... .......... .......... 29% 18.4M 33s
149300K .......... .......... .......... .......... .......... 29% 16.7M 33s
149350K .......... .......... .......... .......... .......... 29% 16.1M 33s
149400K .......... .......... .......... .......... .......... 29% 16.0M 33s
149450K .......... .......... .......... .......... .......... 29% 16.1M 33s
149500K .......... .......... .......... .......... .......... 29% 13.8M 33s
149550K .......... .......... .......... .......... .......... 29% 11.8M 33s
149600K .......... .......... .......... .......... .......... 29% 7.31M 33s
149650K .......... .......... .......... .......... .......... 29% 5.13M 33s
149700K .......... .......... .......... .......... .......... 29% 10.8M 33s
149750K .......... .......... .......... .......... .......... 29% 9.54M 33s
149800K .......... .......... .......... .......... .......... 29% 9.72M 33s
149850K .......... .......... .......... .......... .......... 29% 7.52M 33s
149900K .......... .......... .......... .......... .......... 29% 10.5M 33s
149950K .......... .......... .......... .......... .......... 29% 8.52M 33s
150000K .......... .......... .......... .......... .......... 29% 9.54M 33s
150050K .......... .......... .......... .......... .......... 29% 9.80M 33s
150100K .......... .......... .......... .......... .......... 29% 8.24M 33s
150150K .......... .......... .......... .......... .......... 29% 9.04M 33s
150200K .......... .......... .......... .......... .......... 29% 15.7M 33s
150250K .......... .......... .......... .......... .......... 29% 14.8M 33s
150300K .......... .......... .......... .......... .......... 29% 13.2M 33s
150350K .......... .......... .......... .......... .......... 29% 9.87M 33s
150400K .......... .......... .......... .......... .......... 29% 13.3M 33s
150450K .......... .......... .......... .......... .......... 29% 12.0M 33s
150500K .......... .......... .......... .......... .......... 29% 11.2M 33s
150550K .......... .......... .......... .......... .......... 29% 11.4M 33s
150600K .......... .......... .......... .......... .......... 29% 12.3M 33s
150650K .......... .......... .......... .......... .......... 29% 13.0M 33s
150700K .......... .......... .......... .......... .......... 29% 13.2M 33s
150750K .......... .......... .......... .......... .......... 29% 24.1M 33s
150800K .......... .......... .......... .......... .......... 29% 33.2M 33s
150850K .......... .......... .......... .......... .......... 29% 21.2M 33s
150900K .......... .......... .......... .......... .......... 29% 11.8M 33s
150950K .......... .......... .......... .......... .......... 29% 8.06M 33s
151000K .......... .......... .......... .......... .......... 29% 11.3M 33s
151050K .......... .......... .......... .......... .......... 29% 8.35M 33s
151100K .......... .......... .......... .......... .......... 29% 6.80M 33s
151150K .......... .......... .......... .......... .......... 29% 4.85M 33s
151200K .......... .......... .......... .......... .......... 29% 4.85M 33s
151250K .......... .......... .......... .......... .......... 29% 6.23M 33s
151300K .......... .......... .......... .......... .......... 29% 6.63M 33s
151350K .......... .......... .......... .......... .......... 29% 5.50M 33s
151400K .......... .......... .......... .......... .......... 29% 15.3M 33s
151450K .......... .......... .......... .......... .......... 29% 12.9M 33s
151500K .......... .......... .......... .......... .......... 29% 19.8M 33s
151550K .......... .......... .......... .......... .......... 29% 14.7M 33s
151600K .......... .......... .......... .......... .......... 29% 11.3M 33s
151650K .......... .......... .......... .......... .......... 29% 13.3M 33s
151700K .......... .......... .......... .......... .......... 29% 11.3M 33s
151750K .......... .......... .......... .......... .......... 29% 11.1M 33s
151800K .......... .......... .......... .......... .......... 29% 11.8M 33s
151850K .......... .......... .......... .......... .......... 29% 11.8M 33s
151900K .......... .......... .......... .......... .......... 29% 10.8M 33s
151950K .......... .......... .......... .......... .......... 29% 13.0M 33s
152000K .......... .......... .......... .......... .......... 29% 16.0M 33s
152050K .......... .......... .......... .......... .......... 29% 16.4M 33s
152100K .......... .......... .......... .......... .......... 29% 12.8M 32s
152150K .......... .......... .......... .......... .......... 29% 14.4M 32s
152200K .......... .......... .......... .......... .......... 29% 13.7M 32s
152250K .......... .......... .......... .......... .......... 29% 14.1M 32s
152300K .......... .......... .......... .......... .......... 29% 15.1M 32s
152350K .......... .......... .......... .......... .......... 29% 11.9M 32s
152400K .......... .......... .......... .......... .......... 29% 14.9M 32s
152450K .......... .......... .......... .......... .......... 29% 34.6M 32s
152500K .......... .......... .......... .......... .......... 30% 23.4M 32s
152550K .......... .......... .......... .......... .......... 30% 30.6M 32s
152600K .......... .......... .......... .......... .......... 30% 37.9M 32s
152650K .......... .......... .......... .......... .......... 30% 36.0M 32s
152700K .......... .......... .......... .......... .......... 30% 21.5M 32s
152750K .......... .......... .......... .......... .......... 30% 14.0M 32s
152800K .......... .......... .......... .......... .......... 30% 14.7M 32s
152850K .......... .......... .......... .......... .......... 30% 9.50M 32s
152900K .......... .......... .......... .......... .......... 30% 15.8M 32s
152950K .......... .......... .......... .......... .......... 30% 9.52M 32s
153000K .......... .......... .......... .......... .......... 30% 11.2M 32s
153050K .......... .......... .......... .......... .......... 30% 12.5M 32s
153100K .......... .......... .......... .......... .......... 30% 6.64M 32s
153150K .......... .......... .......... .......... .......... 30% 9.13M 32s
153200K .......... .......... .......... .......... .......... 30% 7.07M 32s
153250K .......... .......... .......... .......... .......... 30% 9.44M 32s
153300K .......... .......... .......... .......... .......... 30% 6.02M 32s
153350K .......... .......... .......... .......... .......... 30% 4.35M 32s
153400K .......... .......... .......... .......... .......... 30% 5.89M 32s
153450K .......... .......... .......... .......... .......... 30% 5.33M 32s
153500K .......... .......... .......... .......... .......... 30% 5.04M 32s
153550K .......... .......... .......... .......... .......... 30% 9.68M 32s
153600K .......... .......... .......... .......... .......... 30% 7.56M 32s
153650K .......... .......... .......... .......... .......... 30% 9.73M 32s
153700K .......... .......... .......... .......... .......... 30% 6.50M 32s
153750K .......... .......... .......... .......... .......... 30% 7.62M 32s
153800K .......... .......... .......... .......... .......... 30% 7.23M 32s
153850K .......... .......... .......... .......... .......... 30% 5.59M 32s
153900K .......... .......... .......... .......... .......... 30% 6.97M 32s
153950K .......... .......... .......... .......... .......... 30% 6.89M 32s
154000K .......... .......... .......... .......... .......... 30% 19.6M 32s
154050K .......... .......... .......... .......... .......... 30% 21.8M 32s
154100K .......... .......... .......... .......... .......... 30% 19.5M 32s
154150K .......... .......... .......... .......... .......... 30% 19.1M 32s
154200K .......... .......... .......... .......... .......... 30% 18.9M 32s
154250K .......... .......... .......... .......... .......... 30% 17.7M 32s
154300K .......... .......... .......... .......... .......... 30% 15.3M 32s
154350K .......... .......... .......... .......... .......... 30% 12.4M 32s
154400K .......... .......... .......... .......... .......... 30% 13.8M 32s
154450K .......... .......... .......... .......... .......... 30% 16.4M 32s
154500K .......... .......... .......... .......... .......... 30% 16.7M 32s
154550K .......... .......... .......... .......... .......... 30% 14.7M 32s
154600K .......... .......... .......... .......... .......... 30% 10.9M 32s
154650K .......... .......... .......... .......... .......... 30% 14.3M 32s
154700K .......... .......... .......... .......... .......... 30% 10.6M 32s
154750K .......... .......... .......... .......... .......... 30% 11.7M 32s
154800K .......... .......... .......... .......... .......... 30% 7.99M 32s
154850K .......... .......... .......... .......... .......... 30% 12.5M 32s
154900K .......... .......... .......... .......... .......... 30% 11.5M 32s
154950K .......... .......... .......... .......... .......... 30% 9.57M 32s
155000K .......... .......... .......... .......... .......... 30% 11.9M 32s
155050K .......... .......... .......... .......... .......... 30% 12.1M 32s
155100K .......... .......... .......... .......... .......... 30% 10.1M 32s
155150K .......... .......... .......... .......... .......... 30% 12.3M 32s
155200K .......... .......... .......... .......... .......... 30% 10.6M 32s
155250K .......... .......... .......... .......... .......... 30% 12.6M 32s
155300K .......... .......... .......... .......... .......... 30% 14.8M 32s
155350K .......... .......... .......... .......... .......... 30% 10.5M 32s
155400K .......... .......... .......... .......... .......... 30% 13.2M 32s
155450K .......... .......... .......... .......... .......... 30% 7.56M 32s
155500K .......... .......... .......... .......... .......... 30% 9.74M 32s
155550K .......... .......... .......... .......... .......... 30% 11.4M 32s
155600K .......... .......... .......... .......... .......... 30% 9.31M 32s
155650K .......... .......... .......... .......... .......... 30% 9.53M 32s
155700K .......... .......... .......... .......... .......... 30% 10.2M 32s
155750K .......... .......... .......... .......... .......... 30% 13.6M 32s
155800K .......... .......... .......... .......... .......... 30% 10.8M 32s
155850K .......... .......... .......... .......... .......... 30% 8.44M 32s
155900K .......... .......... .......... .......... .......... 30% 9.99M 32s
155950K .......... .......... .......... .......... .......... 30% 7.08M 32s
156000K .......... .......... .......... .......... .......... 30% 7.89M 32s
156050K .......... .......... .......... .......... .......... 30% 7.29M 32s
156100K .......... .......... .......... .......... .......... 30% 4.84M 32s
156150K .......... .......... .......... .......... .......... 30% 6.09M 32s
156200K .......... .......... .......... .......... .......... 30% 4.61M 32s
156250K .......... .......... .......... .......... .......... 30% 12.2M 32s
156300K .......... .......... .......... .......... .......... 30% 15.2M 32s
156350K .......... .......... .......... .......... .......... 30% 11.8M 32s
156400K .......... .......... .......... .......... .......... 30% 15.2M 32s
156450K .......... .......... .......... .......... .......... 30% 11.8M 32s
156500K .......... .......... .......... .......... .......... 30% 11.8M 32s
156550K .......... .......... .......... .......... .......... 30% 12.4M 32s
156600K .......... .......... .......... .......... .......... 30% 9.25M 32s
156650K .......... .......... .......... .......... .......... 30% 11.1M 32s
156700K .......... .......... .......... .......... .......... 30% 9.35M 32s
156750K .......... .......... .......... .......... .......... 30% 12.9M 32s
156800K .......... .......... .......... .......... .......... 30% 9.96M 32s
156850K .......... .......... .......... .......... .......... 30% 16.4M 32s
156900K .......... .......... .......... .......... .......... 30% 36.7M 32s
156950K .......... .......... .......... .......... .......... 30% 35.7M 32s
157000K .......... .......... .......... .......... .......... 30% 25.6M 32s
157050K .......... .......... .......... .......... .......... 30% 30.1M 32s
157100K .......... .......... .......... .......... .......... 30% 28.9M 32s
157150K .......... .......... .......... .......... .......... 30% 22.5M 32s
157200K .......... .......... .......... .......... .......... 30% 10.9M 32s
157250K .......... .......... .......... .......... .......... 30% 13.7M 32s
157300K .......... .......... .......... .......... .......... 30% 11.6M 32s
157350K .......... .......... .......... .......... .......... 30% 10.3M 32s
157400K .......... .......... .......... .......... .......... 30% 16.3M 32s
157450K .......... .......... .......... .......... .......... 30% 17.3M 32s
157500K .......... .......... .......... .......... .......... 30% 16.4M 32s
157550K .......... .......... .......... .......... .......... 30% 12.8M 32s
157600K .......... .......... .......... .......... .......... 31% 8.31M 32s
157650K .......... .......... .......... .......... .......... 31% 9.26M 32s
157700K .......... .......... .......... .......... .......... 31% 6.96M 32s
157750K .......... .......... .......... .......... .......... 31% 8.23M 32s
157800K .......... .......... .......... .......... .......... 31% 8.05M 32s
157850K .......... .......... .......... .......... .......... 31% 6.80M 32s
157900K .......... .......... .......... .......... .......... 31% 9.53M 32s
157950K .......... .......... .......... .......... .......... 31% 7.17M 32s
158000K .......... .......... .......... .......... .......... 31% 9.33M 32s
158050K .......... .......... .......... .......... .......... 31% 7.25M 32s
158100K .......... .......... .......... .......... .......... 31% 7.47M 32s
158150K .......... .......... .......... .......... .......... 31% 9.73M 32s
158200K .......... .......... .......... .......... .......... 31% 8.79M 32s
158250K .......... .......... .......... .......... .......... 31% 9.12M 32s
158300K .......... .......... .......... .......... .......... 31% 9.62M 32s
158350K .......... .......... .......... .......... .......... 31% 6.29M 32s
158400K .......... .......... .......... .......... .......... 31% 10.2M 32s
158450K .......... .......... .......... .......... .......... 31% 6.75M 32s
158500K .......... .......... .......... .......... .......... 31% 9.36M 32s
158550K .......... .......... .......... .......... .......... 31% 7.94M 32s
158600K .......... .......... .......... .......... .......... 31% 6.63M 32s
158650K .......... .......... .......... .......... .......... 31% 6.42M 32s
158700K .......... .......... .......... .......... .......... 31% 6.39M 32s
158750K .......... .......... .......... .......... .......... 31% 7.49M 32s
158800K .......... .......... .......... .......... .......... 31% 7.72M 32s
158850K .......... .......... .......... .......... .......... 31% 7.99M 32s
158900K .......... .......... .......... .......... .......... 31% 18.4M 32s
158950K .......... .......... .......... .......... .......... 31% 45.8M 32s
159000K .......... .......... .......... .......... .......... 31% 22.7M 32s
159050K .......... .......... .......... .......... .......... 31% 16.7M 32s
159100K .......... .......... .......... .......... .......... 31% 22.3M 32s
159150K .......... .......... .......... .......... .......... 31% 15.2M 32s
159200K .......... .......... .......... .......... .......... 31% 17.3M 32s
159250K .......... .......... .......... .......... .......... 31% 23.3M 32s
159300K .......... .......... .......... .......... .......... 31% 22.4M 32s
159350K .......... .......... .......... .......... .......... 31% 11.8M 32s
159400K .......... .......... .......... .......... .......... 31% 14.3M 32s
159450K .......... .......... .......... .......... .......... 31% 13.4M 32s
159500K .......... .......... .......... .......... .......... 31% 19.2M 32s
159550K .......... .......... .......... .......... .......... 31% 16.0M 32s
159600K .......... .......... .......... .......... .......... 31% 12.1M 32s
159650K .......... .......... .......... .......... .......... 31% 12.7M 32s
159700K .......... .......... .......... .......... .......... 31% 12.7M 32s
159750K .......... .......... .......... .......... .......... 31% 13.8M 32s
159800K .......... .......... .......... .......... .......... 31% 10.4M 32s
159850K .......... .......... .......... .......... .......... 31% 6.88M 32s
159900K .......... .......... .......... .......... .......... 31% 8.00M 32s
159950K .......... .......... .......... .......... .......... 31% 6.03M 32s
160000K .......... .......... .......... .......... .......... 31% 6.87M 32s
160050K .......... .......... .......... .......... .......... 31% 7.22M 32s
160100K .......... .......... .......... .......... .......... 31% 8.33M 32s
160150K .......... .......... .......... .......... .......... 31% 26.4M 32s
160200K .......... .......... .......... .......... .......... 31% 49.1M 32s
160250K .......... .......... .......... .......... .......... 31% 32.2M 32s
160300K .......... .......... .......... .......... .......... 31% 34.5M 32s
160350K .......... .......... .......... .......... .......... 31% 32.4M 32s
160400K .......... .......... .......... .......... .......... 31% 34.7M 32s
160450K .......... .......... .......... .......... .......... 31% 21.2M 32s
160500K .......... .......... .......... .......... .......... 31% 35.1M 32s
160550K .......... .......... .......... .......... .......... 31% 28.1M 32s
160600K .......... .......... .......... .......... .......... 31% 13.5M 32s
160650K .......... .......... .......... .......... .......... 31% 56.5M 32s
160700K .......... .......... .......... .......... .......... 31% 18.8M 32s
160750K .......... .......... .......... .......... .......... 31% 21.8M 32s
160800K .......... .......... .......... .......... .......... 31% 26.6M 32s
160850K .......... .......... .......... .......... .......... 31% 22.6M 32s
160900K .......... .......... .......... .......... .......... 31% 25.8M 32s
160950K .......... .......... .......... .......... .......... 31% 19.6M 32s
161000K .......... .......... .......... .......... .......... 31% 24.9M 32s
161050K .......... .......... .......... .......... .......... 31% 22.7M 32s
161100K .......... .......... .......... .......... .......... 31% 19.1M 32s
161150K .......... .......... .......... .......... .......... 31% 26.6M 32s
161200K .......... .......... .......... .......... .......... 31% 19.8M 32s
161250K .......... .......... .......... .......... .......... 31% 22.9M 32s
161300K .......... .......... .......... .......... .......... 31% 14.1M 32s
161350K .......... .......... .......... .......... .......... 31% 16.4M 32s
161400K .......... .......... .......... .......... .......... 31% 12.1M 32s
161450K .......... .......... .......... .......... .......... 31% 9.48M 32s
161500K .......... .......... .......... .......... .......... 31% 10.5M 32s
161550K .......... .......... .......... .......... .......... 31% 10.0M 32s
161600K .......... .......... .......... .......... .......... 31% 6.62M 32s
161650K .......... .......... .......... .......... .......... 31% 6.37M 32s
161700K .......... .......... .......... .......... .......... 31% 4.60M 32s
161750K .......... .......... .......... .......... .......... 31% 5.31M 32s
161800K .......... .......... .......... .......... .......... 31% 5.57M 32s
161850K .......... .......... .......... .......... .......... 31% 6.55M 32s
161900K .......... .......... .......... .......... .......... 31% 5.43M 32s
161950K .......... .......... .......... .......... .......... 31% 4.71M 32s
162000K .......... .......... .......... .......... .......... 31% 5.09M 32s
162050K .......... .......... .......... .......... .......... 31% 5.86M 32s
162100K .......... .......... .......... .......... .......... 31% 4.80M 32s
162150K .......... .......... .......... .......... .......... 31% 5.38M 32s
162200K .......... .......... .......... .......... .......... 31% 8.65M 32s
162250K .......... .......... .......... .......... .......... 31% 18.1M 32s
162300K .......... .......... .......... .......... .......... 31% 36.4M 32s
162350K .......... .......... .......... .......... .......... 31% 8.61M 32s
162400K .......... .......... .......... .......... .......... 31% 14.1M 32s
162450K .......... .......... .......... .......... .......... 31% 10.8M 32s
162500K .......... .......... .......... .......... .......... 31% 16.3M 32s
162550K .......... .......... .......... .......... .......... 31% 14.8M 32s
162600K .......... .......... .......... .......... .......... 31% 15.5M 32s
162650K .......... .......... .......... .......... .......... 32% 11.4M 32s
162700K .......... .......... .......... .......... .......... 32% 10.4M 32s
162750K .......... .......... .......... .......... .......... 32% 15.2M 32s
162800K .......... .......... .......... .......... .......... 32% 11.7M 32s
162850K .......... .......... .......... .......... .......... 32% 8.42M 32s
162900K .......... .......... .......... .......... .......... 32% 11.2M 32s
162950K .......... .......... .......... .......... .......... 32% 8.56M 32s
163000K .......... .......... .......... .......... .......... 32% 7.79M 32s
163050K .......... .......... .......... .......... .......... 32% 10.4M 32s
163100K .......... .......... .......... .......... .......... 32% 7.67M 32s
163150K .......... .......... .......... .......... .......... 32% 8.78M 32s
163200K .......... .......... .......... .......... .......... 32% 7.72M 32s
163250K .......... .......... .......... .......... .......... 32% 8.80M 32s
163300K .......... .......... .......... .......... .......... 32% 10.0M 32s
163350K .......... .......... .......... .......... .......... 32% 18.7M 31s
163400K .......... .......... .......... .......... .......... 32% 18.9M 31s
163450K .......... .......... .......... .......... .......... 32% 60.7M 31s
163500K .......... .......... .......... .......... .......... 32% 23.5M 31s
163550K .......... .......... .......... .......... .......... 32% 21.0M 31s
163600K .......... .......... .......... .......... .......... 32% 16.9M 31s
163650K .......... .......... .......... .......... .......... 32% 14.3M 31s
163700K .......... .......... .......... .......... .......... 32% 11.4M 31s
163750K .......... .......... .......... .......... .......... 32% 9.75M 31s
163800K .......... .......... .......... .......... .......... 32% 12.1M 31s
163850K .......... .......... .......... .......... .......... 32% 7.51M 31s
163900K .......... .......... .......... .......... .......... 32% 10.8M 31s
163950K .......... .......... .......... .......... .......... 32% 4.56M 31s
164000K .......... .......... .......... .......... .......... 32% 5.29M 31s
164050K .......... .......... .......... .......... .......... 32% 7.59M 31s
164100K .......... .......... .......... .......... .......... 32% 5.62M 31s
164150K .......... .......... .......... .......... .......... 32% 6.24M 31s
164200K .......... .......... .......... .......... .......... 32% 5.22M 31s
164250K .......... .......... .......... .......... .......... 32% 4.82M 31s
164300K .......... .......... .......... .......... .......... 32% 3.73M 31s
164350K .......... .......... .......... .......... .......... 32% 3.39M 31s
164400K .......... .......... .......... .......... .......... 32% 11.9M 31s
164450K .......... .......... .......... .......... .......... 32% 19.2M 31s
164500K .......... .......... .......... .......... .......... 32% 29.9M 31s
164550K .......... .......... .......... .......... .......... 32% 20.5M 31s
164600K .......... .......... .......... .......... .......... 32% 23.4M 31s
164650K .......... .......... .......... .......... .......... 32% 22.0M 31s
164700K .......... .......... .......... .......... .......... 32% 15.1M 31s
164750K .......... .......... .......... .......... .......... 32% 15.5M 31s
164800K .......... .......... .......... .......... .......... 32% 14.2M 31s
164850K .......... .......... .......... .......... .......... 32% 12.5M 31s
164900K .......... .......... .......... .......... .......... 32% 13.5M 31s
164950K .......... .......... .......... .......... .......... 32% 13.1M 31s
165000K .......... .......... .......... .......... .......... 32% 13.2M 31s
165050K .......... .......... .......... .......... .......... 32% 9.81M 31s
165100K .......... .......... .......... .......... .......... 32% 10.6M 31s
165150K .......... .......... .......... .......... .......... 32% 11.9M 31s
165200K .......... .......... .......... .......... .......... 32% 6.50M 31s
165250K .......... .......... .......... .......... .......... 32% 8.00M 31s
165300K .......... .......... .......... .......... .......... 32% 8.58M 31s
165350K .......... .......... .......... .......... .......... 32% 7.11M 31s
165400K .......... .......... .......... .......... .......... 32% 6.67M 31s
165450K .......... .......... .......... .......... .......... 32% 5.31M 31s
165500K .......... .......... .......... .......... .......... 32% 7.18M 31s
165550K .......... .......... .......... .......... .......... 32% 6.61M 31s
165600K .......... .......... .......... .......... .......... 32% 6.14M 31s
165650K .......... .......... .......... .......... .......... 32% 6.26M 31s
165700K .......... .......... .......... .......... .......... 32% 19.8M 31s
165750K .......... .......... .......... .......... .......... 32% 24.0M 31s
165800K .......... .......... .......... .......... .......... 32% 33.9M 31s
165850K .......... .......... .......... .......... .......... 32% 18.0M 31s
165900K .......... .......... .......... .......... .......... 32% 18.1M 31s
165950K .......... .......... .......... .......... .......... 32% 17.0M 31s
166000K .......... .......... .......... .......... .......... 32% 24.7M 31s
166050K .......... .......... .......... .......... .......... 32% 21.0M 31s
166100K .......... .......... .......... .......... .......... 32% 18.2M 31s
166150K .......... .......... .......... .......... .......... 32% 14.7M 31s
166200K .......... .......... .......... .......... .......... 32% 17.0M 31s
166250K .......... .......... .......... .......... .......... 32% 21.6M 31s
166300K .......... .......... .......... .......... .......... 32% 26.0M 31s
166350K .......... .......... .......... .......... .......... 32% 15.4M 31s
166400K .......... .......... .......... .......... .......... 32% 19.2M 31s
166450K .......... .......... .......... .......... .......... 32% 9.56M 31s
166500K .......... .......... .......... .......... .......... 32% 14.9M 31s
166550K .......... .......... .......... .......... .......... 32% 12.7M 31s
166600K .......... .......... .......... .......... .......... 32% 27.6M 31s
166650K .......... .......... .......... .......... .......... 32% 37.4M 31s
166700K .......... .......... .......... .......... .......... 32% 14.6M 31s
166750K .......... .......... .......... .......... .......... 32% 20.6M 31s
166800K .......... .......... .......... .......... .......... 32% 16.2M 31s
166850K .......... .......... .......... .......... .......... 32% 20.0M 31s
166900K .......... .......... .......... .......... .......... 32% 8.89M 31s
166950K .......... .......... .......... .......... .......... 32% 24.4M 31s
167000K .......... .......... .......... .......... .......... 32% 18.5M 31s
167050K .......... .......... .......... .......... .......... 32% 15.4M 31s
167100K .......... .......... .......... .......... .......... 32% 9.96M 31s
167150K .......... .......... .......... .......... .......... 32% 8.63M 31s
167200K .......... .......... .......... .......... .......... 32% 32.6M 31s
167250K .......... .......... .......... .......... .......... 32% 14.2M 31s
167300K .......... .......... .......... .......... .......... 32% 10.0M 31s
167350K .......... .......... .......... .......... .......... 32% 9.58M 31s
167400K .......... .......... .......... .......... .......... 32% 11.9M 31s
167450K .......... .......... .......... .......... .......... 32% 7.38M 31s
167500K .......... .......... .......... .......... .......... 32% 8.50M 31s
167550K .......... .......... .......... .......... .......... 32% 6.41M 31s
167600K .......... .......... .......... .......... .......... 32% 3.05M 31s
167650K .......... .......... .......... .......... .......... 32% 3.06M 31s
167700K .......... .......... .......... .......... .......... 32% 2.76M 31s
167750K .......... .......... .......... .......... .......... 33% 14.7M 31s
167800K .......... .......... .......... .......... .......... 33% 20.4M 31s
167850K .......... .......... .......... .......... .......... 33% 36.4M 31s
167900K .......... .......... .......... .......... .......... 33% 26.2M 31s
167950K .......... .......... .......... .......... .......... 33% 25.5M 31s
168000K .......... .......... .......... .......... .......... 33% 32.9M 31s
168050K .......... .......... .......... .......... .......... 33% 33.8M 31s
168100K .......... .......... .......... .......... .......... 33% 25.4M 31s
168150K .......... .......... .......... .......... .......... 33% 24.4M 31s
168200K .......... .......... .......... .......... .......... 33% 21.5M 31s
168250K .......... .......... .......... .......... .......... 33% 25.9M 31s
168300K .......... .......... .......... .......... .......... 33% 23.8M 31s
168350K .......... .......... .......... .......... .......... 33% 17.2M 31s
168400K .......... .......... .......... .......... .......... 33% 20.0M 31s
168450K .......... .......... .......... .......... .......... 33% 14.5M 31s
168500K .......... .......... .......... .......... .......... 33% 15.3M 31s
168550K .......... .......... .......... .......... .......... 33% 14.4M 31s
168600K .......... .......... .......... .......... .......... 33% 11.7M 31s
168650K .......... .......... .......... .......... .......... 33% 13.6M 31s
168700K .......... .......... .......... .......... .......... 33% 14.4M 31s
168750K .......... .......... .......... .......... .......... 33% 9.94M 31s
168800K .......... .......... .......... .......... .......... 33% 11.2M 31s
168850K .......... .......... .......... .......... .......... 33% 9.24M 31s
168900K .......... .......... .......... .......... .......... 33% 12.0M 31s
168950K .......... .......... .......... .......... .......... 33% 10.4M 31s
169000K .......... .......... .......... .......... .......... 33% 9.73M 31s
169050K .......... .......... .......... .......... .......... 33% 8.34M 31s
169100K .......... .......... .......... .......... .......... 33% 6.65M 31s
169150K .......... .......... .......... .......... .......... 33% 9.06M 31s
169200K .......... .......... .......... .......... .......... 33% 7.49M 31s
169250K .......... .......... .......... .......... .......... 33% 6.58M 31s
169300K .......... .......... .......... .......... .......... 33% 7.52M 31s
169350K .......... .......... .......... .......... .......... 33% 6.41M 31s
169400K .......... .......... .......... .......... .......... 33% 6.40M 31s
169450K .......... .......... .......... .......... .......... 33% 4.32M 31s
169500K .......... .......... .......... .......... .......... 33% 6.14M 31s
169550K .......... .......... .......... .......... .......... 33% 4.84M 31s
169600K .......... .......... .......... .......... .......... 33% 4.41M 31s
169650K .......... .......... .......... .......... .......... 33% 11.6M 31s
169700K .......... .......... .......... .......... .......... 33% 12.8M 31s
169750K .......... .......... .......... .......... .......... 33% 10.6M 31s
169800K .......... .......... .......... .......... .......... 33% 9.28M 31s
169850K .......... .......... .......... .......... .......... 33% 7.59M 31s
169900K .......... .......... .......... .......... .......... 33% 8.52M 31s
169950K .......... .......... .......... .......... .......... 33% 7.79M 31s
170000K .......... .......... .......... .......... .......... 33% 10.9M 31s
170050K .......... .......... .......... .......... .......... 33% 10.2M 31s
170100K .......... .......... .......... .......... .......... 33% 8.11M 31s
170150K .......... .......... .......... .......... .......... 33% 8.84M 31s
170200K .......... .......... .......... .......... .......... 33% 6.58M 31s
170250K .......... .......... .......... .......... .......... 33% 8.84M 31s
170300K .......... .......... .......... .......... .......... 33% 20.2M 31s
170350K .......... .......... .......... .......... .......... 33% 21.7M 31s
170400K .......... .......... .......... .......... .......... 33% 36.5M 31s
170450K .......... .......... .......... .......... .......... 33% 25.7M 31s
170500K .......... .......... .......... .......... .......... 33% 18.0M 31s
170550K .......... .......... .......... .......... .......... 33% 20.1M 31s
170600K .......... .......... .......... .......... .......... 33% 11.1M 31s
170650K .......... .......... .......... .......... .......... 33% 14.3M 31s
170700K .......... .......... .......... .......... .......... 33% 10.1M 31s
170750K .......... .......... .......... .......... .......... 33% 9.45M 31s
170800K .......... .......... .......... .......... .......... 33% 9.06M 31s
170850K .......... .......... .......... .......... .......... 33% 3.84M 31s
170900K .......... .......... .......... .......... .......... 33% 8.72M 31s
170950K .......... .......... .......... .......... .......... 33% 6.06M 31s
171000K .......... .......... .......... .......... .......... 33% 8.21M 31s
171050K .......... .......... .......... .......... .......... 33% 10.1M 31s
171100K .......... .......... .......... .......... .......... 33% 7.56M 31s
171150K .......... .......... .......... .......... .......... 33% 8.12M 31s
171200K .......... .......... .......... .......... .......... 33% 7.58M 31s
171250K .......... .......... .......... .......... .......... 33% 16.0M 31s
171300K .......... .......... .......... .......... .......... 33% 22.6M 31s
171350K .......... .......... .......... .......... .......... 33% 16.6M 31s
171400K .......... .......... .......... .......... .......... 33% 15.0M 31s
171450K .......... .......... .......... .......... .......... 33% 7.90M 31s
171500K .......... .......... .......... .......... .......... 33% 9.45M 31s
171550K .......... .......... .......... .......... .......... 33% 11.7M 31s
171600K .......... .......... .......... .......... .......... 33% 9.81M 31s
171650K .......... .......... .......... .......... .......... 33% 13.0M 31s
171700K .......... .......... .......... .......... .......... 33% 8.05M 31s
171750K .......... .......... .......... .......... .......... 33% 11.0M 31s
171800K .......... .......... .......... .......... .......... 33% 8.52M 31s
171850K .......... .......... .......... .......... .......... 33% 8.66M 31s
171900K .......... .......... .......... .......... .......... 33% 10.5M 31s
171950K .......... .......... .......... .......... .......... 33% 9.91M 31s
172000K .......... .......... .......... .......... .......... 33% 9.82M 31s
172050K .......... .......... .......... .......... .......... 33% 9.84M 31s
172100K .......... .......... .......... .......... .......... 33% 8.26M 31s
172150K .......... .......... .......... .......... .......... 33% 7.10M 31s
172200K .......... .......... .......... .......... .......... 33% 5.60M 31s
172250K .......... .......... .......... .......... .......... 33% 14.5M 31s
172300K .......... .......... .......... .......... .......... 33% 12.8M 31s
172350K .......... .......... .......... .......... .......... 33% 9.24M 31s
172400K .......... .......... .......... .......... .......... 33% 12.5M 31s
172450K .......... .......... .......... .......... .......... 33% 15.5M 31s
172500K .......... .......... .......... .......... .......... 33% 15.0M 31s
172550K .......... .......... .......... .......... .......... 33% 11.0M 31s
172600K .......... .......... .......... .......... .......... 33% 10.5M 31s
172650K .......... .......... .......... .......... .......... 33% 6.36M 31s
172700K .......... .......... .......... .......... .......... 33% 4.52M 31s
172750K .......... .......... .......... .......... .......... 33% 5.86M 31s
172800K .......... .......... .......... .......... .......... 33% 5.34M 31s
172850K .......... .......... .......... .......... .......... 34% 4.60M 31s
172900K .......... .......... .......... .......... .......... 34% 6.37M 31s
172950K .......... .......... .......... .......... .......... 34% 5.01M 31s
173000K .......... .......... .......... .......... .......... 34% 5.69M 31s
173050K .......... .......... .......... .......... .......... 34% 14.6M 31s
173100K .......... .......... .......... .......... .......... 34% 19.9M 31s
173150K .......... .......... .......... .......... .......... 34% 19.8M 31s
173200K .......... .......... .......... .......... .......... 34% 20.1M 31s
173250K .......... .......... .......... .......... .......... 34% 12.1M 31s
173300K .......... .......... .......... .......... .......... 34% 19.4M 31s
173350K .......... .......... .......... .......... .......... 34% 15.3M 31s
173400K .......... .......... .......... .......... .......... 34% 13.1M 31s
173450K .......... .......... .......... .......... .......... 34% 14.8M 31s
173500K .......... .......... .......... .......... .......... 34% 16.3M 31s
173550K .......... .......... .......... .......... .......... 34% 14.5M 31s
173600K .......... .......... .......... .......... .......... 34% 16.5M 31s
173650K .......... .......... .......... .......... .......... 34% 18.0M 31s
173700K .......... .......... .......... .......... .......... 34% 15.8M 31s
173750K .......... .......... .......... .......... .......... 34% 11.4M 31s
173800K .......... .......... .......... .......... .......... 34% 12.1M 31s
173850K .......... .......... .......... .......... .......... 34% 12.7M 31s
173900K .......... .......... .......... .......... .......... 34% 14.5M 31s
173950K .......... .......... .......... .......... .......... 34% 9.91M 31s
174000K .......... .......... .......... .......... .......... 34% 17.1M 31s
174050K .......... .......... .......... .......... .......... 34% 13.5M 31s
174100K .......... .......... .......... .......... .......... 34% 9.48M 31s
174150K .......... .......... .......... .......... .......... 34% 12.0M 31s
174200K .......... .......... .......... .......... .......... 34% 10.4M 31s
174250K .......... .......... .......... .......... .......... 34% 12.1M 31s
174300K .......... .......... .......... .......... .......... 34% 6.29M 31s
174350K .......... .......... .......... .......... .......... 34% 4.94M 31s
174400K .......... .......... .......... .......... .......... 34% 6.37M 31s
174450K .......... .......... .......... .......... .......... 34% 6.08M 31s
174500K .......... .......... .......... .......... .......... 34% 6.45M 31s
174550K .......... .......... .......... .......... .......... 34% 6.44M 31s
174600K .......... .......... .......... .......... .......... 34% 10.7M 31s
174650K .......... .......... .......... .......... .......... 34% 27.4M 31s
174700K .......... .......... .......... .......... .......... 34% 16.0M 31s
174750K .......... .......... .......... .......... .......... 34% 12.3M 31s
174800K .......... .......... .......... .......... .......... 34% 27.8M 31s
174850K .......... .......... .......... .......... .......... 34% 13.1M 31s
174900K .......... .......... .......... .......... .......... 34% 16.5M 31s
174950K .......... .......... .......... .......... .......... 34% 11.7M 31s
175000K .......... .......... .......... .......... .......... 34% 11.1M 31s
175050K .......... .......... .......... .......... .......... 34% 7.66M 31s
175100K .......... .......... .......... .......... .......... 34% 7.29M 31s
175150K .......... .......... .......... .......... .......... 34% 9.44M 31s
175200K .......... .......... .......... .......... .......... 34% 8.34M 31s
175250K .......... .......... .......... .......... .......... 34% 9.89M 31s
175300K .......... .......... .......... .......... .......... 34% 9.47M 31s
175350K .......... .......... .......... .......... .......... 34% 9.18M 31s
175400K .......... .......... .......... .......... .......... 34% 9.56M 31s
175450K .......... .......... .......... .......... .......... 34% 9.34M 31s
175500K .......... .......... .......... .......... .......... 34% 14.8M 31s
175550K .......... .......... .......... .......... .......... 34% 9.38M 31s
175600K .......... .......... .......... .......... .......... 34% 8.58M 31s
175650K .......... .......... .......... .......... .......... 34% 8.47M 31s
175700K .......... .......... .......... .......... .......... 34% 7.44M 31s
175750K .......... .......... .......... .......... .......... 34% 10.2M 31s
175800K .......... .......... .......... .......... .......... 34% 11.4M 31s
175850K .......... .......... .......... .......... .......... 34% 8.98M 31s
175900K .......... .......... .......... .......... .......... 34% 8.05M 31s
175950K .......... .......... .......... .......... .......... 34% 9.10M 31s
176000K .......... .......... .......... .......... .......... 34% 13.6M 31s
176050K .......... .......... .......... .......... .......... 34% 7.86M 30s
176100K .......... .......... .......... .......... .......... 34% 6.10M 31s
176150K .......... .......... .......... .......... .......... 34% 7.86M 30s
176200K .......... .......... .......... .......... .......... 34% 5.33M 31s
176250K .......... .......... .......... .......... .......... 34% 7.62M 31s
176300K .......... .......... .......... .......... .......... 34% 4.82M 31s
176350K .......... .......... .......... .......... .......... 34% 6.12M 31s
176400K .......... .......... .......... .......... .......... 34% 6.47M 31s
176450K .......... .......... .......... .......... .......... 34% 6.30M 31s
176500K .......... .......... .......... .......... .......... 34% 6.84M 31s
176550K .......... .......... .......... .......... .......... 34% 8.38M 31s
176600K .......... .......... .......... .......... .......... 34% 6.80M 31s
176650K .......... .......... .......... .......... .......... 34% 6.49M 31s
176700K .......... .......... .......... .......... .......... 34% 6.92M 31s
176750K .......... .......... .......... .......... .......... 34% 10.9M 31s
176800K .......... .......... .......... .......... .......... 34% 12.9M 31s
176850K .......... .......... .......... .......... .......... 34% 10.1M 30s
176900K .......... .......... .......... .......... .......... 34% 12.9M 30s
176950K .......... .......... .......... .......... .......... 34% 9.97M 30s
177000K .......... .......... .......... .......... .......... 34% 12.1M 30s
177050K .......... .......... .......... .......... .......... 34% 12.7M 30s
177100K .......... .......... .......... .......... .......... 34% 10.2M 30s
177150K .......... .......... .......... .......... .......... 34% 15.2M 30s
177200K .......... .......... .......... .......... .......... 34% 36.4M 30s
177250K .......... .......... .......... .......... .......... 34% 20.7M 30s
177300K .......... .......... .......... .......... .......... 34%  166M 30s
177350K .......... .......... .......... .......... .......... 34% 16.6M 30s
177400K .......... .......... .......... .......... .......... 34% 24.6M 30s
177450K .......... .......... .......... .......... .......... 34% 14.6M 30s
177500K .......... .......... .......... .......... .......... 34% 17.7M 30s
177550K .......... .......... .......... .......... .......... 34% 17.5M 30s
177600K .......... .......... .......... .......... .......... 34% 11.6M 30s
177650K .......... .......... .......... .......... .......... 34% 8.83M 30s
177700K .......... .......... .......... .......... .......... 34% 11.7M 30s
177750K .......... .......... .......... .......... .......... 34% 9.11M 30s
177800K .......... .......... .......... .......... .......... 34% 12.3M 30s
177850K .......... .......... .......... .......... .......... 34% 8.38M 30s
177900K .......... .......... .......... .......... .......... 34% 9.52M 30s
177950K .......... .......... .......... .......... .......... 35% 6.23M 30s
178000K .......... .......... .......... .......... .......... 35% 8.12M 30s
178050K .......... .......... .......... .......... .......... 35% 6.97M 30s
178100K .......... .......... .......... .......... .......... 35% 4.00M 30s
178150K .......... .......... .......... .......... .......... 35% 5.01M 30s
178200K .......... .......... .......... .......... .......... 35% 9.66M 30s
178250K .......... .......... .......... .......... .......... 35% 13.8M 30s
178300K .......... .......... .......... .......... .......... 35% 12.6M 30s
178350K .......... .......... .......... .......... .......... 35% 11.6M 30s
178400K .......... .......... .......... .......... .......... 35% 8.27M 30s
178450K .......... .......... .......... .......... .......... 35% 8.05M 30s
178500K .......... .......... .......... .......... .......... 35% 11.0M 30s
178550K .......... .......... .......... .......... .......... 35% 9.41M 30s
178600K .......... .......... .......... .......... .......... 35% 9.85M 30s
178650K .......... .......... .......... .......... .......... 35% 12.1M 30s
178700K .......... .......... .......... .......... .......... 35% 8.83M 30s
178750K .......... .......... .......... .......... .......... 35% 10.9M 30s
178800K .......... .......... .......... .......... .......... 35% 11.4M 30s
178850K .......... .......... .......... .......... .......... 35% 8.74M 30s
178900K .......... .......... .......... .......... .......... 35% 12.2M 30s
178950K .......... .......... .......... .......... .......... 35% 12.9M 30s
179000K .......... .......... .......... .......... .......... 35% 12.7M 30s
179050K .......... .......... .......... .......... .......... 35% 16.7M 30s
179100K .......... .......... .......... .......... .......... 35% 11.8M 30s
179150K .......... .......... .......... .......... .......... 35% 15.5M 30s
179200K .......... .......... .......... .......... .......... 35% 11.4M 30s
179250K .......... .......... .......... .......... .......... 35% 10.7M 30s
179300K .......... .......... .......... .......... .......... 35% 13.0M 30s
179350K .......... .......... .......... .......... .......... 35% 9.39M 30s
179400K .......... .......... .......... .......... .......... 35% 11.4M 30s
179450K .......... .......... .......... .......... .......... 35% 9.20M 30s
179500K .......... .......... .......... .......... .......... 35% 12.5M 30s
179550K .......... .......... .......... .......... .......... 35% 9.21M 30s
179600K .......... .......... .......... .......... .......... 35% 11.7M 30s
179650K .......... .......... .......... .......... .......... 35% 15.1M 30s
179700K .......... .......... .......... .......... .......... 35% 22.7M 30s
179750K .......... .......... .......... .......... .......... 35% 40.7M 30s
179800K .......... .......... .......... .......... .......... 35% 50.0M 30s
179850K .......... .......... .......... .......... .......... 35% 41.4M 30s
179900K .......... .......... .......... .......... .......... 35% 30.9M 30s
179950K .......... .......... .......... .......... .......... 35% 36.9M 30s
180000K .......... .......... .......... .......... .......... 35% 41.3M 30s
180050K .......... .......... .......... .......... .......... 35% 25.0M 30s
180100K .......... .......... .......... .......... .......... 35% 46.1M 30s
180150K .......... .......... .......... .......... .......... 35% 26.3M 30s
180200K .......... .......... .......... .......... .......... 35% 23.9M 30s
180250K .......... .......... .......... .......... .......... 35% 26.5M 30s
180300K .......... .......... .......... .......... .......... 35% 32.0M 30s
180350K .......... .......... .......... .......... .......... 35% 22.6M 30s
180400K .......... .......... .......... .......... .......... 35% 12.6M 30s
180450K .......... .......... .......... .......... .......... 35% 13.0M 30s
180500K .......... .......... .......... .......... .......... 35% 17.0M 30s
180550K .......... .......... .......... .......... .......... 35% 18.2M 30s
180600K .......... .......... .......... .......... .......... 35% 14.3M 30s
180650K .......... .......... .......... .......... .......... 35% 16.9M 30s
180700K .......... .......... .......... .......... .......... 35% 13.1M 30s
180750K .......... .......... .......... .......... .......... 35% 15.8M 30s
180800K .......... .......... .......... .......... .......... 35% 14.1M 30s
180850K .......... .......... .......... .......... .......... 35% 12.3M 30s
180900K .......... .......... .......... .......... .......... 35% 11.3M 30s
180950K .......... .......... .......... .......... .......... 35% 10.3M 30s
181000K .......... .......... .......... .......... .......... 35% 11.0M 30s
181050K .......... .......... .......... .......... .......... 35% 11.4M 30s
181100K .......... .......... .......... .......... .......... 35% 12.1M 30s
181150K .......... .......... .......... .......... .......... 35% 12.7M 30s
181200K .......... .......... .......... .......... .......... 35% 11.0M 30s
181250K .......... .......... .......... .......... .......... 35% 8.17M 30s
181300K .......... .......... .......... .......... .......... 35% 5.97M 30s
181350K .......... .......... .......... .......... .......... 35% 6.30M 30s
181400K .......... .......... .......... .......... .......... 35% 6.60M 30s
181450K .......... .......... .......... .......... .......... 35% 6.33M 30s
181500K .......... .......... .......... .......... .......... 35% 7.57M 30s
181550K .......... .......... .......... .......... .......... 35% 8.48M 30s
181600K .......... .......... .......... .......... .......... 35% 7.78M 30s
181650K .......... .......... .......... .......... .......... 35% 9.70M 30s
181700K .......... .......... .......... .......... .......... 35% 12.1M 30s
181750K .......... .......... .......... .......... .......... 35% 15.1M 30s
181800K .......... .......... .......... .......... .......... 35% 15.9M 30s
181850K .......... .......... .......... .......... .......... 35% 11.6M 30s
181900K .......... .......... .......... .......... .......... 35% 16.1M 30s
181950K .......... .......... .......... .......... .......... 35% 13.9M 30s
182000K .......... .......... .......... .......... .......... 35% 16.7M 30s
182050K .......... .......... .......... .......... .......... 35% 17.8M 30s
182100K .......... .......... .......... .......... .......... 35% 13.3M 30s
182150K .......... .......... .......... .......... .......... 35% 17.0M 30s
182200K .......... .......... .......... .......... .......... 35% 13.8M 30s
182250K .......... .......... .......... .......... .......... 35% 17.6M 30s
182300K .......... .......... .......... .......... .......... 35% 14.4M 30s
182350K .......... .......... .......... .......... .......... 35% 12.2M 30s
182400K .......... .......... .......... .......... .......... 35% 15.8M 30s
182450K .......... .......... .......... .......... .......... 35% 11.9M 30s
182500K .......... .......... .......... .......... .......... 35% 14.9M 30s
182550K .......... .......... .......... .......... .......... 35% 15.7M 30s
182600K .......... .......... .......... .......... .......... 35% 12.5M 30s
182650K .......... .......... .......... .......... .......... 35% 14.9M 30s
182700K .......... .......... .......... .......... .......... 35% 14.1M 30s
182750K .......... .......... .......... .......... .......... 35% 12.9M 30s
182800K .......... .......... .......... .......... .......... 35% 12.2M 30s
182850K .......... .......... .......... .......... .......... 35% 9.61M 30s
182900K .......... .......... .......... .......... .......... 35% 13.3M 30s
182950K .......... .......... .......... .......... .......... 35% 11.3M 30s
183000K .......... .......... .......... .......... .......... 36% 10.3M 30s
183050K .......... .......... .......... .......... .......... 36% 14.6M 30s
183100K .......... .......... .......... .......... .......... 36% 10.7M 30s
183150K .......... .......... .......... .......... .......... 36% 13.6M 30s
183200K .......... .......... .......... .......... .......... 36% 23.8M 30s
183250K .......... .......... .......... .......... .......... 36% 29.5M 30s
183300K .......... .......... .......... .......... .......... 36% 34.0M 30s
183350K .......... .......... .......... .......... .......... 36% 18.3M 30s
183400K .......... .......... .......... .......... .......... 36%  112M 30s
183450K .......... .......... .......... .......... .......... 36% 22.4M 30s
183500K .......... .......... .......... .......... .......... 36% 20.8M 30s
183550K .......... .......... .......... .......... .......... 36% 23.9M 30s
183600K .......... .......... .......... .......... .......... 36% 20.2M 30s
183650K .......... .......... .......... .......... .......... 36% 20.9M 30s
183700K .......... .......... .......... .......... .......... 36% 16.2M 30s
183750K .......... .......... .......... .......... .......... 36% 19.1M 30s
183800K .......... .......... .......... .......... .......... 36% 11.5M 30s
183850K .......... .......... .......... .......... .......... 36% 13.2M 30s
183900K .......... .......... .......... .......... .......... 36% 14.9M 30s
183950K .......... .......... .......... .......... .......... 36% 11.3M 30s
184000K .......... .......... .......... .......... .......... 36% 7.03M 30s
184050K .......... .......... .......... .......... .......... 36% 5.49M 30s
184100K .......... .......... .......... .......... .......... 36% 4.83M 30s
184150K .......... .......... .......... .......... .......... 36% 6.26M 30s
184200K .......... .......... .......... .......... .......... 36% 4.82M 30s
184250K .......... .......... .......... .......... .......... 36% 9.12M 30s
184300K .......... .......... .......... .......... .......... 36% 8.78M 30s
184350K .......... .......... .......... .......... .......... 36% 6.04M 30s
184400K .......... .......... .......... .......... .......... 36% 6.13M 30s
184450K .......... .......... .......... .......... .......... 36% 6.56M 30s
184500K .......... .......... .......... .......... .......... 36% 12.4M 30s
184550K .......... .......... .......... .......... .......... 36% 11.5M 30s
184600K .......... .......... .......... .......... .......... 36% 10.1M 30s
184650K .......... .......... .......... .......... .......... 36% 10.7M 30s
184700K .......... .......... .......... .......... .......... 36% 8.89M 30s
184750K .......... .......... .......... .......... .......... 36% 15.6M 30s
184800K .......... .......... .......... .......... .......... 36% 13.5M 30s
184850K .......... .......... .......... .......... .......... 36% 14.6M 30s
184900K .......... .......... .......... .......... .......... 36% 14.7M 30s
184950K .......... .......... .......... .......... .......... 36% 8.80M 30s
185000K .......... .......... .......... .......... .......... 36% 9.51M 30s
185050K .......... .......... .......... .......... .......... 36% 11.8M 30s
185100K .......... .......... .......... .......... .......... 36% 9.11M 30s
185150K .......... .......... .......... .......... .......... 36% 10.3M 30s
185200K .......... .......... .......... .......... .......... 36% 10.8M 30s
185250K .......... .......... .......... .......... .......... 36% 10.8M 30s
185300K .......... .......... .......... .......... .......... 36% 11.3M 30s
185350K .......... .......... .......... .......... .......... 36% 9.49M 30s
185400K .......... .......... .......... .......... .......... 36% 13.3M 30s
185450K .......... .......... .......... .......... .......... 36% 11.7M 30s
185500K .......... .......... .......... .......... .......... 36% 9.28M 30s
185550K .......... .......... .......... .......... .......... 36% 12.4M 30s
185600K .......... .......... .......... .......... .......... 36% 6.62M 30s
185650K .......... .......... .......... .......... .......... 36% 9.40M 30s
185700K .......... .......... .......... .......... .......... 36% 9.74M 30s
185750K .......... .......... .......... .......... .......... 36% 9.10M 30s
185800K .......... .......... .......... .......... .......... 36% 8.80M 30s
185850K .......... .......... .......... .......... .......... 36% 5.69M 30s
185900K .......... .......... .......... .......... .......... 36% 5.79M 30s
185950K .......... .......... .......... .......... .......... 36% 6.74M 30s
186000K .......... .......... .......... .......... .......... 36% 7.00M 30s
186050K .......... .......... .......... .......... .......... 36% 6.48M 30s
186100K .......... .......... .......... .......... .......... 36% 6.55M 30s
186150K .......... .......... .......... .......... .......... 36% 6.99M 30s
186200K .......... .......... .......... .......... .......... 36% 17.2M 30s
186250K .......... .......... .......... .......... .......... 36% 11.4M 30s
186300K .......... .......... .......... .......... .......... 36% 13.1M 30s
186350K .......... .......... .......... .......... .......... 36% 10.8M 30s
186400K .......... .......... .......... .......... .......... 36% 12.9M 30s
186450K .......... .......... .......... .......... .......... 36% 9.83M 30s
186500K .......... .......... .......... .......... .......... 36% 11.6M 30s
186550K .......... .......... .......... .......... .......... 36% 10.5M 30s
186600K .......... .......... .......... .......... .......... 36% 15.0M 30s
186650K .......... .......... .......... .......... .......... 36% 16.6M 29s
186700K .......... .......... .......... .......... .......... 36% 13.0M 29s
186750K .......... .......... .......... .......... .......... 36% 9.98M 29s
186800K .......... .......... .......... .......... .......... 36% 9.61M 29s
186850K .......... .......... .......... .......... .......... 36% 8.01M 29s
186900K .......... .......... .......... .......... .......... 36% 9.20M 29s
186950K .......... .......... .......... .......... .......... 36% 6.94M 29s
187000K .......... .......... .......... .......... .......... 36% 7.94M 29s
187050K .......... .......... .......... .......... .......... 36% 8.31M 29s
187100K .......... .......... .......... .......... .......... 36% 6.37M 29s
187150K .......... .......... .......... .......... .......... 36% 5.68M 29s
187200K .......... .......... .......... .......... .......... 36% 3.89M 29s
187250K .......... .......... .......... .......... .......... 36% 6.03M 29s
187300K .......... .......... .......... .......... .......... 36% 5.66M 29s
187350K .......... .......... .......... .......... .......... 36% 6.83M 29s
187400K .......... .......... .......... .......... .......... 36% 21.5M 29s
187450K .......... .......... .......... .......... .......... 36% 8.45M 29s
187500K .......... .......... .......... .......... .......... 36% 9.91M 29s
187550K .......... .......... .......... .......... .......... 36% 10.5M 29s
187600K .......... .......... .......... .......... .......... 36% 10.6M 29s
187650K .......... .......... .......... .......... .......... 36% 11.2M 29s
187700K .......... .......... .......... .......... .......... 36% 9.81M 29s
187750K .......... .......... .......... .......... .......... 36% 14.8M 29s
187800K .......... .......... .......... .......... .......... 36% 8.68M 29s
187850K .......... .......... .......... .......... .......... 36% 9.06M 29s
187900K .......... .......... .......... .......... .......... 36% 8.73M 29s
187950K .......... .......... .......... .......... .......... 36% 9.38M 29s
188000K .......... .......... .......... .......... .......... 36% 8.98M 29s
188050K .......... .......... .......... .......... .......... 36% 6.47M 29s
188100K .......... .......... .......... .......... .......... 37% 6.72M 29s
188150K .......... .......... .......... .......... .......... 37% 8.18M 29s
188200K .......... .......... .......... .......... .......... 37% 6.33M 29s
188250K .......... .......... .......... .......... .......... 37% 9.60M 29s
188300K .......... .......... .......... .......... .......... 37% 9.28M 29s
188350K .......... .......... .......... .......... .......... 37% 7.33M 29s
188400K .......... .......... .......... .......... .......... 37% 7.99M 29s
188450K .......... .......... .......... .......... .......... 37% 8.87M 29s
188500K .......... .......... .......... .......... .......... 37% 9.34M 29s
188550K .......... .......... .......... .......... .......... 37% 9.64M 29s
188600K .......... .......... .......... .......... .......... 37% 23.8M 29s
188650K .......... .......... .......... .......... .......... 37% 33.5M 29s
188700K .......... .......... .......... .......... .......... 37% 24.8M 29s
188750K .......... .......... .......... .......... .......... 37% 35.0M 29s
188800K .......... .......... .......... .......... .......... 37% 15.9M 29s
188850K .......... .......... .......... .......... .......... 37% 11.4M 29s
188900K .......... .......... .......... .......... .......... 37% 7.51M 29s
188950K .......... .......... .......... .......... .......... 37% 6.13M 29s
189000K .......... .......... .......... .......... .......... 37% 7.98M 29s
189050K .......... .......... .......... .......... .......... 37% 8.60M 29s
189100K .......... .......... .......... .......... .......... 37% 7.61M 29s
189150K .......... .......... .......... .......... .......... 37% 8.87M 29s
189200K .......... .......... .......... .......... .......... 37% 7.67M 29s
189250K .......... .......... .......... .......... .......... 37% 11.3M 29s
189300K .......... .......... .......... .......... .......... 37% 19.6M 29s
189350K .......... .......... .......... .......... .......... 37% 14.0M 29s
189400K .......... .......... .......... .......... .......... 37% 16.8M 29s
189450K .......... .......... .......... .......... .......... 37% 14.5M 29s
189500K .......... .......... .......... .......... .......... 37% 20.0M 29s
189550K .......... .......... .......... .......... .......... 37% 14.7M 29s
189600K .......... .......... .......... .......... .......... 37% 10.5M 29s
189650K .......... .......... .......... .......... .......... 37% 14.9M 29s
189700K .......... .......... .......... .......... .......... 37% 9.44M 29s
189750K .......... .......... .......... .......... .......... 37% 14.0M 29s
189800K .......... .......... .......... .......... .......... 37% 10.0M 29s
189850K .......... .......... .......... .......... .......... 37% 9.36M 29s
189900K .......... .......... .......... .......... .......... 37% 10.9M 29s
189950K .......... .......... .......... .......... .......... 37% 9.35M 29s
190000K .......... .......... .......... .......... .......... 37% 11.5M 29s
190050K .......... .......... .......... .......... .......... 37% 8.43M 29s
190100K .......... .......... .......... .......... .......... 37% 15.7M 29s
190150K .......... .......... .......... .......... .......... 37% 18.2M 29s
190200K .......... .......... .......... .......... .......... 37% 39.1M 29s
190250K .......... .......... .......... .......... .......... 37% 23.7M 29s
190300K .......... .......... .......... .......... .......... 37% 17.3M 29s
190350K .......... .......... .......... .......... .......... 37% 13.0M 29s
190400K .......... .......... .......... .......... .......... 37% 15.8M 29s
190450K .......... .......... .......... .......... .......... 37% 11.9M 29s
190500K .......... .......... .......... .......... .......... 37% 14.2M 29s
190550K .......... .......... .......... .......... .......... 37% 11.7M 29s
190600K .......... .......... .......... .......... .......... 37% 9.03M 29s
190650K .......... .......... .......... .......... .......... 37% 11.4M 29s
190700K .......... .......... .......... .......... .......... 37% 9.12M 29s
190750K .......... .......... .......... .......... .......... 37% 12.1M 29s
190800K .......... .......... .......... .......... .......... 37% 12.7M 29s
190850K .......... .......... .......... .......... .......... 37% 8.60M 29s
190900K .......... .......... .......... .......... .......... 37% 9.00M 29s
190950K .......... .......... .......... .......... .......... 37% 6.17M 29s
191000K .......... .......... .......... .......... .......... 37% 8.35M 29s
191050K .......... .......... .......... .......... .......... 37% 7.18M 29s
191100K .......... .......... .......... .......... .......... 37% 5.99M 29s
191150K .......... .......... .......... .......... .......... 37% 12.1M 29s
191200K .......... .......... .......... .......... .......... 37% 11.7M 29s
191250K .......... .......... .......... .......... .......... 37% 13.0M 29s
191300K .......... .......... .......... .......... .......... 37% 12.4M 29s
191350K .......... .......... .......... .......... .......... 37% 8.68M 29s
191400K .......... .......... .......... .......... .......... 37% 9.61M 29s
191450K .......... .......... .......... .......... .......... 37% 5.59M 29s
191500K .......... .......... .......... .......... .......... 37% 14.0M 29s
191550K .......... .......... .......... .......... .......... 37% 8.48M 29s
191600K .......... .......... .......... .......... .......... 37% 7.44M 29s
191650K .......... .......... .......... .......... .......... 37% 8.29M 29s
191700K .......... .......... .......... .......... .......... 37% 7.40M 29s
191750K .......... .......... .......... .......... .......... 37% 8.54M 29s
191800K .......... .......... .......... .......... .......... 37% 7.71M 29s
191850K .......... .......... .......... .......... .......... 37% 5.61M 29s
191900K .......... .......... .......... .......... .......... 37% 6.78M 29s
191950K .......... .......... .......... .......... .......... 37% 4.83M 29s
192000K .......... .......... .......... .......... .......... 37% 5.83M 29s
192050K .......... .......... .......... .......... .......... 37% 4.62M 29s
192100K .......... .......... .......... .......... .......... 37% 3.83M 29s
192150K .......... .......... .......... .......... .......... 37% 3.56M 29s
192200K .......... .......... .......... .......... .......... 37% 10.7M 29s
192250K .......... .......... .......... .......... .......... 37% 20.4M 29s
192300K .......... .......... .......... .......... .......... 37% 28.8M 29s
192350K .......... .......... .......... .......... .......... 37% 10.8M 29s
192400K .......... .......... .......... .......... .......... 37% 14.5M 29s
192450K .......... .......... .......... .......... .......... 37% 10.8M 29s
192500K .......... .......... .......... .......... .......... 37% 15.4M 29s
192550K .......... .......... .......... .......... .......... 37% 12.8M 29s
192600K .......... .......... .......... .......... .......... 37% 12.1M 29s
192650K .......... .......... .......... .......... .......... 37% 16.9M 29s
192700K .......... .......... .......... .......... .......... 37% 9.97M 29s
192750K .......... .......... .......... .......... .......... 37% 16.1M 29s
192800K .......... .......... .......... .......... .......... 37% 18.2M 29s
192850K .......... .......... .......... .......... .......... 37% 10.5M 29s
192900K .......... .......... .......... .......... .......... 37% 14.7M 29s
192950K .......... .......... .......... .......... .......... 37% 6.99M 29s
193000K .......... .......... .......... .......... .......... 37% 12.3M 29s
193050K .......... .......... .......... .......... .......... 37% 9.16M 29s
193100K .......... .......... .......... .......... .......... 37% 6.19M 29s
193150K .......... .......... .......... .......... .......... 37% 8.65M 29s
193200K .......... .......... .......... .......... .......... 38% 8.98M 29s
193250K .......... .......... .......... .......... .......... 38% 10.3M 29s
193300K .......... .......... .......... .......... .......... 38% 10.6M 29s
193350K .......... .......... .......... .......... .......... 38% 10.4M 29s
193400K .......... .......... .......... .......... .......... 38% 10.8M 29s
193450K .......... .......... .......... .......... .......... 38% 10.7M 29s
193500K .......... .......... .......... .......... .......... 38% 9.57M 29s
193550K .......... .......... .......... .......... .......... 38% 9.87M 29s
193600K .......... .......... .......... .......... .......... 38% 7.81M 29s
193650K .......... .......... .......... .......... .......... 38% 12.0M 29s
193700K .......... .......... .......... .......... .......... 38% 7.97M 29s
193750K .......... .......... .......... .......... .......... 38% 7.54M 29s
193800K .......... .......... .......... .......... .......... 38% 6.40M 29s
193850K .......... .......... .......... .......... .......... 38% 5.87M 29s
193900K .......... .......... .......... .......... .......... 38% 6.45M 29s
193950K .......... .......... .......... .......... .......... 38% 5.40M 29s
194000K .......... .......... .......... .......... .......... 38% 6.01M 29s
194050K .......... .......... .......... .......... .......... 38% 5.88M 29s
194100K .......... .......... .......... .......... .......... 38% 6.36M 29s
194150K .......... .......... .......... .......... .......... 38% 8.67M 29s
194200K .......... .......... .......... .......... .......... 38% 9.53M 29s
194250K .......... .......... .......... .......... .......... 38% 9.63M 29s
194300K .......... .......... .......... .......... .......... 38% 9.72M 29s
194350K .......... .......... .......... .......... .......... 38% 8.15M 29s
194400K .......... .......... .......... .......... .......... 38% 10.9M 29s
194450K .......... .......... .......... .......... .......... 38% 12.1M 29s
194500K .......... .......... .......... .......... .......... 38% 19.3M 29s
194550K .......... .......... .......... .......... .......... 38% 13.4M 29s
194600K .......... .......... .......... .......... .......... 38% 7.00M 29s
194650K .......... .......... .......... .......... .......... 38% 7.28M 29s
194700K .......... .......... .......... .......... .......... 38% 7.77M 29s
194750K .......... .......... .......... .......... .......... 38% 8.87M 29s
194800K .......... .......... .......... .......... .......... 38% 10.0M 29s
194850K .......... .......... .......... .......... .......... 38% 11.5M 29s
194900K .......... .......... .......... .......... .......... 38% 11.9M 29s
194950K .......... .......... .......... .......... .......... 38% 10.5M 29s
195000K .......... .......... .......... .......... .......... 38% 9.35M 29s
195050K .......... .......... .......... .......... .......... 38% 14.0M 29s
195100K .......... .......... .......... .......... .......... 38% 11.7M 29s
195150K .......... .......... .......... .......... .......... 38% 8.82M 29s
195200K .......... .......... .......... .......... .......... 38% 4.00M 29s
195250K .......... .......... .......... .......... .......... 38% 3.91M 29s
195300K .......... .......... .......... .......... .......... 38% 4.40M 29s
195350K .......... .......... .......... .......... .......... 38% 6.57M 29s
195400K .......... .......... .......... .......... .......... 38% 16.1M 29s
195450K .......... .......... .......... .......... .......... 38% 9.43M 29s
195500K .......... .......... .......... .......... .......... 38% 9.30M 29s
195550K .......... .......... .......... .......... .......... 38% 11.6M 29s
195600K .......... .......... .......... .......... .......... 38% 5.57M 29s
195650K .......... .......... .......... .......... .......... 38% 7.99M 29s
195700K .......... .......... .......... .......... .......... 38% 5.97M 29s
195750K .......... .......... .......... .......... .......... 38% 8.00M 29s
195800K .......... .......... .......... .......... .......... 38% 6.78M 29s
195850K .......... .......... .......... .......... .......... 38% 5.48M 29s
195900K .......... .......... .......... .......... .......... 38% 6.22M 29s
195950K .......... .......... .......... .......... .......... 38% 9.27M 29s
196000K .......... .......... .......... .......... .......... 38% 8.49M 29s
196050K .......... .......... .......... .......... .......... 38% 7.35M 29s
196100K .......... .......... .......... .......... .......... 38% 7.27M 29s
196150K .......... .......... .......... .......... .......... 38% 7.81M 29s
196200K .......... .......... .......... .......... .......... 38% 8.35M 29s
196250K .......... .......... .......... .......... .......... 38% 7.31M 29s
196300K .......... .......... .......... .......... .......... 38% 7.75M 29s
196350K .......... .......... .......... .......... .......... 38% 6.54M 29s
196400K .......... .......... .......... .......... .......... 38% 8.01M 29s
196450K .......... .......... .......... .......... .......... 38% 6.13M 29s
196500K .......... .......... .......... .......... .......... 38% 7.16M 29s
196550K .......... .......... .......... .......... .......... 38% 8.48M 29s
196600K .......... .......... .......... .......... .......... 38% 5.81M 29s
196650K .......... .......... .......... .......... .......... 38% 6.94M 29s
196700K .......... .......... .......... .......... .......... 38% 5.17M 29s
196750K .......... .......... .......... .......... .......... 38% 5.47M 29s
196800K .......... .......... .......... .......... .......... 38% 4.62M 29s
196850K .......... .......... .......... .......... .......... 38% 3.41M 29s
196900K .......... .......... .......... .......... .......... 38% 3.98M 29s
196950K .......... .......... .......... .......... .......... 38% 5.93M 29s
197000K .......... .......... .......... .......... .......... 38% 17.8M 29s
197050K .......... .......... .......... .......... .......... 38% 31.5M 29s
197100K .......... .......... .......... .......... .......... 38% 18.0M 29s
197150K .......... .......... .......... .......... .......... 38% 32.4M 29s
197200K .......... .......... .......... .......... .......... 38% 14.8M 29s
197250K .......... .......... .......... .......... .......... 38% 12.3M 29s
197300K .......... .......... .......... .......... .......... 38% 13.1M 29s
197350K .......... .......... .......... .......... .......... 38% 11.7M 29s
197400K .......... .......... .......... .......... .......... 38% 16.5M 29s
197450K .......... .......... .......... .......... .......... 38% 10.1M 29s
197500K .......... .......... .......... .......... .......... 38% 14.2M 29s
197550K .......... .......... .......... .......... .......... 38% 11.0M 29s
197600K .......... .......... .......... .......... .......... 38% 11.4M 29s
197650K .......... .......... .......... .......... .......... 38% 13.7M 29s
197700K .......... .......... .......... .......... .......... 38% 11.3M 29s
197750K .......... .......... .......... .......... .......... 38% 11.3M 29s
197800K .......... .......... .......... .......... .......... 38% 15.2M 29s
197850K .......... .......... .......... .......... .......... 38% 11.4M 29s
197900K .......... .......... .......... .......... .......... 38% 16.0M 29s
197950K .......... .......... .......... .......... .......... 38% 19.7M 29s
198000K .......... .......... .......... .......... .......... 38% 30.0M 29s
198050K .......... .......... .......... .......... .......... 38% 25.2M 29s
198100K .......... .......... .......... .......... .......... 38% 19.9M 29s
198150K .......... .......... .......... .......... .......... 38% 29.8M 29s
198200K .......... .......... .......... .......... .......... 38% 11.8M 29s
198250K .......... .......... .......... .......... .......... 39% 9.25M 29s
198300K .......... .......... .......... .......... .......... 39% 10.3M 29s
198350K .......... .......... .......... .......... .......... 39% 8.96M 29s
198400K .......... .......... .......... .......... .......... 39% 12.5M 29s
198450K .......... .......... .......... .......... .......... 39% 7.11M 29s
198500K .......... .......... .......... .......... .......... 39% 8.25M 29s
198550K .......... .......... .......... .......... .......... 39% 9.10M 29s
198600K .......... .......... .......... .......... .......... 39% 10.4M 29s
198650K .......... .......... .......... .......... .......... 39% 10.1M 29s
198700K .......... .......... .......... .......... .......... 39% 20.4M 29s
198750K .......... .......... .......... .......... .......... 39% 12.6M 29s
198800K .......... .......... .......... .......... .......... 39% 14.7M 29s
198850K .......... .......... .......... .......... .......... 39% 13.0M 29s
198900K .......... .......... .......... .......... .......... 39% 13.0M 29s
198950K .......... .......... .......... .......... .......... 39% 11.8M 29s
199000K .......... .......... .......... .......... .......... 39% 15.4M 29s
199050K .......... .......... .......... .......... .......... 39% 17.9M 29s
199100K .......... .......... .......... .......... .......... 39% 11.6M 29s
199150K .......... .......... .......... .......... .......... 39% 15.6M 29s
199200K .......... .......... .......... .......... .......... 39% 11.6M 29s
199250K .......... .......... .......... .......... .......... 39% 16.4M 29s
199300K .......... .......... .......... .......... .......... 39% 16.1M 29s
199350K .......... .......... .......... .......... .......... 39% 37.0M 29s
199400K .......... .......... .......... .......... .......... 39% 31.0M 29s
199450K .......... .......... .......... .......... .......... 39% 16.4M 29s
199500K .......... .......... .......... .......... .......... 39% 39.8M 29s
199550K .......... .......... .......... .......... .......... 39% 14.3M 29s
199600K .......... .......... .......... .......... .......... 39% 13.6M 29s
199650K .......... .......... .......... .......... .......... 39% 12.0M 29s
199700K .......... .......... .......... .......... .......... 39% 9.61M 29s
199750K .......... .......... .......... .......... .......... 39% 10.3M 29s
199800K .......... .......... .......... .......... .......... 39% 11.3M 29s
199850K .......... .......... .......... .......... .......... 39% 8.46M 29s
199900K .......... .......... .......... .......... .......... 39% 10.8M 29s
199950K .......... .......... .......... .......... .......... 39% 8.85M 29s
200000K .......... .......... .......... .......... .......... 39% 20.0M 29s
200050K .......... .......... .......... .......... .......... 39% 33.7M 29s
200100K .......... .......... .......... .......... .......... 39% 12.3M 29s
200150K .......... .......... .......... .......... .......... 39% 13.9M 29s
200200K .......... .......... .......... .......... .......... 39% 15.7M 29s
200250K .......... .......... .......... .......... .......... 39% 11.4M 29s
200300K .......... .......... .......... .......... .......... 39% 15.3M 29s
200350K .......... .......... .......... .......... .......... 39% 12.1M 28s
200400K .......... .......... .......... .......... .......... 39% 13.2M 28s
200450K .......... .......... .......... .......... .......... 39% 12.5M 28s
200500K .......... .......... .......... .......... .......... 39% 16.8M 28s
200550K .......... .......... .......... .......... .......... 39% 14.0M 28s
200600K .......... .......... .......... .......... .......... 39% 12.1M 28s
200650K .......... .......... .......... .......... .......... 39% 14.1M 28s
200700K .......... .......... .......... .......... .......... 39% 11.6M 28s
200750K .......... .......... .......... .......... .......... 39% 13.5M 28s
200800K .......... .......... .......... .......... .......... 39% 16.4M 28s
200850K .......... .......... .......... .......... .......... 39% 20.6M 28s
200900K .......... .......... .......... .......... .......... 39% 32.9M 28s
200950K .......... .......... .......... .......... .......... 39% 15.2M 28s
201000K .......... .......... .......... .......... .......... 39% 16.7M 28s
201050K .......... .......... .......... .......... .......... 39% 12.1M 28s
201100K .......... .......... .......... .......... .......... 39% 11.3M 28s
201150K .......... .......... .......... .......... .......... 39% 12.0M 28s
201200K .......... .......... .......... .......... .......... 39% 9.67M 28s
201250K .......... .......... .......... .......... .......... 39% 11.7M 28s
201300K .......... .......... .......... .......... .......... 39% 9.13M 28s
201350K .......... .......... .......... .......... .......... 39% 11.4M 28s
201400K .......... .......... .......... .......... .......... 39% 8.05M 28s
201450K .......... .......... .......... .......... .......... 39% 6.85M 28s
201500K .......... .......... .......... .......... .......... 39% 7.24M 28s
201550K .......... .......... .......... .......... .......... 39% 6.63M 28s
201600K .......... .......... .......... .......... .......... 39% 6.35M 28s
201650K .......... .......... .......... .......... .......... 39% 7.60M 28s
201700K .......... .......... .......... .......... .......... 39% 5.59M 28s
201750K .......... .......... .......... .......... .......... 39% 5.84M 28s
201800K .......... .......... .......... .......... .......... 39% 7.41M 28s
201850K .......... .......... .......... .......... .......... 39% 8.52M 28s
201900K .......... .......... .......... .......... .......... 39% 7.49M 28s
201950K .......... .......... .......... .......... .......... 39% 8.10M 28s
202000K .......... .......... .......... .......... .......... 39% 6.36M 28s
202050K .......... .......... .......... .......... .......... 39% 8.06M 28s
202100K .......... .......... .......... .......... .......... 39% 5.79M 28s
202150K .......... .......... .......... .......... .......... 39% 6.90M 28s
202200K .......... .......... .......... .......... .......... 39% 5.40M 28s
202250K .......... .......... .......... .......... .......... 39% 8.26M 28s
202300K .......... .......... .......... .......... .......... 39% 9.59M 28s
202350K .......... .......... .......... .......... .......... 39% 7.27M 28s
202400K .......... .......... .......... .......... .......... 39% 11.1M 28s
202450K .......... .......... .......... .......... .......... 39% 6.95M 28s
202500K .......... .......... .......... .......... .......... 39% 9.79M 28s
202550K .......... .......... .......... .......... .......... 39% 9.89M 28s
202600K .......... .......... .......... .......... .......... 39% 13.2M 28s
202650K .......... .......... .......... .......... .......... 39% 10.2M 28s
202700K .......... .......... .......... .......... .......... 39% 8.48M 28s
202750K .......... .......... .......... .......... .......... 39% 11.4M 28s
202800K .......... .......... .......... .......... .......... 39% 10.1M 28s
202850K .......... .......... .......... .......... .......... 39% 7.40M 28s
202900K .......... .......... .......... .......... .......... 39% 7.64M 28s
202950K .......... .......... .......... .......... .......... 39% 8.03M 28s
203000K .......... .......... .......... .......... .......... 39% 8.84M 28s
203050K .......... .......... .......... .......... .......... 39% 7.30M 28s
203100K .......... .......... .......... .......... .......... 39% 7.92M 28s
203150K .......... .......... .......... .......... .......... 39% 14.9M 28s
203200K .......... .......... .......... .......... .......... 39% 19.9M 28s
203250K .......... .......... .......... .......... .......... 39% 44.3M 28s
203300K .......... .......... .......... .......... .......... 39% 18.8M 28s
203350K .......... .......... .......... .......... .......... 40% 23.6M 28s
203400K .......... .......... .......... .......... .......... 40% 13.6M 28s
203450K .......... .......... .......... .......... .......... 40% 11.6M 28s
203500K .......... .......... .......... .......... .......... 40% 7.96M 28s
203550K .......... .......... .......... .......... .......... 40% 7.55M 28s
203600K .......... .......... .......... .......... .......... 40% 6.07M 28s
203650K .......... .......... .......... .......... .......... 40% 7.01M 28s
203700K .......... .......... .......... .......... .......... 40% 5.62M 28s
203750K .......... .......... .......... .......... .......... 40% 7.13M 28s
203800K .......... .......... .......... .......... .......... 40% 9.84M 28s
203850K .......... .......... .......... .......... .......... 40% 20.6M 28s
203900K .......... .......... .......... .......... .......... 40% 25.4M 28s
203950K .......... .......... .......... .......... .......... 40% 15.2M 28s
204000K .......... .......... .......... .......... .......... 40% 17.0M 28s
204050K .......... .......... .......... .......... .......... 40% 15.5M 28s
204100K .......... .......... .......... .......... .......... 40% 10.2M 28s
204150K .......... .......... .......... .......... .......... 40% 10.9M 28s
204200K .......... .......... .......... .......... .......... 40% 8.93M 28s
204250K .......... .......... .......... .......... .......... 40% 8.39M 28s
204300K .......... .......... .......... .......... .......... 40% 9.40M 28s
204350K .......... .......... .......... .......... .......... 40% 7.43M 28s
204400K .......... .......... .......... .......... .......... 40% 10.8M 28s
204450K .......... .......... .......... .......... .......... 40% 8.02M 28s
204500K .......... .......... .......... .......... .......... 40% 9.71M 28s
204550K .......... .......... .......... .......... .......... 40% 13.8M 28s
204600K .......... .......... .......... .......... .......... 40% 7.78M 28s
204650K .......... .......... .......... .......... .......... 40% 7.29M 28s
204700K .......... .......... .......... .......... .......... 40% 8.15M 28s
204750K .......... .......... .......... .......... .......... 40% 6.61M 28s
204800K .......... .......... .......... .......... .......... 40% 8.01M 28s
204850K .......... .......... .......... .......... .......... 40% 9.08M 28s
204900K .......... .......... .......... .......... .......... 40% 8.31M 28s
204950K .......... .......... .......... .......... .......... 40% 7.69M 28s
205000K .......... .......... .......... .......... .......... 40% 8.36M 28s
205050K .......... .......... .......... .......... .......... 40% 5.96M 28s
205100K .......... .......... .......... .......... .......... 40% 6.01M 28s
205150K .......... .......... .......... .......... .......... 40% 6.31M 28s
205200K .......... .......... .......... .......... .......... 40% 5.00M 28s
205250K .......... .......... .......... .......... .......... 40% 5.16M 28s
205300K .......... .......... .......... .......... .......... 40% 5.03M 28s
205350K .......... .......... .......... .......... .......... 40% 5.44M 28s
205400K .......... .......... .......... .......... .......... 40% 21.9M 28s
205450K .......... .......... .......... .......... .......... 40% 16.9M 28s
205500K .......... .......... .......... .......... .......... 40% 50.9M 28s
205550K .......... .......... .......... .......... .......... 40% 22.3M 28s
205600K .......... .......... .......... .......... .......... 40% 12.2M 28s
205650K .......... .......... .......... .......... .......... 40% 26.6M 28s
205700K .......... .......... .......... .......... .......... 40% 10.7M 28s
205750K .......... .......... .......... .......... .......... 40% 12.8M 28s
205800K .......... .......... .......... .......... .......... 40% 5.28M 28s
205850K .......... .......... .......... .......... .......... 40% 12.0M 28s
205900K .......... .......... .......... .......... .......... 40% 7.63M 28s
205950K .......... .......... .......... .......... .......... 40% 5.96M 28s
206000K .......... .......... .......... .......... .......... 40% 7.78M 28s
206050K .......... .......... .......... .......... .......... 40% 7.83M 28s
206100K .......... .......... .......... .......... .......... 40% 12.1M 28s
206150K .......... .......... .......... .......... .......... 40% 9.87M 28s
206200K .......... .......... .......... .......... .......... 40% 6.65M 28s
206250K .......... .......... .......... .......... .......... 40% 9.54M 28s
206300K .......... .......... .......... .......... .......... 40% 9.24M 28s
206350K .......... .......... .......... .......... .......... 40% 7.09M 28s
206400K .......... .......... .......... .......... .......... 40% 8.05M 28s
206450K .......... .......... .......... .......... .......... 40% 7.96M 28s
206500K .......... .......... .......... .......... .......... 40% 8.60M 28s
206550K .......... .......... .......... .......... .......... 40% 9.82M 28s
206600K .......... .......... .......... .......... .......... 40% 9.42M 28s
206650K .......... .......... .......... .......... .......... 40% 24.0M 28s
206700K .......... .......... .......... .......... .......... 40% 22.3M 28s
206750K .......... .......... .......... .......... .......... 40% 28.4M 28s
206800K .......... .......... .......... .......... .......... 40% 23.8M 28s
206850K .......... .......... .......... .......... .......... 40% 14.6M 28s
206900K .......... .......... .......... .......... .......... 40% 16.2M 28s
206950K .......... .......... .......... .......... .......... 40% 13.6M 28s
207000K .......... .......... .......... .......... .......... 40% 11.2M 28s
207050K .......... .......... .......... .......... .......... 40% 16.7M 28s
207100K .......... .......... .......... .......... .......... 40% 10.5M 28s
207150K .......... .......... .......... .......... .......... 40% 13.2M 28s
207200K .......... .......... .......... .......... .......... 40% 12.2M 28s
207250K .......... .......... .......... .......... .......... 40% 16.0M 28s
207300K .......... .......... .......... .......... .......... 40% 14.0M 28s
207350K .......... .......... .......... .......... .......... 40% 10.3M 28s
207400K .......... .......... .......... .......... .......... 40% 15.6M 28s
207450K .......... .......... .......... .......... .......... 40% 16.0M 28s
207500K .......... .......... .......... .......... .......... 40% 14.6M 28s
207550K .......... .......... .......... .......... .......... 40% 15.2M 28s
207600K .......... .......... .......... .......... .......... 40% 12.5M 28s
207650K .......... .......... .......... .......... .......... 40% 24.5M 28s
207700K .......... .......... .......... .......... .......... 40% 33.0M 28s
207750K .......... .......... .......... .......... .......... 40% 24.7M 28s
207800K .......... .......... .......... .......... .......... 40%  218M 28s
207850K .......... .......... .......... .......... .......... 40% 43.0M 28s
207900K .......... .......... .......... .......... .......... 40% 23.3M 28s
207950K .......... .......... .......... .......... .......... 40%  103M 28s
208000K .......... .......... .......... .......... .......... 40% 36.4M 28s
208050K .......... .......... .......... .......... .......... 40% 23.2M 28s
208100K .......... .......... .......... .......... .......... 40% 23.8M 28s
208150K .......... .......... .......... .......... .......... 40% 17.7M 28s
208200K .......... .......... .......... .......... .......... 40% 20.3M 28s
208250K .......... .......... .......... .......... .......... 40% 30.6M 28s
208300K .......... .......... .......... .......... .......... 40% 18.7M 28s
208350K .......... .......... .......... .......... .......... 40% 19.1M 28s
208400K .......... .......... .......... .......... .......... 40% 17.7M 28s
208450K .......... .......... .......... .......... .......... 41% 15.6M 28s
208500K .......... .......... .......... .......... .......... 41% 17.5M 28s
208550K .......... .......... .......... .......... .......... 41% 16.8M 28s
208600K .......... .......... .......... .......... .......... 41% 14.0M 28s
208650K .......... .......... .......... .......... .......... 41% 16.4M 28s
208700K .......... .......... .......... .......... .......... 41% 12.0M 28s
208750K .......... .......... .......... .......... .......... 41% 16.2M 28s
208800K .......... .......... .......... .......... .......... 41% 16.6M 28s
208850K .......... .......... .......... .......... .......... 41% 9.90M 28s
208900K .......... .......... .......... .......... .......... 41% 14.3M 28s
208950K .......... .......... .......... .......... .......... 41% 13.5M 28s
209000K .......... .......... .......... .......... .......... 41% 15.0M 28s
209050K .......... .......... .......... .......... .......... 41% 16.4M 28s
209100K .......... .......... .......... .......... .......... 41% 9.57M 28s
209150K .......... .......... .......... .......... .......... 41% 10.2M 28s
209200K .......... .......... .......... .......... .......... 41% 11.6M 28s
209250K .......... .......... .......... .......... .......... 41% 7.78M 28s
209300K .......... .......... .......... .......... .......... 41% 10.3M 28s
209350K .......... .......... .......... .......... .......... 41% 7.52M 28s
209400K .......... .......... .......... .......... .......... 41% 6.87M 28s
209450K .......... .......... .......... .......... .......... 41% 6.38M 28s
209500K .......... .......... .......... .......... .......... 41% 6.94M 28s
209550K .......... .......... .......... .......... .......... 41% 7.34M 28s
209600K .......... .......... .......... .......... .......... 41% 5.84M 28s
209650K .......... .......... .......... .......... .......... 41% 5.49M 28s
209700K .......... .......... .......... .......... .......... 41% 9.15M 28s
209750K .......... .......... .......... .......... .......... 41% 10.6M 28s
209800K .......... .......... .......... .......... .......... 41% 8.98M 28s
209850K .......... .......... .......... .......... .......... 41% 9.62M 28s
209900K .......... .......... .......... .......... .......... 41% 10.7M 28s
209950K .......... .......... .......... .......... .......... 41% 6.39M 28s
210000K .......... .......... .......... .......... .......... 41% 7.78M 28s
210050K .......... .......... .......... .......... .......... 41% 8.17M 28s
210100K .......... .......... .......... .......... .......... 41% 7.54M 28s
210150K .......... .......... .......... .......... .......... 41% 7.04M 28s
210200K .......... .......... .......... .......... .......... 41% 7.72M 28s
210250K .......... .......... .......... .......... .......... 41% 7.65M 28s
210300K .......... .......... .......... .......... .......... 41% 5.79M 28s
210350K .......... .......... .......... .......... .......... 41% 5.95M 28s
210400K .......... .......... .......... .......... .......... 41% 6.66M 28s
210450K .......... .......... .......... .......... .......... 41% 6.55M 28s
210500K .......... .......... .......... .......... .......... 41% 7.08M 28s
210550K .......... .......... .......... .......... .......... 41% 5.55M 28s
210600K .......... .......... .......... .......... .......... 41% 6.57M 28s
210650K .......... .......... .......... .......... .......... 41% 4.70M 28s
210700K .......... .......... .......... .......... .......... 41% 5.49M 28s
210750K .......... .......... .......... .......... .......... 41% 5.58M 28s
210800K .......... .......... .......... .......... .......... 41% 10.6M 28s
210850K .......... .......... .......... .......... .......... 41% 10.2M 28s
210900K .......... .......... .......... .......... .......... 41% 14.0M 28s
210950K .......... .......... .......... .......... .......... 41% 10.2M 28s
211000K .......... .......... .......... .......... .......... 41% 14.9M 28s
211050K .......... .......... .......... .......... .......... 41% 13.1M 28s
211100K .......... .......... .......... .......... .......... 41% 10.6M 28s
211150K .......... .......... .......... .......... .......... 41% 15.9M 28s
211200K .......... .......... .......... .......... .......... 41% 14.4M 28s
211250K .......... .......... .......... .......... .......... 41% 23.4M 28s
211300K .......... .......... .......... .......... .......... 41% 17.2M 28s
211350K .......... .......... .......... .......... .......... 41% 13.6M 28s
211400K .......... .......... .......... .......... .......... 41% 18.0M 28s
211450K .......... .......... .......... .......... .......... 41% 15.9M 28s
211500K .......... .......... .......... .......... .......... 41% 16.3M 28s
211550K .......... .......... .......... .......... .......... 41% 15.4M 28s
211600K .......... .......... .......... .......... .......... 41% 12.4M 28s
211650K .......... .......... .......... .......... .......... 41% 17.9M 28s
211700K .......... .......... .......... .......... .......... 41% 11.9M 28s
211750K .......... .......... .......... .......... .......... 41% 13.1M 28s
211800K .......... .......... .......... .......... .......... 41% 13.7M 28s
211850K .......... .......... .......... .......... .......... 41% 11.8M 28s
211900K .......... .......... .......... .......... .......... 41% 12.7M 28s
211950K .......... .......... .......... .......... .......... 41% 7.14M 28s
212000K .......... .......... .......... .......... .......... 41% 39.8M 27s
212050K .......... .......... .......... .......... .......... 41% 12.4M 27s
212100K .......... .......... .......... .......... .......... 41% 10.2M 27s
212150K .......... .......... .......... .......... .......... 41% 17.5M 27s
212200K .......... .......... .......... .......... .......... 41% 29.6M 27s
212250K .......... .......... .......... .......... .......... 41% 39.9M 27s
212300K .......... .......... .......... .......... .......... 41% 45.8M 27s
212350K .......... .......... .......... .......... .......... 41% 39.3M 27s
212400K .......... .......... .......... .......... .......... 41% 49.1M 27s
212450K .......... .......... .......... .......... .......... 41% 23.0M 27s
212500K .......... .......... .......... .......... .......... 41%  162M 27s
212550K .......... .......... .......... .......... .......... 41% 31.5M 27s
212600K .......... .......... .......... .......... .......... 41% 24.0M 27s
212650K .......... .......... .......... .......... .......... 41% 23.4M 27s
212700K .......... .......... .......... .......... .......... 41% 20.3M 27s
212750K .......... .......... .......... .......... .......... 41% 20.8M 27s
212800K .......... .......... .......... .......... .......... 41% 20.8M 27s
212850K .......... .......... .......... .......... .......... 41% 20.3M 27s
212900K .......... .......... .......... .......... .......... 41% 23.4M 27s
212950K .......... .......... .......... .......... .......... 41% 20.8M 27s
213000K .......... .......... .......... .......... .......... 41% 24.5M 27s
213050K .......... .......... .......... .......... .......... 41% 24.7M 27s
213100K .......... .......... .......... .......... .......... 41% 21.8M 27s
213150K .......... .......... .......... .......... .......... 41% 14.4M 27s
213200K .......... .......... .......... .......... .......... 41% 18.0M 27s
213250K .......... .......... .......... .......... .......... 41% 12.1M 27s
213300K .......... .......... .......... .......... .......... 41% 9.02M 27s
213350K .......... .......... .......... .......... .......... 41% 7.67M 27s
213400K .......... .......... .......... .......... .......... 41% 8.96M 27s
213450K .......... .......... .......... .......... .......... 41% 7.53M 27s
213500K .......... .......... .......... .......... .......... 42% 7.60M 27s
213550K .......... .......... .......... .......... .......... 42% 8.53M 27s
213600K .......... .......... .......... .......... .......... 42% 6.57M 27s
213650K .......... .......... .......... .......... .......... 42% 7.06M 27s
213700K .......... .......... .......... .......... .......... 42% 5.66M 27s
213750K .......... .......... .......... .......... .......... 42% 6.76M 27s
213800K .......... .......... .......... .......... .......... 42% 6.08M 27s
213850K .......... .......... .......... .......... .......... 42% 6.56M 27s
213900K .......... .......... .......... .......... .......... 42% 6.36M 27s
213950K .......... .......... .......... .......... .......... 42% 5.76M 27s
214000K .......... .......... .......... .......... .......... 42% 7.32M 27s
214050K .......... .......... .......... .......... .......... 42% 7.15M 27s
214100K .......... .......... .......... .......... .......... 42% 20.0M 27s
214150K .......... .......... .......... .......... .......... 42% 19.5M 27s
214200K .......... .......... .......... .......... .......... 42% 18.3M 27s
214250K .......... .......... .......... .......... .......... 42% 39.4M 27s
214300K .......... .......... .......... .......... .......... 42% 10.8M 27s
214350K .......... .......... .......... .......... .......... 42% 12.5M 27s
214400K .......... .......... .......... .......... .......... 42% 6.81M 27s
214450K .......... .......... .......... .......... .......... 42% 7.17M 27s
214500K .......... .......... .......... .......... .......... 42% 8.90M 27s
214550K .......... .......... .......... .......... .......... 42% 7.59M 27s
214600K .......... .......... .......... .......... .......... 42% 6.24M 27s
214650K .......... .......... .......... .......... .......... 42% 9.44M 27s
214700K .......... .......... .......... .......... .......... 42% 10.1M 27s
214750K .......... .......... .......... .......... .......... 42% 12.4M 27s
214800K .......... .......... .......... .......... .......... 42% 11.2M 27s
214850K .......... .......... .......... .......... .......... 42% 9.69M 27s
214900K .......... .......... .......... .......... .......... 42% 10.3M 27s
214950K .......... .......... .......... .......... .......... 42% 8.70M 27s
215000K .......... .......... .......... .......... .......... 42% 11.8M 27s
215050K .......... .......... .......... .......... .......... 42% 10.0M 27s
215100K .......... .......... .......... .......... .......... 42% 7.88M 27s
215150K .......... .......... .......... .......... .......... 42% 8.86M 27s
215200K .......... .......... .......... .......... .......... 42% 7.89M 27s
215250K .......... .......... .......... .......... .......... 42% 9.30M 27s
215300K .......... .......... .......... .......... .......... 42% 7.74M 27s
215350K .......... .......... .......... .......... .......... 42% 4.58M 27s
215400K .......... .......... .......... .......... .......... 42% 6.17M 27s
215450K .......... .......... .......... .......... .......... 42% 5.20M 27s
215500K .......... .......... .......... .......... .......... 42% 4.29M 27s
215550K .......... .......... .......... .......... .......... 42% 8.69M 27s
215600K .......... .......... .......... .......... .......... 42% 7.11M 27s
215650K .......... .......... .......... .......... .......... 42% 8.21M 27s
215700K .......... .......... .......... .......... .......... 42% 9.66M 27s
215750K .......... .......... .......... .......... .......... 42% 12.1M 27s
215800K .......... .......... .......... .......... .......... 42% 11.7M 27s
215850K .......... .......... .......... .......... .......... 42% 8.10M 27s
215900K .......... .......... .......... .......... .......... 42% 9.30M 27s
215950K .......... .......... .......... .......... .......... 42% 5.82M 27s
216000K .......... .......... .......... .......... .......... 42% 7.15M 27s
216050K .......... .......... .......... .......... .......... 42% 6.81M 27s
216100K .......... .......... .......... .......... .......... 42% 5.27M 27s
216150K .......... .......... .......... .......... .......... 42% 10.9M 27s
216200K .......... .......... .......... .......... .......... 42% 33.7M 27s
216250K .......... .......... .......... .......... .......... 42% 25.5M 27s
216300K .......... .......... .......... .......... .......... 42% 23.8M 27s
216350K .......... .......... .......... .......... .......... 42% 16.2M 27s
216400K .......... .......... .......... .......... .......... 42% 26.0M 27s
216450K .......... .......... .......... .......... .......... 42% 17.9M 27s
216500K .......... .......... .......... .......... .......... 42% 22.2M 27s
216550K .......... .......... .......... .......... .......... 42% 24.7M 27s
216600K .......... .......... .......... .......... .......... 42% 18.4M 27s
216650K .......... .......... .......... .......... .......... 42% 18.4M 27s
216700K .......... .......... .......... .......... .......... 42% 20.7M 27s
216750K .......... .......... .......... .......... .......... 42% 21.5M 27s
216800K .......... .......... .......... .......... .......... 42% 20.2M 27s
216850K .......... .......... .......... .......... .......... 42% 18.6M 27s
216900K .......... .......... .......... .......... .......... 42% 17.0M 27s
216950K .......... .......... .......... .......... .......... 42% 18.0M 27s
217000K .......... .......... .......... .......... .......... 42% 14.3M 27s
217050K .......... .......... .......... .......... .......... 42% 10.8M 27s
217100K .......... .......... .......... .......... .......... 42% 8.23M 27s
217150K .......... .......... .......... .......... .......... 42% 8.27M 27s
217200K .......... .......... .......... .......... .......... 42% 7.13M 27s
217250K .......... .......... .......... .......... .......... 42% 7.49M 27s
217300K .......... .......... .......... .......... .......... 42% 7.74M 27s
217350K .......... .......... .......... .......... .......... 42% 6.71M 27s
217400K .......... .......... .......... .......... .......... 42% 14.6M 27s
217450K .......... .......... .......... .......... .......... 42% 7.96M 27s
217500K .......... .......... .......... .......... .......... 42% 12.0M 27s
217550K .......... .......... .......... .......... .......... 42% 14.6M 27s
217600K .......... .......... .......... .......... .......... 42% 9.20M 27s
217650K .......... .......... .......... .......... .......... 42% 9.23M 27s
217700K .......... .......... .......... .......... .......... 42% 7.22M 27s
217750K .......... .......... .......... .......... .......... 42% 8.99M 27s
217800K .......... .......... .......... .......... .......... 42% 11.0M 27s
217850K .......... .......... .......... .......... .......... 42% 5.38M 27s
217900K .......... .......... .......... .......... .......... 42% 5.78M 27s
217950K .......... .......... .......... .......... .......... 42% 6.55M 27s
218000K .......... .......... .......... .......... .......... 42% 9.14M 27s
218050K .......... .......... .......... .......... .......... 42% 9.70M 27s
218100K .......... .......... .......... .......... .......... 42% 9.09M 27s
218150K .......... .......... .......... .......... .......... 42% 8.98M 27s
218200K .......... .......... .......... .......... .......... 42% 3.48M 27s
218250K .......... .......... .......... .......... .......... 42% 3.73M 27s
218300K .......... .......... .......... .......... .......... 42% 3.99M 27s
218350K .......... .......... .......... .......... .......... 42% 11.9M 27s
218400K .......... .......... .......... .......... .......... 42% 22.2M 27s
218450K .......... .......... .......... .......... .......... 42% 45.8M 27s
218500K .......... .......... .......... .......... .......... 42% 26.8M 27s
218550K .......... .......... .......... .......... .......... 42% 28.2M 27s
218600K .......... .......... .......... .......... .......... 43% 19.3M 27s
218650K .......... .......... .......... .......... .......... 43% 19.0M 27s
218700K .......... .......... .......... .......... .......... 43% 11.9M 27s
218750K .......... .......... .......... .......... .......... 43% 13.0M 27s
218800K .......... .......... .......... .......... .......... 43% 10.9M 27s
218850K .......... .......... .......... .......... .......... 43% 11.3M 27s
218900K .......... .......... .......... .......... .......... 43% 12.4M 27s
218950K .......... .......... .......... .......... .......... 43% 15.2M 27s
219000K .......... .......... .......... .......... .......... 43% 11.6M 27s
219050K .......... .......... .......... .......... .......... 43% 11.3M 27s
219100K .......... .......... .......... .......... .......... 43% 9.29M 27s
219150K .......... .......... .......... .......... .......... 43% 16.1M 27s
219200K .......... .......... .......... .......... .......... 43% 10.6M 27s
219250K .......... .......... .......... .......... .......... 43% 14.3M 27s
219300K .......... .......... .......... .......... .......... 43% 12.3M 27s
219350K .......... .......... .......... .......... .......... 43% 11.3M 27s
219400K .......... .......... .......... .......... .......... 43% 13.4M 27s
219450K .......... .......... .......... .......... .......... 43% 10.4M 27s
219500K .......... .......... .......... .......... .......... 43% 14.0M 27s
219550K .......... .......... .......... .......... .......... 43% 30.8M 27s
219600K .......... .......... .......... .......... .......... 43% 36.4M 27s
219650K .......... .......... .......... .......... .......... 43% 21.7M 27s
219700K .......... .......... .......... .......... .......... 43% 49.5M 27s
219750K .......... .......... .......... .......... .......... 43% 35.9M 27s
219800K .......... .......... .......... .......... .......... 43% 24.4M 27s
219850K .......... .......... .......... .......... .......... 43% 25.8M 27s
219900K .......... .......... .......... .......... .......... 43% 15.1M 27s
219950K .......... .......... .......... .......... .......... 43% 17.9M 27s
220000K .......... .......... .......... .......... .......... 43% 15.3M 27s
220050K .......... .......... .......... .......... .......... 43% 16.7M 27s
220100K .......... .......... .......... .......... .......... 43% 15.8M 27s
220150K .......... .......... .......... .......... .......... 43% 16.1M 27s
220200K .......... .......... .......... .......... .......... 43% 13.5M 27s
220250K .......... .......... .......... .......... .......... 43% 20.9M 27s
220300K .......... .......... .......... .......... .......... 43% 16.0M 27s
220350K .......... .......... .......... .......... .......... 43% 13.7M 27s
220400K .......... .......... .......... .......... .......... 43% 13.5M 27s
220450K .......... .......... .......... .......... .......... 43% 9.08M 27s
220500K .......... .......... .......... .......... .......... 43% 11.3M 27s
220550K .......... .......... .......... .......... .......... 43% 9.85M 27s
220600K .......... .......... .......... .......... .......... 43% 7.23M 27s
220650K .......... .......... .......... .......... .......... 43% 7.78M 27s
220700K .......... .......... .......... .......... .......... 43% 7.08M 27s
220750K .......... .......... .......... .......... .......... 43% 6.54M 27s
220800K .......... .......... .......... .......... .......... 43% 7.00M 27s
220850K .......... .......... .......... .......... .......... 43% 5.79M 27s
220900K .......... .......... .......... .......... .......... 43% 6.39M 27s
220950K .......... .......... .......... .......... .......... 43% 6.05M 27s
221000K .......... .......... .......... .......... .......... 43% 12.4M 27s
221050K .......... .......... .......... .......... .......... 43% 22.9M 27s
221100K .......... .......... .......... .......... .......... 43% 14.2M 27s
221150K .......... .......... .......... .......... .......... 43% 13.7M 27s
221200K .......... .......... .......... .......... .......... 43% 10.7M 27s
221250K .......... .......... .......... .......... .......... 43% 14.1M 27s
221300K .......... .......... .......... .......... .......... 43% 11.4M 27s
221350K .......... .......... .......... .......... .......... 43% 11.1M 27s
221400K .......... .......... .......... .......... .......... 43% 8.55M 27s
221450K .......... .......... .......... .......... .......... 43% 10.0M 27s
221500K .......... .......... .......... .......... .......... 43% 8.45M 27s
221550K .......... .......... .......... .......... .......... 43% 7.59M 27s
221600K .......... .......... .......... .......... .......... 43% 7.04M 27s
221650K .......... .......... .......... .......... .......... 43% 7.99M 27s
221700K .......... .......... .......... .......... .......... 43% 7.22M 27s
221750K .......... .......... .......... .......... .......... 43% 8.55M 27s
221800K .......... .......... .......... .......... .......... 43% 13.8M 27s
221850K .......... .......... .......... .......... .......... 43% 18.4M 27s
221900K .......... .......... .......... .......... .......... 43% 95.2M 27s
221950K .......... .......... .......... .......... .......... 43% 30.3M 27s
222000K .......... .......... .......... .......... .......... 43% 26.5M 27s
222050K .......... .......... .......... .......... .......... 43% 40.7M 27s
222100K .......... .......... .......... .......... .......... 43% 16.2M 27s
222150K .......... .......... .......... .......... .......... 43% 19.8M 27s
222200K .......... .......... .......... .......... .......... 43% 17.1M 27s
222250K .......... .......... .......... .......... .......... 43% 22.6M 27s
222300K .......... .......... .......... .......... .......... 43% 18.7M 27s
222350K .......... .......... .......... .......... .......... 43% 17.6M 26s
222400K .......... .......... .......... .......... .......... 43% 14.2M 26s
222450K .......... .......... .......... .......... .......... 43% 15.4M 26s
222500K .......... .......... .......... .......... .......... 43% 20.3M 26s
222550K .......... .......... .......... .......... .......... 43% 18.4M 26s
222600K .......... .......... .......... .......... .......... 43% 13.8M 26s
222650K .......... .......... .......... .......... .......... 43% 15.7M 26s
222700K .......... .......... .......... .......... .......... 43% 12.2M 26s
222750K .......... .......... .......... .......... .......... 43% 9.33M 26s
222800K .......... .......... .......... .......... .......... 43% 8.12M 26s
222850K .......... .......... .......... .......... .......... 43% 9.35M 26s
222900K .......... .......... .......... .......... .......... 43% 10.1M 26s
222950K .......... .......... .......... .......... .......... 43% 8.85M 26s
223000K .......... .......... .......... .......... .......... 43% 8.56M 26s
223050K .......... .......... .......... .......... .......... 43% 8.14M 26s
223100K .......... .......... .......... .......... .......... 43% 9.53M 26s
223150K .......... .......... .......... .......... .......... 43% 7.98M 26s
223200K .......... .......... .......... .......... .......... 43% 9.22M 26s
223250K .......... .......... .......... .......... .......... 43% 12.7M 26s
223300K .......... .......... .......... .......... .......... 43% 10.2M 26s
223350K .......... .......... .......... .......... .......... 43% 7.06M 26s
223400K .......... .......... .......... .......... .......... 43% 9.13M 26s
223450K .......... .......... .......... .......... .......... 43% 9.28M 26s
223500K .......... .......... .......... .......... .......... 43% 13.2M 26s
223550K .......... .......... .......... .......... .......... 43% 16.5M 26s
223600K .......... .......... .......... .......... .......... 43% 10.9M 26s
223650K .......... .......... .......... .......... .......... 43% 13.3M 26s
223700K .......... .......... .......... .......... .......... 44% 9.25M 26s
223750K .......... .......... .......... .......... .......... 44% 8.68M 26s
223800K .......... .......... .......... .......... .......... 44% 10.8M 26s
223850K .......... .......... .......... .......... .......... 44% 11.2M 26s
223900K .......... .......... .......... .......... .......... 44% 14.8M 26s
223950K .......... .......... .......... .......... .......... 44% 8.64M 26s
224000K .......... .......... .......... .......... .......... 44% 12.1M 26s
224050K .......... .......... .......... .......... .......... 44% 11.1M 26s
224100K .......... .......... .......... .......... .......... 44% 8.27M 26s
224150K .......... .......... .......... .......... .......... 44% 8.95M 26s
224200K .......... .......... .......... .......... .......... 44% 6.68M 26s
224250K .......... .......... .......... .......... .......... 44% 9.23M 26s
224300K .......... .......... .......... .......... .......... 44% 6.66M 26s
224350K .......... .......... .......... .......... .......... 44% 7.05M 26s
224400K .......... .......... .......... .......... .......... 44% 15.1M 26s
224450K .......... .......... .......... .......... .......... 44% 11.2M 26s
224500K .......... .......... .......... .......... .......... 44% 14.8M 26s
224550K .......... .......... .......... .......... .......... 44% 14.2M 26s
224600K .......... .......... .......... .......... .......... 44% 11.7M 26s
224650K .......... .......... .......... .......... .......... 44% 14.4M 26s
224700K .......... .......... .......... .......... .......... 44% 12.6M 26s
224750K .......... .......... .......... .......... .......... 44% 13.0M 26s
224800K .......... .......... .......... .......... .......... 44% 15.9M 26s
224850K .......... .......... .......... .......... .......... 44% 25.2M 26s
224900K .......... .......... .......... .......... .......... 44% 27.8M 26s
224950K .......... .......... .......... .......... .......... 44% 36.4M 26s
225000K .......... .......... .......... .......... .......... 44% 60.6M 26s
225050K .......... .......... .......... .......... .......... 44% 21.9M 26s
225100K .......... .......... .......... .......... .......... 44% 15.3M 26s
225150K .......... .......... .......... .......... .......... 44% 33.4M 26s
225200K .......... .......... .......... .......... .......... 44% 22.9M 26s
225250K .......... .......... .......... .......... .......... 44% 16.3M 26s
225300K .......... .......... .......... .......... .......... 44% 45.8M 26s
225350K .......... .......... .......... .......... .......... 44% 22.6M 26s
225400K .......... .......... .......... .......... .......... 44% 19.5M 26s
225450K .......... .......... .......... .......... .......... 44% 14.7M 26s
225500K .......... .......... .......... .......... .......... 44% 21.7M 26s
225550K .......... .......... .......... .......... .......... 44% 17.3M 26s
225600K .......... .......... .......... .......... .......... 44% 14.3M 26s
225650K .......... .......... .......... .......... .......... 44% 17.6M 26s
225700K .......... .......... .......... .......... .......... 44% 14.8M 26s
225750K .......... .......... .......... .......... .......... 44% 16.7M 26s
225800K .......... .......... .......... .......... .......... 44% 13.2M 26s
225850K .......... .......... .......... .......... .......... 44% 9.59M 26s
225900K .......... .......... .......... .......... .......... 44% 12.0M 26s
225950K .......... .......... .......... .......... .......... 44% 10.2M 26s
226000K .......... .......... .......... .......... .......... 44% 13.1M 26s
226050K .......... .......... .......... .......... .......... 44% 9.24M 26s
226100K .......... .......... .......... .......... .......... 44% 11.6M 26s
226150K .......... .......... .......... .......... .......... 44% 10.4M 26s
226200K .......... .......... .......... .......... .......... 44% 8.45M 26s
226250K .......... .......... .......... .......... .......... 44% 13.2M 26s
226300K .......... .......... .......... .......... .......... 44% 10.4M 26s
226350K .......... .......... .......... .......... .......... 44% 11.1M 26s
226400K .......... .......... .......... .......... .......... 44% 12.2M 26s
226450K .......... .......... .......... .......... .......... 44% 10.6M 26s
226500K .......... .......... .......... .......... .......... 44% 12.9M 26s
226550K .......... .......... .......... .......... .......... 44% 10.7M 26s
226600K .......... .......... .......... .......... .......... 44% 10.8M 26s
226650K .......... .......... .......... .......... .......... 44% 11.4M 26s
226700K .......... .......... .......... .......... .......... 44% 8.59M 26s
226750K .......... .......... .......... .......... .......... 44% 7.59M 26s
226800K .......... .......... .......... .......... .......... 44% 8.98M 26s
226850K .......... .......... .......... .......... .......... 44% 6.10M 26s
226900K .......... .......... .......... .......... .......... 44% 6.37M 26s
226950K .......... .......... .......... .......... .......... 44% 5.82M 26s
227000K .......... .......... .......... .......... .......... 44% 6.81M 26s
227050K .......... .......... .......... .......... .......... 44% 5.15M 26s
227100K .......... .......... .......... .......... .......... 44% 9.09M 26s
227150K .......... .......... .......... .......... .......... 44% 11.8M 26s
227200K .......... .......... .......... .......... .......... 44% 9.19M 26s
227250K .......... .......... .......... .......... .......... 44% 8.00M 26s
227300K .......... .......... .......... .......... .......... 44% 3.55M 26s
227350K .......... .......... .......... .......... .......... 44% 3.11M 26s
227400K .......... .......... .......... .......... .......... 44% 3.57M 26s
227450K .......... .......... .......... .......... .......... 44% 3.44M 26s
227500K .......... .......... .......... .......... .......... 44% 3.72M 26s
227550K .......... .......... .......... .......... .......... 44% 5.85M 26s
227600K .......... .......... .......... .......... .......... 44% 15.6M 26s
227650K .......... .......... .......... .......... .......... 44% 10.5M 26s
227700K .......... .......... .......... .......... .......... 44% 9.31M 26s
227750K .......... .......... .......... .......... .......... 44% 12.0M 26s
227800K .......... .......... .......... .......... .......... 44% 11.3M 26s
227850K .......... .......... .......... .......... .......... 44% 8.95M 26s
227900K .......... .......... .......... .......... .......... 44% 11.9M 26s
227950K .......... .......... .......... .......... .......... 44% 7.09M 26s
228000K .......... .......... .......... .......... .......... 44% 10.5M 26s
228050K .......... .......... .......... .......... .......... 44% 9.98M 26s
228100K .......... .......... .......... .......... .......... 44% 9.91M 26s
228150K .......... .......... .......... .......... .......... 44% 12.1M 26s
228200K .......... .......... .......... .......... .......... 44% 7.33M 26s
228250K .......... .......... .......... .......... .......... 44% 9.41M 26s
228300K .......... .......... .......... .......... .......... 44% 9.59M 26s
228350K .......... .......... .......... .......... .......... 44% 7.78M 26s
228400K .......... .......... .......... .......... .......... 44% 8.89M 26s
228450K .......... .......... .......... .......... .......... 44% 7.49M 26s
228500K .......... .......... .......... .......... .......... 44% 15.4M 26s
228550K .......... .......... .......... .......... .......... 44% 21.5M 26s
228600K .......... .......... .......... .......... .......... 44% 46.1M 26s
228650K .......... .......... .......... .......... .......... 44% 33.7M 26s
228700K .......... .......... .......... .......... .......... 44% 26.2M 26s
228750K .......... .......... .......... .......... .......... 45% 29.1M 26s
228800K .......... .......... .......... .......... .......... 45% 43.4M 26s
228850K .......... .......... .......... .......... .......... 45% 18.1M 26s
228900K .......... .......... .......... .......... .......... 45% 14.9M 26s
228950K .......... .......... .......... .......... .......... 45% 16.0M 26s
229000K .......... .......... .......... .......... .......... 45% 15.2M 26s
229050K .......... .......... .......... .......... .......... 45% 21.6M 26s
229100K .......... .......... .......... .......... .......... 45% 15.1M 26s
229150K .......... .......... .......... .......... .......... 45% 15.3M 26s
229200K .......... .......... .......... .......... .......... 45% 13.7M 26s
229250K .......... .......... .......... .......... .......... 45% 9.31M 26s
229300K .......... .......... .......... .......... .......... 45% 11.0M 26s
229350K .......... .......... .......... .......... .......... 45% 5.61M 26s
229400K .......... .......... .......... .......... .......... 45% 14.1M 26s
229450K .......... .......... .......... .......... .......... 45% 7.03M 26s
229500K .......... .......... .......... .......... .......... 45% 11.3M 26s
229550K .......... .......... .......... .......... .......... 45% 9.03M 26s
229600K .......... .......... .......... .......... .......... 45% 7.57M 26s
229650K .......... .......... .......... .......... .......... 45% 10.8M 26s
229700K .......... .......... .......... .......... .......... 45% 20.7M 26s
229750K .......... .......... .......... .......... .......... 45% 24.4M 26s
229800K .......... .......... .......... .......... .......... 45% 21.0M 26s
229850K .......... .......... .......... .......... .......... 45% 28.5M 26s
229900K .......... .......... .......... .......... .......... 45% 20.6M 26s
229950K .......... .......... .......... .......... .......... 45% 11.3M 26s
230000K .......... .......... .......... .......... .......... 45% 15.8M 26s
230050K .......... .......... .......... .......... .......... 45% 17.0M 26s
230100K .......... .......... .......... .......... .......... 45% 11.7M 26s
230150K .......... .......... .......... .......... .......... 45% 15.5M 26s
230200K .......... .......... .......... .......... .......... 45% 9.94M 26s
230250K .......... .......... .......... .......... .......... 45% 10.4M 26s
230300K .......... .......... .......... .......... .......... 45% 15.5M 26s
230350K .......... .......... .......... .......... .......... 45% 9.98M 26s
230400K .......... .......... .......... .......... .......... 45% 9.35M 26s
230450K .......... .......... .......... .......... .......... 45% 7.74M 26s
230500K .......... .......... .......... .......... .......... 45% 7.96M 26s
230550K .......... .......... .......... .......... .......... 45% 9.44M 26s
230600K .......... .......... .......... .......... .......... 45% 7.83M 26s
230650K .......... .......... .......... .......... .......... 45% 7.78M 26s
230700K .......... .......... .......... .......... .......... 45% 8.61M 26s
230750K .......... .......... .......... .......... .......... 45% 10.9M 26s
230800K .......... .......... .......... .......... .......... 45% 7.93M 26s
230850K .......... .......... .......... .......... .......... 45% 8.90M 26s
230900K .......... .......... .......... .......... .......... 45% 10.2M 26s
230950K .......... .......... .......... .......... .......... 45% 7.70M 26s
231000K .......... .......... .......... .......... .......... 45% 9.11M 26s
231050K .......... .......... .......... .......... .......... 45% 9.11M 26s
231100K .......... .......... .......... .......... .......... 45% 6.42M 26s
231150K .......... .......... .......... .......... .......... 45% 6.22M 26s
231200K .......... .......... .......... .......... .......... 45% 5.93M 26s
231250K .......... .......... .......... .......... .......... 45% 6.60M 26s
231300K .......... .......... .......... .......... .......... 45% 7.01M 26s
231350K .......... .......... .......... .......... .......... 45% 7.85M 26s
231400K .......... .......... .......... .......... .......... 45% 19.5M 26s
231450K .......... .......... .......... .......... .......... 45% 31.1M 26s
231500K .......... .......... .......... .......... .......... 45% 26.5M 26s
231550K .......... .......... .......... .......... .......... 45% 18.6M 26s
231600K .......... .......... .......... .......... .......... 45% 17.3M 26s
231650K .......... .......... .......... .......... .......... 45% 14.7M 26s
231700K .......... .......... .......... .......... .......... 45% 7.56M 26s
231750K .......... .......... .......... .......... .......... 45% 8.37M 26s
231800K .......... .......... .......... .......... .......... 45% 7.55M 26s
231850K .......... .......... .......... .......... .......... 45% 6.02M 26s
231900K .......... .......... .......... .......... .......... 45% 9.19M 26s
231950K .......... .......... .......... .......... .......... 45% 5.84M 26s
232000K .......... .......... .......... .......... .......... 45% 7.39M 26s
232050K .......... .......... .......... .......... .......... 45% 6.00M 26s
232100K .......... .......... .......... .......... .......... 45% 5.07M 26s
232150K .......... .......... .......... .......... .......... 45% 5.92M 26s
232200K .......... .......... .......... .......... .......... 45% 4.76M 26s
232250K .......... .......... .......... .......... .......... 45% 14.3M 26s
232300K .......... .......... .......... .......... .......... 45% 24.8M 26s
232350K .......... .......... .......... .......... .......... 45% 20.2M 26s
232400K .......... .......... .......... .......... .......... 45% 16.4M 26s
232450K .......... .......... .......... .......... .......... 45% 10.7M 26s
232500K .......... .......... .......... .......... .......... 45% 15.0M 26s
232550K .......... .......... .......... .......... .......... 45% 14.7M 26s
232600K .......... .......... .......... .......... .......... 45% 7.54M 26s
232650K .......... .......... .......... .......... .......... 45% 7.63M 26s
232700K .......... .......... .......... .......... .......... 45% 6.11M 26s
232750K .......... .......... .......... .......... .......... 45% 7.51M 26s
232800K .......... .......... .......... .......... .......... 45% 6.01M 26s
232850K .......... .......... .......... .......... .......... 45% 5.61M 26s
232900K .......... .......... .......... .......... .......... 45% 8.05M 26s
232950K .......... .......... .......... .......... .......... 45% 6.84M 26s
233000K .......... .......... .......... .......... .......... 45% 7.44M 26s
233050K .......... .......... .......... .......... .......... 45% 7.80M 26s
233100K .......... .......... .......... .......... .......... 45% 12.5M 26s
233150K .......... .......... .......... .......... .......... 45% 20.6M 26s
233200K .......... .......... .......... .......... .......... 45% 19.1M 26s
233250K .......... .......... .......... .......... .......... 45% 29.1M 26s
233300K .......... .......... .......... .......... .......... 45% 18.9M 26s
233350K .......... .......... .......... .......... .......... 45% 12.2M 26s
233400K .......... .......... .......... .......... .......... 45% 16.0M 26s
233450K .......... .......... .......... .......... .......... 45% 10.3M 26s
233500K .......... .......... .......... .......... .......... 45% 13.9M 26s
233550K .......... .......... .......... .......... .......... 45% 11.7M 26s
233600K .......... .......... .......... .......... .......... 45% 8.26M 26s
233650K .......... .......... .......... .......... .......... 45% 7.97M 26s
233700K .......... .......... .......... .......... .......... 45% 6.21M 25s
233750K .......... .......... .......... .......... .......... 45% 7.33M 25s
233800K .......... .......... .......... .......... .......... 45% 7.50M 25s
233850K .......... .......... .......... .......... .......... 46% 5.79M 25s
233900K .......... .......... .......... .......... .......... 46% 14.0M 25s
233950K .......... .......... .......... .......... .......... 46% 19.3M 25s
234000K .......... .......... .......... .......... .......... 46% 32.8M 25s
234050K .......... .......... .......... .......... .......... 46% 23.4M 25s
234100K .......... .......... .......... .......... .......... 46% 14.7M 25s
234150K .......... .......... .......... .......... .......... 46% 24.6M 25s
234200K .......... .......... .......... .......... .......... 46% 20.1M 25s
234250K .......... .......... .......... .......... .......... 46% 24.2M 25s
234300K .......... .......... .......... .......... .......... 46% 19.0M 25s
234350K .......... .......... .......... .......... .......... 46% 12.9M 25s
234400K .......... .......... .......... .......... .......... 46% 18.1M 25s
234450K .......... .......... .......... .......... .......... 46% 9.82M 25s
234500K .......... .......... .......... .......... .......... 46% 24.4M 25s
234550K .......... .......... .......... .......... .......... 46% 14.3M 25s
234600K .......... .......... .......... .......... .......... 46% 12.4M 25s
234650K .......... .......... .......... .......... .......... 46% 13.6M 25s
234700K .......... .......... .......... .......... .......... 46% 6.66M 25s
234750K .......... .......... .......... .......... .......... 46% 7.69M 25s
234800K .......... .......... .......... .......... .......... 46% 12.0M 25s
234850K .......... .......... .......... .......... .......... 46% 11.9M 25s
234900K .......... .......... .......... .......... .......... 46% 11.9M 25s
234950K .......... .......... .......... .......... .......... 46% 11.7M 25s
235000K .......... .......... .......... .......... .......... 46% 13.3M 25s
235050K .......... .......... .......... .......... .......... 46% 11.7M 25s
235100K .......... .......... .......... .......... .......... 46% 8.91M 25s
235150K .......... .......... .......... .......... .......... 46% 11.1M 25s
235200K .......... .......... .......... .......... .......... 46% 8.25M 25s
235250K .......... .......... .......... .......... .......... 46% 9.38M 25s
235300K .......... .......... .......... .......... .......... 46% 12.6M 25s
235350K .......... .......... .......... .......... .......... 46% 9.71M 25s
235400K .......... .......... .......... .......... .......... 46% 12.5M 25s
235450K .......... .......... .......... .......... .......... 46% 9.59M 25s
235500K .......... .......... .......... .......... .......... 46% 17.2M 25s
235550K .......... .......... .......... .......... .......... 46% 19.5M 25s
235600K .......... .......... .......... .......... .......... 46% 13.0M 25s
235650K .......... .......... .......... .......... .......... 46% 33.8M 25s
235700K .......... .......... .......... .......... .......... 46% 9.60M 25s
235750K .......... .......... .......... .......... .......... 46% 9.05M 25s
235800K .......... .......... .......... .......... .......... 46% 6.72M 25s
235850K .......... .......... .......... .......... .......... 46% 7.04M 25s
235900K .......... .......... .......... .......... .......... 46% 8.59M 25s
235950K .......... .......... .......... .......... .......... 46% 4.99M 25s
236000K .......... .......... .......... .......... .......... 46% 6.20M 25s
236050K .......... .......... .......... .......... .......... 46% 7.33M 25s
236100K .......... .......... .......... .......... .......... 46% 5.67M 25s
236150K .......... .......... .......... .......... .......... 46% 7.04M 25s
236200K .......... .......... .......... .......... .......... 46% 5.67M 25s
236250K .......... .......... .......... .......... .......... 46% 5.48M 25s
236300K .......... .......... .......... .......... .......... 46% 7.94M 25s
236350K .......... .......... .......... .......... .......... 46% 6.02M 25s
236400K .......... .......... .......... .......... .......... 46% 5.16M 25s
236450K .......... .......... .......... .......... .......... 46% 4.93M 25s
236500K .......... .......... .......... .......... .......... 46% 5.74M 25s
236550K .......... .......... .......... .......... .......... 46% 5.45M 25s
236600K .......... .......... .......... .......... .......... 46% 5.70M 25s
236650K .......... .......... .......... .......... .......... 46% 7.95M 25s
236700K .......... .......... .......... .......... .......... 46% 20.0M 25s
236750K .......... .......... .......... .......... .......... 46% 41.8M 25s
236800K .......... .......... .......... .......... .......... 46% 20.8M 25s
236850K .......... .......... .......... .......... .......... 46% 80.7M 25s
236900K .......... .......... .......... .......... .......... 46% 44.8M 25s
236950K .......... .......... .......... .......... .......... 46% 33.8M 25s
237000K .......... .......... .......... .......... .......... 46% 43.8M 25s
237050K .......... .......... .......... .......... .......... 46% 20.7M 25s
237100K .......... .......... .......... .......... .......... 46% 11.8M 25s
237150K .......... .......... .......... .......... .......... 46% 12.5M 25s
237200K .......... .......... .......... .......... .......... 46% 8.80M 25s
237250K .......... .......... .......... .......... .......... 46% 7.61M 25s
237300K .......... .......... .......... .......... .......... 46% 5.90M 25s
237350K .......... .......... .......... .......... .......... 46% 5.48M 25s
237400K .......... .......... .......... .......... .......... 46% 7.45M 25s
237450K .......... .......... .......... .......... .......... 46% 5.65M 25s
237500K .......... .......... .......... .......... .......... 46% 7.07M 25s
237550K .......... .......... .......... .......... .......... 46% 10.1M 25s
237600K .......... .......... .......... .......... .......... 46% 20.0M 25s
237650K .......... .......... .......... .......... .......... 46% 38.6M 25s
237700K .......... .......... .......... .......... .......... 46% 20.5M 25s
237750K .......... .......... .......... .......... .......... 46% 15.9M 25s
237800K .......... .......... .......... .......... .......... 46% 30.1M 25s
237850K .......... .......... .......... .......... .......... 46% 13.3M 25s
237900K .......... .......... .......... .......... .......... 46% 13.7M 25s
237950K .......... .......... .......... .......... .......... 46% 15.0M 25s
238000K .......... .......... .......... .......... .......... 46% 12.3M 25s
238050K .......... .......... .......... .......... .......... 46% 11.8M 25s
238100K .......... .......... .......... .......... .......... 46% 8.05M 25s
238150K .......... .......... .......... .......... .......... 46% 11.9M 25s
238200K .......... .......... .......... .......... .......... 46% 10.8M 25s
238250K .......... .......... .......... .......... .......... 46% 14.8M 25s
238300K .......... .......... .......... .......... .......... 46% 7.05M 25s
238350K .......... .......... .......... .......... .......... 46% 8.02M 25s
238400K .......... .......... .......... .......... .......... 46% 11.9M 25s
238450K .......... .......... .......... .......... .......... 46% 8.31M 25s
238500K .......... .......... .......... .......... .......... 46% 11.9M 25s
238550K .......... .......... .......... .......... .......... 46% 9.03M 25s
238600K .......... .......... .......... .......... .......... 46% 7.38M 25s
238650K .......... .......... .......... .......... .......... 46% 10.2M 25s
238700K .......... .......... .......... .......... .......... 46% 6.69M 25s
238750K .......... .......... .......... .......... .......... 46% 8.72M 25s
238800K .......... .......... .......... .......... .......... 46% 8.56M 25s
238850K .......... .......... .......... .......... .......... 46% 7.08M 25s
238900K .......... .......... .......... .......... .......... 46% 7.60M 25s
238950K .......... .......... .......... .......... .......... 47% 9.25M 25s
239000K .......... .......... .......... .......... .......... 47% 8.25M 25s
239050K .......... .......... .......... .......... .......... 47% 9.89M 25s
239100K .......... .......... .......... .......... .......... 47% 9.16M 25s
239150K .......... .......... .......... .......... .......... 47% 10.4M 25s
239200K .......... .......... .......... .......... .......... 47% 9.32M 25s
239250K .......... .......... .......... .......... .......... 47% 8.61M 25s
239300K .......... .......... .......... .......... .......... 47% 7.66M 25s
239350K .......... .......... .......... .......... .......... 47% 7.24M 25s
239400K .......... .......... .......... .......... .......... 47% 8.58M 25s
239450K .......... .......... .......... .......... .......... 47% 7.10M 25s
239500K .......... .......... .......... .......... .......... 47% 7.09M 25s
239550K .......... .......... .......... .......... .......... 47% 8.08M 25s
239600K .......... .......... .......... .......... .......... 47% 5.95M 25s
239650K .......... .......... .......... .......... .......... 47% 8.51M 25s
239700K .......... .......... .......... .......... .......... 47% 7.22M 25s
239750K .......... .......... .......... .......... .......... 47% 6.20M 25s
239800K .......... .......... .......... .......... .......... 47% 7.72M 25s
239850K .......... .......... .......... .......... .......... 47% 4.44M 25s
239900K .......... .......... .......... .......... .......... 47% 3.83M 25s
239950K .......... .......... .......... .......... .......... 47% 6.84M 25s
240000K .......... .......... .......... .......... .......... 47% 8.46M 25s
240050K .......... .......... .......... .......... .......... 47% 8.61M 25s
240100K .......... .......... .......... .......... .......... 47% 6.32M 25s
240150K .......... .......... .......... .......... .......... 47% 8.76M 25s
240200K .......... .......... .......... .......... .......... 47% 7.25M 25s
240250K .......... .......... .......... .......... .......... 47% 6.69M 25s
240300K .......... .......... .......... .......... .......... 47% 6.51M 25s
240350K .......... .......... .......... .......... .......... 47% 7.02M 25s
240400K .......... .......... .......... .......... .......... 47% 7.46M 25s
240450K .......... .......... .......... .......... .......... 47% 6.59M 25s
240500K .......... .......... .......... .......... .......... 47% 7.13M 25s
240550K .......... .......... .......... .......... .......... 47% 8.21M 25s
240600K .......... .......... .......... .......... .......... 47% 7.62M 25s
240650K .......... .......... .......... .......... .......... 47% 12.0M 25s
240700K .......... .......... .......... .......... .......... 47% 9.30M 25s
240750K .......... .......... .......... .......... .......... 47% 11.8M 25s
240800K .......... .......... .......... .......... .......... 47% 10.9M 25s
240850K .......... .......... .......... .......... .......... 47% 9.01M 25s
240900K .......... .......... .......... .......... .......... 47% 9.91M 25s
240950K .......... .......... .......... .......... .......... 47% 9.35M 25s
241000K .......... .......... .......... .......... .......... 47% 12.6M 25s
241050K .......... .......... .......... .......... .......... 47% 12.3M 25s
241100K .......... .......... .......... .......... .......... 47% 10.8M 25s
241150K .......... .......... .......... .......... .......... 47% 11.3M 25s
241200K .......... .......... .......... .......... .......... 47% 8.53M 25s
241250K .......... .......... .......... .......... .......... 47% 7.87M 25s
241300K .......... .......... .......... .......... .......... 47% 8.30M 25s
241350K .......... .......... .......... .......... .......... 47% 6.62M 25s
241400K .......... .......... .......... .......... .......... 47% 7.60M 25s
241450K .......... .......... .......... .......... .......... 47% 5.31M 25s
241500K .......... .......... .......... .......... .......... 47% 5.72M 25s
241550K .......... .......... .......... .......... .......... 47% 8.02M 25s
241600K .......... .......... .......... .......... .......... 47% 4.42M 25s
241650K .......... .......... .......... .......... .......... 47% 3.24M 25s
241700K .......... .......... .......... .......... .......... 47% 3.71M 25s
241750K .......... .......... .......... .......... .......... 47% 5.88M 25s
241800K .......... .......... .......... .......... .......... 47% 6.22M 25s
241850K .......... .......... .......... .......... .......... 47% 8.69M 25s
241900K .......... .......... .......... .......... .......... 47% 10.5M 25s
241950K .......... .......... .......... .......... .......... 47% 9.84M 25s
242000K .......... .......... .......... .......... .......... 47% 11.6M 25s
242050K .......... .......... .......... .......... .......... 47% 9.42M 25s
242100K .......... .......... .......... .......... .......... 47% 9.12M 25s
242150K .......... .......... .......... .......... .......... 47% 13.0M 25s
242200K .......... .......... .......... .......... .......... 47% 9.62M 25s
242250K .......... .......... .......... .......... .......... 47% 11.5M 25s
242300K .......... .......... .......... .......... .......... 47% 9.68M 25s
242350K .......... .......... .......... .......... .......... 47% 8.84M 25s
242400K .......... .......... .......... .......... .......... 47% 8.59M 25s
242450K .......... .......... .......... .......... .......... 47% 7.74M 25s
242500K .......... .......... .......... .......... .......... 47% 7.99M 25s
242550K .......... .......... .......... .......... .......... 47% 12.1M 25s
242600K .......... .......... .......... .......... .......... 47% 8.00M 25s
242650K .......... .......... .......... .......... .......... 47% 9.39M 25s
242700K .......... .......... .......... .......... .......... 47% 7.70M 25s
242750K .......... .......... .......... .......... .......... 47% 7.52M 25s
242800K .......... .......... .......... .......... .......... 47% 8.29M 25s
242850K .......... .......... .......... .......... .......... 47% 15.0M 25s
242900K .......... .......... .......... .......... .......... 47% 19.7M 25s
242950K .......... .......... .......... .......... .......... 47% 19.1M 25s
243000K .......... .......... .......... .......... .......... 47% 12.5M 25s
243050K .......... .......... .......... .......... .......... 47% 14.7M 25s
243100K .......... .......... .......... .......... .......... 47% 7.45M 25s
243150K .......... .......... .......... .......... .......... 47% 6.80M 25s
243200K .......... .......... .......... .......... .......... 47% 7.45M 25s
243250K .......... .......... .......... .......... .......... 47% 8.55M 25s
243300K .......... .......... .......... .......... .......... 47% 9.22M 25s
243350K .......... .......... .......... .......... .......... 47% 6.72M 25s
243400K .......... .......... .......... .......... .......... 47% 6.52M 25s
243450K .......... .......... .......... .......... .......... 47% 11.4M 25s
243500K .......... .......... .......... .......... .......... 47% 11.3M 25s
243550K .......... .......... .......... .......... .......... 47% 10.7M 25s
243600K .......... .......... .......... .......... .......... 47% 9.85M 25s
243650K .......... .......... .......... .......... .......... 47% 10.6M 25s
243700K .......... .......... .......... .......... .......... 47% 12.0M 25s
243750K .......... .......... .......... .......... .......... 47% 10.9M 25s
243800K .......... .......... .......... .......... .......... 47% 13.6M 25s
243850K .......... .......... .......... .......... .......... 47% 21.4M 25s
243900K .......... .......... .......... .......... .......... 47% 37.7M 25s
243950K .......... .......... .......... .......... .......... 47% 17.8M 25s
244000K .......... .......... .......... .......... .......... 48% 38.7M 25s
244050K .......... .......... .......... .......... .......... 48% 40.8M 25s
244100K .......... .......... .......... .......... .......... 48% 17.2M 25s
244150K .......... .......... .......... .......... .......... 48% 17.2M 25s
244200K .......... .......... .......... .......... .......... 48% 16.6M 25s
244250K .......... .......... .......... .......... .......... 48% 16.8M 25s
244300K .......... .......... .......... .......... .......... 48% 16.4M 25s
244350K .......... .......... .......... .......... .......... 48% 15.4M 25s
244400K .......... .......... .......... .......... .......... 48% 16.1M 25s
244450K .......... .......... .......... .......... .......... 48% 10.2M 25s
244500K .......... .......... .......... .......... .......... 48% 13.6M 25s
244550K .......... .......... .......... .......... .......... 48% 10.8M 25s
244600K .......... .......... .......... .......... .......... 48% 10.7M 25s
244650K .......... .......... .......... .......... .......... 48% 9.22M 25s
244700K .......... .......... .......... .......... .......... 48% 9.20M 25s
244750K .......... .......... .......... .......... .......... 48% 10.6M 25s
244800K .......... .......... .......... .......... .......... 48% 8.67M 25s
244850K .......... .......... .......... .......... .......... 48% 6.93M 25s
244900K .......... .......... .......... .......... .......... 48% 8.03M 25s
244950K .......... .......... .......... .......... .......... 48% 6.17M 25s
245000K .......... .......... .......... .......... .......... 48% 6.74M 25s
245050K .......... .......... .......... .......... .......... 48% 7.11M 25s
245100K .......... .......... .......... .......... .......... 48% 6.95M 25s
245150K .......... .......... .......... .......... .......... 48% 31.3M 25s
245200K .......... .......... .......... .......... .......... 48% 16.7M 25s
245250K .......... .......... .......... .......... .......... 48% 22.0M 25s
245300K .......... .......... .......... .......... .......... 48% 11.5M 25s
245350K .......... .......... .......... .......... .......... 48% 14.7M 25s
245400K .......... .......... .......... .......... .......... 48% 13.2M 25s
245450K .......... .......... .......... .......... .......... 48% 7.72M 25s
245500K .......... .......... .......... .......... .......... 48% 8.49M 25s
245550K .......... .......... .......... .......... .......... 48% 9.08M 25s
245600K .......... .......... .......... .......... .......... 48% 7.76M 25s
245650K .......... .......... .......... .......... .......... 48% 7.37M 25s
245700K .......... .......... .......... .......... .......... 48% 7.69M 25s
245750K .......... .......... .......... .......... .......... 48% 11.8M 25s
245800K .......... .......... .......... .......... .......... 48% 21.7M 25s
245850K .......... .......... .......... .......... .......... 48% 32.6M 25s
245900K .......... .......... .......... .......... .......... 48% 20.4M 25s
245950K .......... .......... .......... .......... .......... 48% 26.5M 25s
246000K .......... .......... .......... .......... .......... 48% 20.4M 25s
246050K .......... .......... .......... .......... .......... 48% 18.6M 24s
246100K .......... .......... .......... .......... .......... 48% 16.5M 24s
246150K .......... .......... .......... .......... .......... 48% 16.9M 24s
246200K .......... .......... .......... .......... .......... 48% 11.1M 24s
246250K .......... .......... .......... .......... .......... 48% 14.9M 24s
246300K .......... .......... .......... .......... .......... 48% 11.2M 24s
246350K .......... .......... .......... .......... .......... 48% 10.6M 24s
246400K .......... .......... .......... .......... .......... 48% 11.3M 24s
246450K .......... .......... .......... .......... .......... 48% 14.4M 24s
246500K .......... .......... .......... .......... .......... 48% 10.6M 24s
246550K .......... .......... .......... .......... .......... 48% 8.78M 24s
246600K .......... .......... .......... .......... .......... 48% 6.64M 24s
246650K .......... .......... .......... .......... .......... 48% 7.80M 24s
246700K .......... .......... .......... .......... .......... 48% 6.03M 24s
246750K .......... .......... .......... .......... .......... 48% 11.4M 24s
246800K .......... .......... .......... .......... .......... 48% 11.0M 24s
246850K .......... .......... .......... .......... .......... 48% 8.79M 24s
246900K .......... .......... .......... .......... .......... 48% 9.28M 24s
246950K .......... .......... .......... .......... .......... 48% 7.83M 24s
247000K .......... .......... .......... .......... .......... 48% 7.63M 24s
247050K .......... .......... .......... .......... .......... 48% 6.40M 24s
247100K .......... .......... .......... .......... .......... 48% 5.78M 24s
247150K .......... .......... .......... .......... .......... 48% 6.75M 24s
247200K .......... .......... .......... .......... .......... 48% 5.94M 24s
247250K .......... .......... .......... .......... .......... 48% 11.1M 24s
247300K .......... .......... .......... .......... .......... 48% 10.3M 24s
247350K .......... .......... .......... .......... .......... 48% 8.84M 24s
247400K .......... .......... .......... .......... .......... 48% 13.0M 24s
247450K .......... .......... .......... .......... .......... 48% 11.0M 24s
247500K .......... .......... .......... .......... .......... 48% 8.90M 24s
247550K .......... .......... .......... .......... .......... 48% 12.7M 24s
247600K .......... .......... .......... .......... .......... 48% 10.3M 24s
247650K .......... .......... .......... .......... .......... 48% 12.9M 24s
247700K .......... .......... .......... .......... .......... 48% 10.4M 24s
247750K .......... .......... .......... .......... .......... 48% 13.2M 24s
247800K .......... .......... .......... .......... .......... 48% 8.84M 24s
247850K .......... .......... .......... .......... .......... 48% 17.6M 24s
247900K .......... .......... .......... .......... .......... 48% 14.5M 24s
247950K .......... .......... .......... .......... .......... 48% 16.2M 24s
248000K .......... .......... .......... .......... .......... 48% 27.9M 24s
248050K .......... .......... .......... .......... .......... 48% 13.7M 24s
248100K .......... .......... .......... .......... .......... 48% 34.8M 24s
248150K .......... .......... .......... .......... .......... 48% 30.8M 24s
248200K .......... .......... .......... .......... .......... 48% 13.3M 24s
248250K .......... .......... .......... .......... .......... 48% 21.1M 24s
248300K .......... .......... .......... .......... .......... 48% 15.1M 24s
248350K .......... .......... .......... .......... .......... 48% 14.8M 24s
248400K .......... .......... .......... .......... .......... 48% 14.9M 24s
248450K .......... .......... .......... .......... .......... 48% 15.1M 24s
248500K .......... .......... .......... .......... .......... 48% 16.9M 24s
248550K .......... .......... .......... .......... .......... 48% 12.0M 24s
248600K .......... .......... .......... .......... .......... 48% 11.3M 24s
248650K .......... .......... .......... .......... .......... 48% 11.9M 24s
248700K .......... .......... .......... .......... .......... 48% 10.7M 24s
248750K .......... .......... .......... .......... .......... 48% 11.9M 24s
248800K .......... .......... .......... .......... .......... 48% 11.2M 24s
248850K .......... .......... .......... .......... .......... 48% 9.79M 24s
248900K .......... .......... .......... .......... .......... 48% 11.3M 24s
248950K .......... .......... .......... .......... .......... 48% 8.45M 24s
249000K .......... .......... .......... .......... .......... 48% 8.80M 24s
249050K .......... .......... .......... .......... .......... 48% 9.59M 24s
249100K .......... .......... .......... .......... .......... 49% 7.19M 24s
249150K .......... .......... .......... .......... .......... 49% 9.00M 24s
249200K .......... .......... .......... .......... .......... 49% 7.14M 24s
249250K .......... .......... .......... .......... .......... 49% 9.94M 24s
249300K .......... .......... .......... .......... .......... 49% 7.81M 24s
249350K .......... .......... .......... .......... .......... 49% 13.8M 24s
249400K .......... .......... .......... .......... .......... 49% 26.3M 24s
249450K .......... .......... .......... .......... .......... 49% 20.6M 24s
249500K .......... .......... .......... .......... .......... 49% 16.1M 24s
249550K .......... .......... .......... .......... .......... 49% 23.4M 24s
249600K .......... .......... .......... .......... .......... 49% 14.5M 24s
249650K .......... .......... .......... .......... .......... 49% 26.1M 24s
249700K .......... .......... .......... .......... .......... 49% 15.0M 24s
249750K .......... .......... .......... .......... .......... 49% 12.9M 24s
249800K .......... .......... .......... .......... .......... 49% 17.4M 24s
249850K .......... .......... .......... .......... .......... 49% 12.0M 24s
249900K .......... .......... .......... .......... .......... 49% 17.2M 24s
249950K .......... .......... .......... .......... .......... 49% 12.3M 24s
250000K .......... .......... .......... .......... .......... 49% 12.2M 24s
250050K .......... .......... .......... .......... .......... 49% 13.9M 24s
250100K .......... .......... .......... .......... .......... 49% 10.2M 24s
250150K .......... .......... .......... .......... .......... 49% 14.8M 24s
250200K .......... .......... .......... .......... .......... 49% 6.77M 24s
250250K .......... .......... .......... .......... .......... 49% 15.7M 24s
250300K .......... .......... .......... .......... .......... 49% 10.9M 24s
250350K .......... .......... .......... .......... .......... 49% 8.74M 24s
250400K .......... .......... .......... .......... .......... 49% 12.2M 24s
250450K .......... .......... .......... .......... .......... 49% 8.47M 24s
250500K .......... .......... .......... .......... .......... 49% 12.0M 24s
250550K .......... .......... .......... .......... .......... 49% 11.4M 24s
250600K .......... .......... .......... .......... .......... 49% 8.87M 24s
250650K .......... .......... .......... .......... .......... 49% 13.5M 24s
250700K .......... .......... .......... .......... .......... 49% 19.1M 24s
250750K .......... .......... .......... .......... .......... 49% 22.7M 24s
250800K .......... .......... .......... .......... .......... 49% 23.4M 24s
250850K .......... .......... .......... .......... .......... 49% 10.9M 24s
250900K .......... .......... .......... .......... .......... 49% 22.6M 24s
250950K .......... .......... .......... .......... .......... 49% 14.7M 24s
251000K .......... .......... .......... .......... .......... 49% 15.5M 24s
251050K .......... .......... .......... .......... .......... 49% 18.2M 24s
251100K .......... .......... .......... .......... .......... 49% 15.3M 24s
251150K .......... .......... .......... .......... .......... 49% 18.7M 24s
251200K .......... .......... .......... .......... .......... 49% 13.5M 24s
251250K .......... .......... .......... .......... .......... 49% 16.4M 24s
251300K .......... .......... .......... .......... .......... 49% 20.1M 24s
251350K .......... .......... .......... .......... .......... 49% 14.7M 24s
251400K .......... .......... .......... .......... .......... 49% 14.6M 24s
251450K .......... .......... .......... .......... .......... 49% 15.6M 24s
251500K .......... .......... .......... .......... .......... 49% 17.4M 24s
251550K .......... .......... .......... .......... .......... 49% 12.6M 24s
251600K .......... .......... .......... .......... .......... 49% 98.6M 24s
251650K .......... .......... .......... .......... .......... 49% 38.8M 24s
251700K .......... .......... .......... .......... .......... 49% 19.7M 24s
251750K .......... .......... .......... .......... .......... 49% 21.1M 24s
251800K .......... .......... .......... .......... .......... 49% 22.0M 24s
251850K .......... .......... .......... .......... .......... 49% 15.8M 24s
251900K .......... .......... .......... .......... .......... 49% 22.1M 24s
251950K .......... .......... .......... .......... .......... 49% 16.2M 24s
252000K .......... .......... .......... .......... .......... 49% 18.3M 24s
252050K .......... .......... .......... .......... .......... 49% 21.5M 24s
252100K .......... .......... .......... .......... .......... 49% 14.8M 24s
252150K .......... .......... .......... .......... .......... 49% 23.3M 24s
252200K .......... .......... .......... .......... .......... 49% 21.5M 24s
252250K .......... .......... .......... .......... .......... 49% 13.9M 24s
252300K .......... .......... .......... .......... .......... 49% 21.6M 24s
252350K .......... .......... .......... .......... .......... 49% 15.0M 24s
252400K .......... .......... .......... .......... .......... 49% 17.9M 24s
252450K .......... .......... .......... .......... .......... 49% 15.4M 24s
252500K .......... .......... .......... .......... .......... 49% 10.6M 24s
252550K .......... .......... .......... .......... .......... 49% 13.4M 24s
252600K .......... .......... .......... .......... .......... 49% 15.3M 24s
252650K .......... .......... .......... .......... .......... 49% 16.0M 24s
252700K .......... .......... .......... .......... .......... 49% 13.6M 24s
252750K .......... .......... .......... .......... .......... 49% 16.6M 24s
252800K .......... .......... .......... .......... .......... 49% 20.4M 24s
252850K .......... .......... .......... .......... .......... 49% 21.1M 24s
252900K .......... .......... .......... .......... .......... 49% 30.4M 24s
252950K .......... .......... .......... .......... .......... 49% 34.9M 24s
253000K .......... .......... .......... .......... .......... 49% 39.3M 24s
253050K .......... .......... .......... .......... .......... 49% 57.6M 24s
253100K .......... .......... .......... .......... .......... 49% 26.8M 24s
253150K .......... .......... .......... .......... .......... 49% 54.9M 24s
253200K .......... .......... .......... .......... .......... 49% 36.4M 24s
253250K .......... .......... .......... .......... .......... 49% 28.7M 24s
253300K .......... .......... .......... .......... .......... 49%  127M 24s
253350K .......... .......... .......... .......... .......... 49% 34.5M 24s
253400K .......... .......... .......... .......... .......... 49% 29.9M 24s
253450K .......... .......... .......... .......... .......... 49% 28.4M 24s
253500K .......... .......... .......... .......... .......... 49% 35.6M 24s
253550K .......... .......... .......... .......... .......... 49% 25.7M 24s
253600K .......... .......... .......... .......... .......... 49% 35.6M 24s
253650K .......... .......... .......... .......... .......... 49% 24.0M 24s
253700K .......... .......... .......... .......... .......... 49% 27.4M 24s
253750K .......... .......... .......... .......... .......... 49% 16.8M 24s
253800K .......... .......... .......... .......... .......... 49% 22.0M 24s
253850K .......... .......... .......... .......... .......... 49% 18.0M 24s
253900K .......... .......... .......... .......... .......... 49% 25.2M 24s
253950K .......... .......... .......... .......... .......... 49% 17.4M 24s
254000K .......... .......... .......... .......... .......... 49% 25.9M 24s
254050K .......... .......... .......... .......... .......... 49% 23.7M 24s
254100K .......... .......... .......... .......... .......... 49% 17.0M 24s
254150K .......... .......... .......... .......... .......... 49% 24.9M 24s
254200K .......... .......... .......... .......... .......... 50% 18.5M 24s
254250K .......... .......... .......... .......... .......... 50% 23.8M 24s
254300K .......... .......... .......... .......... .......... 50% 20.2M 24s
254350K .......... .......... .......... .......... .......... 50% 11.3M 24s
254400K .......... .......... .......... .......... .......... 50% 11.6M 24s
254450K .......... .......... .......... .......... .......... 50% 12.0M 24s
254500K .......... .......... .......... .......... .......... 50% 12.4M 24s
254550K .......... .......... .......... .......... .......... 50% 10.5M 24s
254600K .......... .......... .......... .......... .......... 50% 8.84M 24s
254650K .......... .......... .......... .......... .......... 50% 10.5M 24s
254700K .......... .......... .......... .......... .......... 50% 7.68M 24s
254750K .......... .......... .......... .......... .......... 50% 10.9M 23s
254800K .......... .......... .......... .......... .......... 50% 10.4M 23s
254850K .......... .......... .......... .......... .......... 50% 10.4M 23s
254900K .......... .......... .......... .......... .......... 50% 10.9M 23s
254950K .......... .......... .......... .......... .......... 50% 5.67M 23s
255000K .......... .......... .......... .......... .......... 50% 6.31M 23s
255050K .......... .......... .......... .......... .......... 50% 13.6M 23s
255100K .......... .......... .......... .......... .......... 50% 11.2M 23s
255150K .......... .......... .......... .......... .......... 50% 18.3M 23s
255200K .......... .......... .......... .......... .......... 50% 16.1M 23s
255250K .......... .......... .......... .......... .......... 50% 14.8M 23s
255300K .......... .......... .......... .......... .......... 50% 17.7M 23s
255350K .......... .......... .......... .......... .......... 50% 13.3M 23s
255400K .......... .......... .......... .......... .......... 50% 16.3M 23s
255450K .......... .......... .......... .......... .......... 50% 17.1M 23s
255500K .......... .......... .......... .......... .......... 50% 18.1M 23s
255550K .......... .......... .......... .......... .......... 50% 16.0M 23s
255600K .......... .......... .......... .......... .......... 50% 19.6M 23s
255650K .......... .......... .......... .......... .......... 50% 25.0M 23s
255700K .......... .......... .......... .......... .......... 50% 15.2M 23s
255750K .......... .......... .......... .......... .......... 50% 29.3M 23s
255800K .......... .......... .......... .......... .......... 50% 81.8M 23s
255850K .......... .......... .......... .......... .......... 50% 17.5M 23s
255900K .......... .......... .......... .......... .......... 50% 62.4M 23s
255950K .......... .......... .......... .......... .......... 50% 22.2M 23s
256000K .......... .......... .......... .......... .......... 50% 37.4M 23s
256050K .......... .......... .......... .......... .......... 50% 21.7M 23s
256100K .......... .......... .......... .......... .......... 50% 28.7M 23s
256150K .......... .......... .......... .......... .......... 50% 31.9M 23s
256200K .......... .......... .......... .......... .......... 50% 23.1M 23s
256250K .......... .......... .......... .......... .......... 50% 25.5M 23s
256300K .......... .......... .......... .......... .......... 50% 30.6M 23s
256350K .......... .......... .......... .......... .......... 50% 27.3M 23s
256400K .......... .......... .......... .......... .......... 50% 25.3M 23s
256450K .......... .......... .......... .......... .......... 50% 23.4M 23s
256500K .......... .......... .......... .......... .......... 50% 23.5M 23s
256550K .......... .......... .......... .......... .......... 50% 39.4M 23s
256600K .......... .......... .......... .......... .......... 50% 20.1M 23s
256650K .......... .......... .......... .......... .......... 50% 24.8M 23s
256700K .......... .......... .......... .......... .......... 50% 23.5M 23s
256750K .......... .......... .......... .......... .......... 50% 28.9M 23s
256800K .......... .......... .......... .......... .......... 50% 23.0M 23s
256850K .......... .......... .......... .......... .......... 50% 14.0M 23s
256900K .......... .......... .......... .......... .......... 50% 20.8M 23s
256950K .......... .......... .......... .......... .......... 50% 15.2M 23s
257000K .......... .......... .......... .......... .......... 50% 14.0M 23s
257050K .......... .......... .......... .......... .......... 50% 18.4M 23s
257100K .......... .......... .......... .......... .......... 50% 16.1M 23s
257150K .......... .......... .......... .......... .......... 50% 17.1M 23s
257200K .......... .......... .......... .......... .......... 50% 24.7M 23s
257250K .......... .......... .......... .......... .......... 50% 15.3M 23s
257300K .......... .......... .......... .......... .......... 50% 23.0M 23s
257350K .......... .......... .......... .......... .......... 50% 16.3M 23s
257400K .......... .......... .......... .......... .......... 50% 21.3M 23s
257450K .......... .......... .......... .......... .......... 50% 17.7M 23s
257500K .......... .......... .......... .......... .......... 50% 24.7M 23s
257550K .......... .......... .......... .......... .......... 50% 41.2M 23s
257600K .......... .......... .......... .......... .......... 50% 43.1M 23s
257650K .......... .......... .......... .......... .......... 50% 25.8M 23s
257700K .......... .......... .......... .......... .......... 50% 28.1M 23s
257750K .......... .......... .......... .......... .......... 50%  221M 23s
257800K .......... .......... .......... .......... .......... 50%  212M 23s
257850K .......... .......... .......... .......... .......... 50% 76.3M 23s
257900K .......... .......... .......... .......... .......... 50% 39.9M 23s
257950K .......... .......... .......... .......... .......... 50% 40.7M 23s
258000K .......... .......... .......... .......... .......... 50% 55.9M 23s
258050K .......... .......... .......... .......... .......... 50% 38.2M 23s
258100K .......... .......... .......... .......... .......... 50% 47.5M 23s
258150K .......... .......... .......... .......... .......... 50% 46.4M 23s
258200K .......... .......... .......... .......... .......... 50% 33.7M 23s
258250K .......... .......... .......... .......... .......... 50% 46.6M 23s
258300K .......... .......... .......... .......... .......... 50% 37.6M 23s
258350K .......... .......... .......... .......... .......... 50% 30.1M 23s
258400K .......... .......... .......... .......... .......... 50% 19.2M 23s
258450K .......... .......... .......... .......... .......... 50% 49.4M 23s
258500K .......... .......... .......... .......... .......... 50% 41.2M 23s
258550K .......... .......... .......... .......... .......... 50% 19.0M 23s
258600K .......... .......... .......... .......... .......... 50% 16.4M 23s
258650K .......... .......... .......... .......... .......... 50% 15.6M 23s
258700K .......... .......... .......... .......... .......... 50% 18.5M 23s
258750K .......... .......... .......... .......... .......... 50% 16.5M 23s
258800K .......... .......... .......... .......... .......... 50% 18.7M 23s
258850K .......... .......... .......... .......... .......... 50% 14.7M 23s
258900K .......... .......... .......... .......... .......... 50% 20.9M 23s
258950K .......... .......... .......... .......... .......... 50% 10.8M 23s
259000K .......... .......... .......... .......... .......... 50% 14.0M 23s
259050K .......... .......... .......... .......... .......... 50% 13.1M 23s
259100K .......... .......... .......... .......... .......... 50% 12.4M 23s
259150K .......... .......... .......... .......... .......... 50% 7.35M 23s
259200K .......... .......... .......... .......... .......... 50% 10.4M 23s
259250K .......... .......... .......... .......... .......... 51% 12.3M 23s
259300K .......... .......... .......... .......... .......... 51% 15.7M 23s
259350K .......... .......... .......... .......... .......... 51% 12.3M 23s
259400K .......... .......... .......... .......... .......... 51% 13.4M 23s
259450K .......... .......... .......... .......... .......... 51% 12.6M 23s
259500K .......... .......... .......... .......... .......... 51% 13.9M 23s
259550K .......... .......... .......... .......... .......... 51% 13.0M 23s
259600K .......... .......... .......... .......... .......... 51% 13.3M 23s
259650K .......... .......... .......... .......... .......... 51% 15.0M 23s
259700K .......... .......... .......... .......... .......... 51% 9.16M 23s
259750K .......... .......... .......... .......... .......... 51% 12.1M 23s
259800K .......... .......... .......... .......... .......... 51% 13.2M 23s
259850K .......... .......... .......... .......... .......... 51% 11.9M 23s
259900K .......... .......... .......... .......... .......... 51% 17.6M 23s
259950K .......... .......... .......... .......... .......... 51% 14.8M 23s
260000K .......... .......... .......... .......... .......... 51% 12.4M 23s
260050K .......... .......... .......... .......... .......... 51% 15.4M 23s
260100K .......... .......... .......... .......... .......... 51% 11.6M 23s
260150K .......... .......... .......... .......... .......... 51% 16.5M 23s
260200K .......... .......... .......... .......... .......... 51% 11.8M 23s
260250K .......... .......... .......... .......... .......... 51% 13.1M 23s
260300K .......... .......... .......... .......... .......... 51% 26.4M 23s
260350K .......... .......... .......... .......... .......... 51% 25.8M 23s
260400K .......... .......... .......... .......... .......... 51% 15.7M 23s
260450K .......... .......... .......... .......... .......... 51% 22.2M 23s
260500K .......... .......... .......... .......... .......... 51% 45.4M 23s
260550K .......... .......... .......... .......... .......... 51% 17.7M 23s
260600K .......... .......... .......... .......... .......... 51% 16.4M 23s
260650K .......... .......... .......... .......... .......... 51% 19.8M 23s
260700K .......... .......... .......... .......... .......... 51% 18.1M 23s
260750K .......... .......... .......... .......... .......... 51% 19.5M 23s
260800K .......... .......... .......... .......... .......... 51% 18.0M 23s
260850K .......... .......... .......... .......... .......... 51% 17.3M 23s
260900K .......... .......... .......... .......... .......... 51% 21.1M 23s
260950K .......... .......... .......... .......... .......... 51% 17.5M 23s
261000K .......... .......... .......... .......... .......... 51% 19.0M 23s
261050K .......... .......... .......... .......... .......... 51% 15.7M 23s
261100K .......... .......... .......... .......... .......... 51% 18.1M 23s
261150K .......... .......... .......... .......... .......... 51% 16.9M 23s
261200K .......... .......... .......... .......... .......... 51% 12.0M 23s
261250K .......... .......... .......... .......... .......... 51% 14.3M 23s
261300K .......... .......... .......... .......... .......... 51% 16.6M 23s
261350K .......... .......... .......... .......... .......... 51% 11.8M 23s
261400K .......... .......... .......... .......... .......... 51% 16.6M 23s
261450K .......... .......... .......... .......... .......... 51% 15.7M 23s
261500K .......... .......... .......... .......... .......... 51% 15.6M 23s
261550K .......... .......... .......... .......... .......... 51% 18.7M 23s
261600K .......... .......... .......... .......... .......... 51% 13.3M 23s
261650K .......... .......... .......... .......... .......... 51% 15.9M 23s
261700K .......... .......... .......... .......... .......... 51% 16.8M 23s
261750K .......... .......... .......... .......... .......... 51% 15.0M 23s
261800K .......... .......... .......... .......... .......... 51% 13.5M 23s
261850K .......... .......... .......... .......... .......... 51% 16.3M 23s
261900K .......... .......... .......... .......... .......... 51% 11.9M 23s
261950K .......... .......... .......... .......... .......... 51% 28.1M 23s
262000K .......... .......... .......... .......... .......... 51% 16.7M 23s
262050K .......... .......... .......... .......... .......... 51% 17.4M 23s
262100K .......... .......... .......... .......... .......... 51% 9.58M 23s
262150K .......... .......... .......... .......... .......... 51%  147M 23s
262200K .......... .......... .......... .......... .......... 51% 16.0M 23s
262250K .......... .......... .......... .......... .......... 51% 23.4M 23s
262300K .......... .......... .......... .......... .......... 51% 21.0M 23s
262350K .......... .......... .......... .......... .......... 51% 12.6M 23s
262400K .......... .......... .......... .......... .......... 51% 20.0M 23s
262450K .......... .......... .......... .......... .......... 51% 20.5M 23s
262500K .......... .......... .......... .......... .......... 51% 15.9M 23s
262550K .......... .......... .......... .......... .......... 51% 25.0M 23s
262600K .......... .......... .......... .......... .......... 51% 13.8M 22s
262650K .......... .......... .......... .......... .......... 51% 56.8M 22s
262700K .......... .......... .......... .......... .......... 51% 22.7M 22s
262750K .......... .......... .......... .......... .......... 51% 16.4M 22s
262800K .......... .......... .......... .......... .......... 51% 26.9M 22s
262850K .......... .......... .......... .......... .......... 51% 16.4M 22s
262900K .......... .......... .......... .......... .......... 51% 16.2M 22s
262950K .......... .......... .......... .......... .......... 51% 12.3M 22s
263000K .......... .......... .......... .......... .......... 51% 22.4M 22s
263050K .......... .......... .......... .......... .......... 51% 15.5M 22s
263100K .......... .......... .......... .......... .......... 51% 13.3M 22s
263150K .......... .......... .......... .......... .......... 51% 20.1M 22s
263200K .......... .......... .......... .......... .......... 51% 15.9M 22s
263250K .......... .......... .......... .......... .......... 51% 17.0M 22s
263300K .......... .......... .......... .......... .......... 51% 14.8M 22s
263350K .......... .......... .......... .......... .......... 51% 14.7M 22s
263400K .......... .......... .......... .......... .......... 51% 20.5M 22s
263450K .......... .......... .......... .......... .......... 51% 14.6M 22s
263500K .......... .......... .......... .......... .......... 51% 16.7M 22s
263550K .......... .......... .......... .......... .......... 51% 33.6M 22s
263600K .......... .......... .......... .......... .......... 51% 23.0M 22s
263650K .......... .......... .......... .......... .......... 51%  121M 22s
263700K .......... .......... .......... .......... .......... 51% 22.4M 22s
263750K .......... .......... .......... .......... .......... 51% 71.1M 22s
263800K .......... .......... .......... .......... .......... 51% 32.3M 22s
263850K .......... .......... .......... .......... .......... 51% 59.1M 22s
263900K .......... .......... .......... .......... .......... 51% 30.8M 22s
263950K .......... .......... .......... .......... .......... 51% 31.7M 22s
264000K .......... .......... .......... .......... .......... 51% 31.5M 22s
264050K .......... .......... .......... .......... .......... 51% 25.4M 22s
264100K .......... .......... .......... .......... .......... 51% 38.1M 22s
264150K .......... .......... .......... .......... .......... 51% 12.8M 22s
264200K .......... .......... .......... .......... .......... 51%  189M 22s
264250K .......... .......... .......... .......... .......... 51% 91.3M 22s
264300K .......... .......... .......... .......... .......... 51% 28.4M 22s
264350K .......... .......... .......... .......... .......... 52% 27.9M 22s
264400K .......... .......... .......... .......... .......... 52% 36.8M 22s
264450K .......... .......... .......... .......... .......... 52% 26.9M 22s
264500K .......... .......... .......... .......... .......... 52% 39.1M 22s
264550K .......... .......... .......... .......... .......... 52% 32.3M 22s
264600K .......... .......... .......... .......... .......... 52% 32.0M 22s
264650K .......... .......... .......... .......... .......... 52% 26.3M 22s
264700K .......... .......... .......... .......... .......... 52% 32.0M 22s
264750K .......... .......... .......... .......... .......... 52% 33.2M 22s
264800K .......... .......... .......... .......... .......... 52% 31.0M 22s
264850K .......... .......... .......... .......... .......... 52% 29.9M 22s
264900K .......... .......... .......... .......... .......... 52% 27.3M 22s
264950K .......... .......... .......... .......... .......... 52% 32.1M 22s
265000K .......... .......... .......... .......... .......... 52% 30.7M 22s
265050K .......... .......... .......... .......... .......... 52% 15.5M 22s
265100K .......... .......... .......... .......... .......... 52% 21.7M 22s
265150K .......... .......... .......... .......... .......... 52% 18.3M 22s
265200K .......... .......... .......... .......... .......... 52% 25.1M 22s
265250K .......... .......... .......... .......... .......... 52% 34.5M 22s
265300K .......... .......... .......... .......... .......... 52% 80.8M 22s
265350K .......... .......... .......... .......... .......... 52% 33.9M 22s
265400K .......... .......... .......... .......... .......... 52% 29.1M 22s
265450K .......... .......... .......... .......... .......... 52% 27.9M 22s
265500K .......... .......... .......... .......... .......... 52% 34.1M 22s
265550K .......... .......... .......... .......... .......... 52% 37.5M 22s
265600K .......... .......... .......... .......... .......... 52% 24.0M 22s
265650K .......... .......... .......... .......... .......... 52% 27.6M 22s
265700K .......... .......... .......... .......... .......... 52% 33.0M 22s
265750K .......... .......... .......... .......... .......... 52% 30.9M 22s
265800K .......... .......... .......... .......... .......... 52% 28.5M 22s
265850K .......... .......... .......... .......... .......... 52% 31.5M 22s
265900K .......... .......... .......... .......... .......... 52% 27.1M 22s
265950K .......... .......... .......... .......... .......... 52% 24.0M 22s
266000K .......... .......... .......... .......... .......... 52% 38.7M 22s
266050K .......... .......... .......... .......... .......... 52% 23.6M 22s
266100K .......... .......... .......... .......... .......... 52% 43.3M 22s
266150K .......... .......... .......... .......... .......... 52% 25.8M 22s
266200K .......... .......... .......... .......... .......... 52% 25.8M 22s
266250K .......... .......... .......... .......... .......... 52% 38.5M 22s
266300K .......... .......... .......... .......... .......... 52% 38.4M 22s
266350K .......... .......... .......... .......... .......... 52% 23.1M 22s
266400K .......... .......... .......... .......... .......... 52% 41.1M 22s
266450K .......... .......... .......... .......... .......... 52% 38.1M 22s
266500K .......... .......... .......... .......... .......... 52% 22.8M 22s
266550K .......... .......... .......... .......... .......... 52%  158M 22s
266600K .......... .......... .......... .......... .......... 52%  171M 22s
266650K .......... .......... .......... .......... .......... 52% 39.9M 22s
266700K .......... .......... .......... .......... .......... 52% 45.0M 22s
266750K .......... .......... .......... .......... .......... 52%  136M 22s
266800K .......... .......... .......... .......... .......... 52% 39.7M 22s
266850K .......... .......... .......... .......... .......... 52% 29.5M 22s
266900K .......... .......... .......... .......... .......... 52% 28.7M 22s
266950K .......... .......... .......... .......... .......... 52% 30.8M 22s
267000K .......... .......... .......... .......... .......... 52% 40.6M 22s
267050K .......... .......... .......... .......... .......... 52% 41.6M 22s
267100K .......... .......... .......... .......... .......... 52% 31.2M 22s
267150K .......... .......... .......... .......... .......... 52% 31.7M 22s
267200K .......... .......... .......... .......... .......... 52% 36.5M 22s
267250K .......... .......... .......... .......... .......... 52% 40.0M 22s
267300K .......... .......... .......... .......... .......... 52% 32.9M 22s
267350K .......... .......... .......... .......... .......... 52% 35.2M 22s
267400K .......... .......... .......... .......... .......... 52% 43.8M 22s
267450K .......... .......... .......... .......... .......... 52% 36.4M 22s
267500K .......... .......... .......... .......... .......... 52% 32.6M 22s
267550K .......... .......... .......... .......... .......... 52% 45.9M 22s
267600K .......... .......... .......... .......... .......... 52% 32.9M 22s
267650K .......... .......... .......... .......... .......... 52% 40.9M 22s
267700K .......... .......... .......... .......... .......... 52% 24.4M 22s
267750K .......... .......... .......... .......... .......... 52% 48.6M 22s
267800K .......... .......... .......... .......... .......... 52% 43.1M 22s
267850K .......... .......... .......... .......... .......... 52% 26.2M 22s
267900K .......... .......... .......... .......... .......... 52% 47.0M 22s
267950K .......... .......... .......... .......... .......... 52% 28.8M 22s
268000K .......... .......... .......... .......... .......... 52% 32.0M 22s
268050K .......... .......... .......... .......... .......... 52% 51.5M 22s
268100K .......... .......... .......... .......... .......... 52% 27.7M 22s
268150K .......... .......... .......... .......... .......... 52% 74.3M 22s
268200K .......... .......... .......... .......... .......... 52% 19.9M 22s
268250K .......... .......... .......... .......... .......... 52%  111M 22s
268300K .......... .......... .......... .......... .......... 52%  143M 22s
268350K .......... .......... .......... .......... .......... 52% 20.2M 22s
268400K .......... .......... .......... .......... .......... 52% 88.8M 22s
268450K .......... .......... .......... .......... .......... 52% 52.2M 22s
268500K .......... .......... .......... .......... .......... 52%  144M 22s
268550K .......... .......... .......... .......... .......... 52% 26.2M 22s
268600K .......... .......... .......... .......... .......... 52% 22.0M 22s
268650K .......... .......... .......... .......... .......... 52% 30.3M 22s
268700K .......... .......... .......... .......... .......... 52% 15.8M 22s
268750K .......... .......... .......... .......... .......... 52% 17.1M 22s
268800K .......... .......... .......... .......... .......... 52% 23.5M 22s
268850K .......... .......... .......... .......... .......... 52% 17.8M 22s
268900K .......... .......... .......... .......... .......... 52% 26.4M 22s
268950K .......... .......... .......... .......... .......... 52% 15.5M 22s
269000K .......... .......... .......... .......... .......... 52% 18.7M 22s
269050K .......... .......... .......... .......... .......... 52% 17.2M 22s
269100K .......... .......... .......... .......... .......... 52% 19.5M 22s
269150K .......... .......... .......... .......... .......... 52% 21.2M 22s
269200K .......... .......... .......... .......... .......... 52% 14.6M 22s
269250K .......... .......... .......... .......... .......... 52% 26.3M 22s
269300K .......... .......... .......... .......... .......... 52% 22.8M 22s
269350K .......... .......... .......... .......... .......... 52% 19.1M 22s
269400K .......... .......... .......... .......... .......... 52% 21.1M 22s
269450K .......... .......... .......... .......... .......... 53% 17.2M 22s
269500K .......... .......... .......... .......... .......... 53%  120M 22s
269550K .......... .......... .......... .......... .......... 53% 21.1M 22s
269600K .......... .......... .......... .......... .......... 53% 28.3M 22s
269650K .......... .......... .......... .......... .......... 53% 27.1M 22s
269700K .......... .......... .......... .......... .......... 53% 24.2M 21s
269750K .......... .......... .......... .......... .......... 53% 27.5M 21s
269800K .......... .......... .......... .......... .......... 53% 19.3M 21s
269850K .......... .......... .......... .......... .......... 53% 24.4M 21s
269900K .......... .......... .......... .......... .......... 53% 24.4M 21s
269950K .......... .......... .......... .......... .......... 53% 21.5M 21s
270000K .......... .......... .......... .......... .......... 53% 27.5M 21s
270050K .......... .......... .......... .......... .......... 53% 26.1M 21s
270100K .......... .......... .......... .......... .......... 53% 18.7M 21s
270150K .......... .......... .......... .......... .......... 53% 23.0M 21s
270200K .......... .......... .......... .......... .......... 53% 18.0M 21s
270250K .......... .......... .......... .......... .......... 53% 33.5M 21s
270300K .......... .......... .......... .......... .......... 53% 17.4M 21s
270350K .......... .......... .......... .......... .......... 53% 21.5M 21s
270400K .......... .......... .......... .......... .......... 53% 30.6M 21s
270450K .......... .......... .......... .......... .......... 53% 12.5M 21s
270500K .......... .......... .......... .......... .......... 53%  132M 21s
270550K .......... .......... .......... .......... .......... 53% 38.5M 21s
270600K .......... .......... .......... .......... .......... 53% 26.3M 21s
270650K .......... .......... .......... .......... .......... 53% 26.4M 21s
270700K .......... .......... .......... .......... .......... 53% 36.9M 21s
270750K .......... .......... .......... .......... .......... 53% 25.4M 21s
270800K .......... .......... .......... .......... .......... 53% 26.8M 21s
270850K .......... .......... .......... .......... .......... 53% 17.5M 21s
270900K .......... .......... .......... .......... .......... 53% 20.8M 21s
270950K .......... .......... .......... .......... .......... 53% 18.0M 21s
271000K .......... .......... .......... .......... .......... 53% 19.3M 21s
271050K .......... .......... .......... .......... .......... 53% 22.3M 21s
271100K .......... .......... .......... .......... .......... 53% 18.4M 21s
271150K .......... .......... .......... .......... .......... 53% 23.4M 21s
271200K .......... .......... .......... .......... .......... 53% 19.0M 21s
271250K .......... .......... .......... .......... .......... 53% 24.3M 21s
271300K .......... .......... .......... .......... .......... 53% 25.0M 21s
271350K .......... .......... .......... .......... .......... 53% 19.5M 21s
271400K .......... .......... .......... .......... .......... 53% 16.8M 21s
271450K .......... .......... .......... .......... .......... 53% 22.9M 21s
271500K .......... .......... .......... .......... .......... 53% 21.2M 21s
271550K .......... .......... .......... .......... .......... 53% 21.0M 21s
271600K .......... .......... .......... .......... .......... 53% 27.2M 21s
271650K .......... .......... .......... .......... .......... 53% 99.0M 21s
271700K .......... .......... .......... .......... .......... 53% 17.6M 21s
271750K .......... .......... .......... .......... .......... 53% 70.5M 21s
271800K .......... .......... .......... .......... .......... 53%  187M 21s
271850K .......... .......... .......... .......... .......... 53% 29.3M 21s
271900K .......... .......... .......... .......... .......... 53% 34.9M 21s
271950K .......... .......... .......... .......... .......... 53% 32.9M 21s
272000K .......... .......... .......... .......... .......... 53% 37.0M 21s
272050K .......... .......... .......... .......... .......... 53% 23.5M 21s
272100K .......... .......... .......... .......... .......... 53% 25.4M 21s
272150K .......... .......... .......... .......... .......... 53% 33.2M 21s
272200K .......... .......... .......... .......... .......... 53% 27.4M 21s
272250K .......... .......... .......... .......... .......... 53% 27.2M 21s
272300K .......... .......... .......... .......... .......... 53% 26.7M 21s
272350K .......... .......... .......... .......... .......... 53% 28.1M 21s
272400K .......... .......... .......... .......... .......... 53% 25.6M 21s
272450K .......... .......... .......... .......... .......... 53% 42.5M 21s
272500K .......... .......... .......... .......... .......... 53% 30.0M 21s
272550K .......... .......... .......... .......... .......... 53% 24.2M 21s
272600K .......... .......... .......... .......... .......... 53% 27.3M 21s
272650K .......... .......... .......... .......... .......... 53% 34.3M 21s
272700K .......... .......... .......... .......... .......... 53% 25.9M 21s
272750K .......... .......... .......... .......... .......... 53% 34.8M 21s
272800K .......... .......... .......... .......... .......... 53% 25.7M 21s
272850K .......... .......... .......... .......... .......... 53% 43.6M 21s
272900K .......... .......... .......... .......... .......... 53% 24.0M 21s
272950K .......... .......... .......... .......... .......... 53% 28.6M 21s
273000K .......... .......... .......... .......... .......... 53% 13.2M 21s
273050K .......... .......... .......... .......... .......... 53% 81.1M 21s
273100K .......... .......... .......... .......... .......... 53% 23.4M 21s
273150K .......... .......... .......... .......... .......... 53% 33.8M 21s
273200K .......... .......... .......... .......... .......... 53% 19.1M 21s
273250K .......... .......... .......... .......... .......... 53% 18.5M 21s
273300K .......... .......... .......... .......... .......... 53% 24.7M 21s
273350K .......... .......... .......... .......... .......... 53% 17.1M 21s
273400K .......... .......... .......... .......... .......... 53% 20.8M 21s
273450K .......... .......... .......... .......... .......... 53% 19.5M 21s
273500K .......... .......... .......... .......... .......... 53% 19.0M 21s
273550K .......... .......... .......... .......... .......... 53% 22.0M 21s
273600K .......... .......... .......... .......... .......... 53% 17.1M 21s
273650K .......... .......... .......... .......... .......... 53% 24.4M 21s
273700K .......... .......... .......... .......... .......... 53% 15.3M 21s
273750K .......... .......... .......... .......... .......... 53% 25.3M 21s
273800K .......... .......... .......... .......... .......... 53% 16.3M 21s
273850K .......... .......... .......... .......... .......... 53% 21.5M 21s
273900K .......... .......... .......... .......... .......... 53% 18.5M 21s
273950K .......... .......... .......... .......... .......... 53% 7.44M 21s
274000K .......... .......... .......... .......... .......... 53% 28.4M 21s
274050K .......... .......... .......... .......... .......... 53% 30.2M 21s
274100K .......... .......... .......... .......... .......... 53% 18.6M 21s
274150K .......... .......... .......... .......... .......... 53% 15.5M 21s
274200K .......... .......... .......... .......... .......... 53% 16.3M 21s
274250K .......... .......... .......... .......... .......... 53% 15.0M 21s
274300K .......... .......... .......... .......... .......... 53% 20.9M 21s
274350K .......... .......... .......... .......... .......... 53% 12.4M 21s
274400K .......... .......... .......... .......... .......... 53% 17.5M 21s
274450K .......... .......... .......... .......... .......... 53% 14.3M 21s
274500K .......... .......... .......... .......... .......... 53% 18.2M 21s
274550K .......... .......... .......... .......... .......... 54% 15.1M 21s
274600K .......... .......... .......... .......... .......... 54% 14.7M 21s
274650K .......... .......... .......... .......... .......... 54% 15.5M 21s
274700K .......... .......... .......... .......... .......... 54% 18.9M 21s
274750K .......... .......... .......... .......... .......... 54% 25.7M 21s
274800K .......... .......... .......... .......... .......... 54% 19.6M 21s
274850K .......... .......... .......... .......... .......... 54% 15.9M 21s
274900K .......... .......... .......... .......... .......... 54% 40.4M 21s
274950K .......... .......... .......... .......... .......... 54% 20.6M 21s
275000K .......... .......... .......... .......... .......... 54% 49.1M 21s
275050K .......... .......... .......... .......... .......... 54% 31.0M 21s
275100K .......... .......... .......... .......... .......... 54% 27.1M 21s
275150K .......... .......... .......... .......... .......... 54% 21.6M 21s
275200K .......... .......... .......... .......... .......... 54% 28.4M 21s
275250K .......... .......... .......... .......... .......... 54% 34.7M 21s
275300K .......... .......... .......... .......... .......... 54% 30.2M 21s
275350K .......... .......... .......... .......... .......... 54% 26.4M 21s
275400K .......... .......... .......... .......... .......... 54% 25.2M 21s
275450K .......... .......... .......... .......... .......... 54% 21.1M 21s
275500K .......... .......... .......... .......... .......... 54% 68.6M 21s
275550K .......... .......... .......... .......... .......... 54% 24.7M 21s
275600K .......... .......... .......... .......... .......... 54% 28.7M 21s
275650K .......... .......... .......... .......... .......... 54% 26.8M 21s
275700K .......... .......... .......... .......... .......... 54% 23.2M 21s
275750K .......... .......... .......... .......... .......... 54% 25.4M 21s
275800K .......... .......... .......... .......... .......... 54% 37.2M 21s
275850K .......... .......... .......... .......... .......... 54% 23.3M 21s
275900K .......... .......... .......... .......... .......... 54% 24.6M 21s
275950K .......... .......... .......... .......... .......... 54% 27.7M 21s
276000K .......... .......... .......... .......... .......... 54% 48.0M 21s
276050K .......... .......... .......... .......... .......... 54% 10.1M 21s
276100K .......... .......... .......... .......... .......... 54%  120M 21s
276150K .......... .......... .......... .......... .......... 54%  194M 21s
276200K .......... .......... .......... .......... .......... 54% 24.5M 21s
276250K .......... .......... .......... .......... .......... 54% 20.6M 21s
276300K .......... .......... .......... .......... .......... 54% 30.9M 21s
276350K .......... .......... .......... .......... .......... 54% 23.5M 21s
276400K .......... .......... .......... .......... .......... 54% 23.7M 21s
276450K .......... .......... .......... .......... .......... 54% 23.2M 21s
276500K .......... .......... .......... .......... .......... 54% 18.4M 21s
276550K .......... .......... .......... .......... .......... 54% 20.6M 21s
276600K .......... .......... .......... .......... .......... 54% 18.1M 21s
276650K .......... .......... .......... .......... .......... 54% 25.8M 21s
276700K .......... .......... .......... .......... .......... 54% 16.5M 21s
276750K .......... .......... .......... .......... .......... 54% 21.3M 21s
276800K .......... .......... .......... .......... .......... 54% 23.8M 21s
276850K .......... .......... .......... .......... .......... 54% 15.8M 21s
276900K .......... .......... .......... .......... .......... 54% 22.2M 21s
276950K .......... .......... .......... .......... .......... 54% 21.4M 21s
277000K .......... .......... .......... .......... .......... 54% 20.1M 21s
277050K .......... .......... .......... .......... .......... 54% 24.8M 21s
277100K .......... .......... .......... .......... .......... 54% 27.9M 21s
277150K .......... .......... .......... .......... .......... 54% 33.2M 21s
277200K .......... .......... .......... .......... .......... 54% 23.4M 21s
277250K .......... .......... .......... .......... .......... 54% 37.6M 21s
277300K .......... .......... .......... .......... .......... 54%  164M 21s
277350K .......... .......... .......... .......... .......... 54% 17.7M 20s
277400K .......... .......... .......... .......... .......... 54% 46.5M 20s
277450K .......... .......... .......... .......... .......... 54% 21.9M 20s
277500K .......... .......... .......... .......... .......... 54% 16.6M 20s
277550K .......... .......... .......... .......... .......... 54%  174M 20s
277600K .......... .......... .......... .......... .......... 54% 32.4M 20s
277650K .......... .......... .......... .......... .......... 54% 26.8M 20s
277700K .......... .......... .......... .......... .......... 54% 34.8M 20s
277750K .......... .......... .......... .......... .......... 54% 24.8M 20s
277800K .......... .......... .......... .......... .......... 54% 30.0M 20s
277850K .......... .......... .......... .......... .......... 54% 24.1M 20s
277900K .......... .......... .......... .......... .......... 54% 27.7M 20s
277950K .......... .......... .......... .......... .......... 54% 31.8M 20s
278000K .......... .......... .......... .......... .......... 54% 24.4M 20s
278050K .......... .......... .......... .......... .......... 54% 36.9M 20s
278100K .......... .......... .......... .......... .......... 54% 23.6M 20s
278150K .......... .......... .......... .......... .......... 54% 37.0M 20s
278200K .......... .......... .......... .......... .......... 54% 24.0M 20s
278250K .......... .......... .......... .......... .......... 54% 27.7M 20s
278300K .......... .......... .......... .......... .......... 54% 36.2M 20s
278350K .......... .......... .......... .......... .......... 54% 24.9M 20s
278400K .......... .......... .......... .......... .......... 54% 29.5M 20s
278450K .......... .......... .......... .......... .......... 54% 23.2M 20s
278500K .......... .......... .......... .......... .......... 54% 35.1M 20s
278550K .......... .......... .......... .......... .......... 54% 60.7M 20s
278600K .......... .......... .......... .......... .......... 54% 16.0M 20s
278650K .......... .......... .......... .......... .......... 54%  167M 20s
278700K .......... .......... .......... .......... .......... 54% 16.8M 20s
278750K .......... .......... .......... .......... .......... 54%  191M 20s
278800K .......... .......... .......... .......... .......... 54% 19.7M 20s
278850K .......... .......... .......... .......... .......... 54% 29.8M 20s
278900K .......... .......... .......... .......... .......... 54% 2.22M 20s
278950K .......... .......... .......... .......... .......... 54%  140M 20s
279000K .......... .......... .......... .......... .......... 54%  141M 20s
279050K .......... .......... .......... .......... .......... 54%  114M 20s
279100K .......... .......... .......... .......... .......... 54%  139M 20s
279150K .......... .......... .......... .......... .......... 54% 34.7M 20s
279200K .......... .......... .......... .......... .......... 54% 21.3M 20s
279250K .......... .......... .......... .......... .......... 54% 25.6M 20s
279300K .......... .......... .......... .......... .......... 54% 21.1M 20s
279350K .......... .......... .......... .......... .......... 54% 21.9M 20s
279400K .......... .......... .......... .......... .......... 54% 18.7M 20s
279450K .......... .......... .......... .......... .......... 54% 20.8M 20s
279500K .......... .......... .......... .......... .......... 54% 22.2M 20s
279550K .......... .......... .......... .......... .......... 54% 40.4M 20s
279600K .......... .......... .......... .......... .......... 55%  146M 20s
279650K .......... .......... .......... .......... .......... 55% 22.6M 20s
279700K .......... .......... .......... .......... .......... 55% 40.1M 20s
279750K .......... .......... .......... .......... .......... 55% 37.0M 20s
279800K .......... .......... .......... .......... .......... 55% 23.8M 20s
279850K .......... .......... .......... .......... .......... 55% 25.2M 20s
279900K .......... .......... .......... .......... .......... 55% 22.3M 20s
279950K .......... .......... .......... .......... .......... 55% 21.2M 20s
280000K .......... .......... .......... .......... .......... 55% 37.6M 20s
280050K .......... .......... .......... .......... .......... 55% 26.5M 20s
280100K .......... .......... .......... .......... .......... 55% 25.3M 20s
280150K .......... .......... .......... .......... .......... 55% 26.3M 20s
280200K .......... .......... .......... .......... .......... 55% 28.3M 20s
280250K .......... .......... .......... .......... .......... 55% 23.9M 20s
280300K .......... .......... .......... .......... .......... 55% 36.9M 20s
280350K .......... .......... .......... .......... .......... 55% 21.9M 20s
280400K .......... .......... .......... .......... .......... 55% 23.6M 20s
280450K .......... .......... .......... .......... .......... 55% 27.4M 20s
280500K .......... .......... .......... .......... .......... 55% 29.2M 20s
280550K .......... .......... .......... .......... .......... 55% 30.8M 20s
280600K .......... .......... .......... .......... .......... 55% 25.4M 20s
280650K .......... .......... .......... .......... .......... 55% 36.0M 20s
280700K .......... .......... .......... .......... .......... 55% 35.7M 20s
280750K .......... .......... .......... .......... .......... 55%  112M 20s
280800K .......... .......... .......... .......... .......... 55% 17.1M 20s
280850K .......... .......... .......... .......... .......... 55%  130M 20s
280900K .......... .......... .......... .......... .......... 55% 79.7M 20s
280950K .......... .......... .......... .......... .......... 55% 23.8M 20s
281000K .......... .......... .......... .......... .......... 55%  136M 20s
281050K .......... .......... .......... .......... .......... 55% 24.4M 20s
281100K .......... .......... .......... .......... .......... 55% 18.3M 20s
281150K .......... .......... .......... .......... .......... 55%  131M 20s
281200K .......... .......... .......... .......... .......... 55% 23.0M 20s
281250K .......... .......... .......... .......... .......... 55% 19.0M 20s
281300K .......... .......... .......... .......... .......... 55% 22.2M 20s
281350K .......... .......... .......... .......... .......... 55% 23.1M 20s
281400K .......... .......... .......... .......... .......... 55% 19.8M 20s
281450K .......... .......... .......... .......... .......... 55% 16.1M 20s
281500K .......... .......... .......... .......... .......... 55% 20.8M 20s
281550K .......... .......... .......... .......... .......... 55% 25.7M 20s
281600K .......... .......... .......... .......... .......... 55% 22.3M 20s
281650K .......... .......... .......... .......... .......... 55% 26.3M 20s
281700K .......... .......... .......... .......... .......... 55% 21.8M 20s
281750K .......... .......... .......... .......... .......... 55% 25.4M 20s
281800K .......... .......... .......... .......... .......... 55% 22.4M 20s
281850K .......... .......... .......... .......... .......... 55% 16.2M 20s
281900K .......... .......... .......... .......... .......... 55% 21.4M 20s
281950K .......... .......... .......... .......... .......... 55% 7.66M 20s
282000K .......... .......... .......... .......... .......... 55% 13.5M 20s
282050K .......... .......... .......... .......... .......... 55% 16.8M 20s
282100K .......... .......... .......... .......... .......... 55% 11.5M 20s
282150K .......... .......... .......... .......... .......... 55% 16.1M 20s
282200K .......... .......... .......... .......... .......... 55% 13.2M 20s
282250K .......... .......... .......... .......... .......... 55% 15.0M 20s
282300K .......... .......... .......... .......... .......... 55% 17.6M 20s
282350K .......... .......... .......... .......... .......... 55% 12.5M 20s
282400K .......... .......... .......... .......... .......... 55% 15.6M 20s
282450K .......... .......... .......... .......... .......... 55% 13.6M 20s
282500K .......... .......... .......... .......... .......... 55% 17.9M 20s
282550K .......... .......... .......... .......... .......... 55% 26.5M 20s
282600K .......... .......... .......... .......... .......... 55% 10.7M 20s
282650K .......... .......... .......... .......... .......... 55% 92.3M 20s
282700K .......... .......... .......... .......... .......... 55% 15.8M 20s
282750K .......... .......... .......... .......... .......... 55%  140M 20s
282800K .......... .......... .......... .......... .......... 55% 19.4M 20s
282850K .......... .......... .......... .......... .......... 55% 19.3M 20s
282900K .......... .......... .......... .......... .......... 55% 19.2M 20s
282950K .......... .......... .......... .......... .......... 55% 19.7M 20s
283000K .......... .......... .......... .......... .......... 55% 19.7M 20s
283050K .......... .......... .......... .......... .......... 55% 19.6M 20s
283100K .......... .......... .......... .......... .......... 55% 19.3M 20s
283150K .......... .......... .......... .......... .......... 55% 18.8M 20s
283200K .......... .......... .......... .......... .......... 55% 16.6M 20s
283250K .......... .......... .......... .......... .......... 55% 22.6M 20s
283300K .......... .......... .......... .......... .......... 55% 19.6M 20s
283350K .......... .......... .......... .......... .......... 55% 19.4M 20s
283400K .......... .......... .......... .......... .......... 55% 22.0M 20s
283450K .......... .......... .......... .......... .......... 55% 18.7M 20s
283500K .......... .......... .......... .......... .......... 55% 19.0M 20s
283550K .......... .......... .......... .......... .......... 55% 22.7M 20s
283600K .......... .......... .......... .......... .......... 55% 14.2M 20s
283650K .......... .......... .......... .......... .......... 55% 16.8M 20s
283700K .......... .......... .......... .......... .......... 55% 35.7M 20s
283750K .......... .......... .......... .......... .......... 55% 15.1M 20s
283800K .......... .......... .......... .......... .......... 55% 22.7M 20s
283850K .......... .......... .......... .......... .......... 55% 10.4M 20s
283900K .......... .......... .......... .......... .......... 55% 16.3M 20s
283950K .......... .......... .......... .......... .......... 55% 12.6M 20s
284000K .......... .......... .......... .......... .......... 55% 12.3M 20s
284050K .......... .......... .......... .......... .......... 55% 13.1M 20s
284100K .......... .......... .......... .......... .......... 55% 10.6M 20s
284150K .......... .......... .......... .......... .......... 55% 17.4M 20s
284200K .......... .......... .......... .......... .......... 55% 10.9M 20s
284250K .......... .......... .......... .......... .......... 55% 14.6M 20s
284300K .......... .......... .......... .......... .......... 55% 13.6M 20s
284350K .......... .......... .......... .......... .......... 55% 14.2M 20s
284400K .......... .......... .......... .......... .......... 55% 20.5M 20s
284450K .......... .......... .......... .......... .......... 55% 11.4M 20s
284500K .......... .......... .......... .......... .......... 55% 16.6M 20s
284550K .......... .......... .......... .......... .......... 55% 13.1M 20s
284600K .......... .......... .......... .......... .......... 55% 12.4M 20s
284650K .......... .......... .......... .......... .......... 55% 14.9M 20s
284700K .......... .......... .......... .......... .......... 56% 12.2M 20s
284750K .......... .......... .......... .......... .......... 56% 14.2M 20s
284800K .......... .......... .......... .......... .......... 56% 16.5M 20s
284850K .......... .......... .......... .......... .......... 56% 13.0M 20s
284900K .......... .......... .......... .......... .......... 56% 17.1M 20s
284950K .......... .......... .......... .......... .......... 56% 11.9M 20s
285000K .......... .......... .......... .......... .......... 56% 17.7M 20s
285050K .......... .......... .......... .......... .......... 56% 16.7M 20s
285100K .......... .......... .......... .......... .......... 56% 21.2M 20s
285150K .......... .......... .......... .......... .......... 56% 22.1M 20s
285200K .......... .......... .......... .......... .......... 56% 17.7M 20s
285250K .......... .......... .......... .......... .......... 56% 24.3M 20s
285300K .......... .......... .......... .......... .......... 56% 20.3M 20s
285350K .......... .......... .......... .......... .......... 56% 13.6M 20s
285400K .......... .......... .......... .......... .......... 56% 18.6M 20s
285450K .......... .......... .......... .......... .......... 56% 13.7M 20s
285500K .......... .......... .......... .......... .......... 56% 18.5M 20s
285550K .......... .......... .......... .......... .......... 56% 13.7M 20s
285600K .......... .......... .......... .......... .......... 56% 15.4M 20s
285650K .......... .......... .......... .......... .......... 56% 19.2M 20s
285700K .......... .......... .......... .......... .......... 56% 17.7M 20s
285750K .......... .......... .......... .......... .......... 56% 14.4M 19s
285800K .......... .......... .......... .......... .......... 56% 19.6M 19s
285850K .......... .......... .......... .......... .......... 56% 15.6M 19s
285900K .......... .......... .......... .......... .......... 56% 20.0M 19s
285950K .......... .......... .......... .......... .......... 56% 16.0M 19s
286000K .......... .......... .......... .......... .......... 56% 26.3M 19s
286050K .......... .......... .......... .......... .......... 56% 21.2M 19s
286100K .......... .......... .......... .......... .......... 56%  119M 19s
286150K .......... .......... .......... .......... .......... 56% 30.4M 19s
286200K .......... .......... .......... .......... .......... 56%  148M 19s
286250K .......... .......... .......... .......... .......... 56% 36.5M 19s
286300K .......... .......... .......... .......... .......... 56% 47.8M 19s
286350K .......... .......... .......... .......... .......... 56% 31.6M 19s
286400K .......... .......... .......... .......... .......... 56% 45.5M 19s
286450K .......... .......... .......... .......... .......... 56% 28.7M 19s
286500K .......... .......... .......... .......... .......... 56% 38.2M 19s
286550K .......... .......... .......... .......... .......... 56% 43.2M 19s
286600K .......... .......... .......... .......... .......... 56% 28.1M 19s
286650K .......... .......... .......... .......... .......... 56% 37.8M 19s
286700K .......... .......... .......... .......... .......... 56% 30.4M 19s
286750K .......... .......... .......... .......... .......... 56% 33.8M 19s
286800K .......... .......... .......... .......... .......... 56% 42.4M 19s
286850K .......... .......... .......... .......... .......... 56% 32.5M 19s
286900K .......... .......... .......... .......... .......... 56% 32.6M 19s
286950K .......... .......... .......... .......... .......... 56% 39.3M 19s
287000K .......... .......... .......... .......... .......... 56% 31.7M 19s
287050K .......... .......... .......... .......... .......... 56% 14.6M 19s
287100K .......... .......... .......... .......... .......... 56% 13.6M 19s
287150K .......... .......... .......... .......... .......... 56%  139M 19s
287200K .......... .......... .......... .......... .......... 56%  187M 19s
287250K .......... .......... .......... .......... .......... 56%  225M 19s
287300K .......... .......... .......... .......... .......... 56% 45.3M 19s
287350K .......... .......... .......... .......... .......... 56% 33.1M 19s
287400K .......... .......... .......... .......... .......... 56% 35.5M 19s
287450K .......... .......... .......... .......... .......... 56% 35.6M 19s
287500K .......... .......... .......... .......... .......... 56% 35.6M 19s
287550K .......... .......... .......... .......... .......... 56% 20.0M 19s
287600K .......... .......... .......... .......... .......... 56% 48.3M 19s
287650K .......... .......... .......... .......... .......... 56% 41.2M 19s
287700K .......... .......... .......... .......... .......... 56% 43.5M 19s
287750K .......... .......... .......... .......... .......... 56% 31.5M 19s
287800K .......... .......... .......... .......... .......... 56% 28.5M 19s
287850K .......... .......... .......... .......... .......... 56% 38.4M 19s
287900K .......... .......... .......... .......... .......... 56% 39.5M 19s
287950K .......... .......... .......... .......... .......... 56% 22.7M 19s
288000K .......... .......... .......... .......... .......... 56% 41.3M 19s
288050K .......... .......... .......... .......... .......... 56% 27.4M 19s
288100K .......... .......... .......... .......... .......... 56% 25.3M 19s
288150K .......... .......... .......... .......... .......... 56% 28.2M 19s
288200K .......... .......... .......... .......... .......... 56% 25.9M 19s
288250K .......... .......... .......... .......... .......... 56% 32.4M 19s
288300K .......... .......... .......... .......... .......... 56% 42.3M 19s
288350K .......... .......... .......... .......... .......... 56% 24.1M 19s
288400K .......... .......... .......... .......... .......... 56% 30.9M 19s
288450K .......... .......... .......... .......... .......... 56% 25.3M 19s
288500K .......... .......... .......... .......... .......... 56% 25.7M 19s
288550K .......... .......... .......... .......... .......... 56% 35.5M 19s
288600K .......... .......... .......... .......... .......... 56% 24.0M 19s
288650K .......... .......... .......... .......... .......... 56% 32.0M 19s
288700K .......... .......... .......... .......... .......... 56% 27.9M 19s
288750K .......... .......... .......... .......... .......... 56% 34.5M 19s
288800K .......... .......... .......... .......... .......... 56% 26.1M 19s
288850K .......... .......... .......... .......... .......... 56% 22.9M 19s
288900K .......... .......... .......... .......... .......... 56% 6.27M 19s
288950K .......... .......... .......... .......... .......... 56%  131M 19s
289000K .......... .......... .......... .......... .......... 56%  173M 19s
289050K .......... .......... .......... .......... .......... 56%  165M 19s
289100K .......... .......... .......... .......... .......... 56% 6.00M 19s
289150K .......... .......... .......... .......... .......... 56% 16.9M 19s
289200K .......... .......... .......... .......... .......... 56% 5.63M 19s
289250K .......... .......... .......... .......... .......... 56%  157M 19s
289300K .......... .......... .......... .......... .......... 56%  150M 19s
289350K .......... .......... .......... .......... .......... 56%  197M 19s
289400K .......... .......... .......... .......... .......... 56% 39.8M 19s
289450K .......... .......... .......... .......... .......... 56% 32.2M 19s
289500K .......... .......... .......... .......... .......... 56% 18.4M 19s
289550K .......... .......... .......... .......... .......... 56% 20.0M 19s
289600K .......... .......... .......... .......... .......... 56% 15.4M 19s
289650K .......... .......... .......... .......... .......... 56% 19.1M 19s
289700K .......... .......... .......... .......... .......... 56% 17.6M 19s
289750K .......... .......... .......... .......... .......... 56% 17.8M 19s
289800K .......... .......... .......... .......... .......... 57% 15.6M 19s
289850K .......... .......... .......... .......... .......... 57% 13.8M 19s
289900K .......... .......... .......... .......... .......... 57% 19.5M 19s
289950K .......... .......... .......... .......... .......... 57% 11.2M 19s
290000K .......... .......... .......... .......... .......... 57% 12.0M 19s
290050K .......... .......... .......... .......... .......... 57% 12.2M 19s
290100K .......... .......... .......... .......... .......... 57% 13.8M 19s
290150K .......... .......... .......... .......... .......... 57% 15.9M 19s
290200K .......... .......... .......... .......... .......... 57% 12.9M 19s
290250K .......... .......... .......... .......... .......... 57% 15.1M 19s
290300K .......... .......... .......... .......... .......... 57% 14.4M 19s
290350K .......... .......... .......... .......... .......... 57% 14.3M 19s
290400K .......... .......... .......... .......... .......... 57% 16.6M 19s
290450K .......... .......... .......... .......... .......... 57% 9.95M 19s
290500K .......... .......... .......... .......... .......... 57% 9.14M 19s
290550K .......... .......... .......... .......... .......... 57% 12.1M 19s
290600K .......... .......... .......... .......... .......... 57% 10.8M 19s
290650K .......... .......... .......... .......... .......... 57% 11.9M 19s
290700K .......... .......... .......... .......... .......... 57% 10.5M 19s
290750K .......... .......... .......... .......... .......... 57% 12.8M 19s
290800K .......... .......... .......... .......... .......... 57% 11.4M 19s
290850K .......... .......... .......... .......... .......... 57% 12.5M 19s
290900K .......... .......... .......... .......... .......... 57% 16.7M 19s
290950K .......... .......... .......... .......... .......... 57% 49.2M 19s
291000K .......... .......... .......... .......... .......... 57% 38.2M 19s
291050K .......... .......... .......... .......... .......... 57% 23.0M 19s
291100K .......... .......... .......... .......... .......... 57% 86.6M 19s
291150K .......... .......... .......... .......... .......... 57% 57.4M 19s
291200K .......... .......... .......... .......... .......... 57% 18.3M 19s
291250K .......... .......... .......... .......... .......... 57% 58.5M 19s
291300K .......... .......... .......... .......... .......... 57% 27.6M 19s
291350K .......... .......... .......... .......... .......... 57% 26.6M 19s
291400K .......... .......... .......... .......... .......... 57% 24.7M 19s
291450K .......... .......... .......... .......... .......... 57% 22.5M 19s
291500K .......... .......... .......... .......... .......... 57% 26.8M 19s
291550K .......... .......... .......... .......... .......... 57% 25.7M 19s
291600K .......... .......... .......... .......... .......... 57% 20.7M 19s
291650K .......... .......... .......... .......... .......... 57% 23.2M 19s
291700K .......... .......... .......... .......... .......... 57% 26.8M 19s
291750K .......... .......... .......... .......... .......... 57% 26.9M 19s
291800K .......... .......... .......... .......... .......... 57% 27.6M 19s
291850K .......... .......... .......... .......... .......... 57% 18.6M 19s
291900K .......... .......... .......... .......... .......... 57% 32.9M 19s
291950K .......... .......... .......... .......... .......... 57% 19.2M 19s
292000K .......... .......... .......... .......... .......... 57% 19.2M 19s
292050K .......... .......... .......... .......... .......... 57% 21.0M 19s
292100K .......... .......... .......... .......... .......... 57% 19.8M 19s
292150K .......... .......... .......... .......... .......... 57% 24.6M 19s
292200K .......... .......... .......... .......... .......... 57% 14.2M 19s
292250K .......... .......... .......... .......... .......... 57% 16.3M 19s
292300K .......... .......... .......... .......... .......... 57% 31.0M 19s
292350K .......... .......... .......... .......... .......... 57% 36.7M 19s
292400K .......... .......... .......... .......... .......... 57% 30.5M 19s
292450K .......... .......... .......... .......... .......... 57% 32.5M 19s
292500K .......... .......... .......... .......... .......... 57% 29.2M 19s
292550K .......... .......... .......... .......... .......... 57% 28.5M 19s
292600K .......... .......... .......... .......... .......... 57% 25.7M 19s
292650K .......... .......... .......... .......... .......... 57% 22.1M 19s
292700K .......... .......... .......... .......... .......... 57% 29.1M 19s
292750K .......... .......... .......... .......... .......... 57% 32.2M 19s
292800K .......... .......... .......... .......... .......... 57% 25.1M 19s
292850K .......... .......... .......... .......... .......... 57% 25.2M 19s
292900K .......... .......... .......... .......... .......... 57% 22.6M 19s
292950K .......... .......... .......... .......... .......... 57% 23.4M 19s
293000K .......... .......... .......... .......... .......... 57% 28.1M 19s
293050K .......... .......... .......... .......... .......... 57% 22.9M 19s
293100K .......... .......... .......... .......... .......... 57% 24.2M 19s
293150K .......... .......... .......... .......... .......... 57% 35.7M 19s
293200K .......... .......... .......... .......... .......... 57% 25.7M 19s
293250K .......... .......... .......... .......... .......... 57% 18.3M 19s
293300K .......... .......... .......... .......... .......... 57%  173M 19s
293350K .......... .......... .......... .......... .......... 57% 20.5M 19s
293400K .......... .......... .......... .......... .......... 57% 17.1M 19s
293450K .......... .......... .......... .......... .......... 57% 20.6M 19s
293500K .......... .......... .......... .......... .......... 57% 65.5M 19s
293550K .......... .......... .......... .......... .......... 57% 12.9M 19s
293600K .......... .......... .......... .......... .......... 57% 13.6M 19s
293650K .......... .......... .......... .......... .......... 57% 21.0M 19s
293700K .......... .......... .......... .......... .......... 57% 13.0M 19s
293750K .......... .......... .......... .......... .......... 57% 22.2M 19s
293800K .......... .......... .......... .......... .......... 57% 16.3M 19s
293850K .......... .......... .......... .......... .......... 57% 14.3M 19s
293900K .......... .......... .......... .......... .......... 57% 16.5M 19s
293950K .......... .......... .......... .......... .......... 57% 15.1M 19s
294000K .......... .......... .......... .......... .......... 57% 14.3M 19s
294050K .......... .......... .......... .......... .......... 57% 16.8M 19s
294100K .......... .......... .......... .......... .......... 57% 13.3M 19s
294150K .......... .......... .......... .......... .......... 57% 23.0M 18s
294200K .......... .......... .......... .......... .......... 57% 13.3M 18s
294250K .......... .......... .......... .......... .......... 57% 25.8M 18s
294300K .......... .......... .......... .......... .......... 57% 12.5M 18s
294350K .......... .......... .......... .......... .......... 57% 12.9M 18s
294400K .......... .......... .......... .......... .......... 57% 30.1M 18s
294450K .......... .......... .......... .......... .......... 57% 19.9M 18s
294500K .......... .......... .......... .......... .......... 57% 17.2M 18s
294550K .......... .......... .......... .......... .......... 57% 17.3M 18s
294600K .......... .......... .......... .......... .......... 57% 13.3M 18s
294650K .......... .......... .......... .......... .......... 57% 16.2M 18s
294700K .......... .......... .......... .......... .......... 57% 15.4M 18s
294750K .......... .......... .......... .......... .......... 57% 18.5M 18s
294800K .......... .......... .......... .......... .......... 57% 16.2M 18s
294850K .......... .......... .......... .......... .......... 58% 10.5M 18s
294900K .......... .......... .......... .......... .......... 58% 16.4M 18s
294950K .......... .......... .......... .......... .......... 58% 16.8M 18s
295000K .......... .......... .......... .......... .......... 58% 17.5M 18s
295050K .......... .......... .......... .......... .......... 58% 13.6M 18s
295100K .......... .......... .......... .......... .......... 58% 13.8M 18s
295150K .......... .......... .......... .......... .......... 58% 18.3M 18s
295200K .......... .......... .......... .......... .......... 58% 10.6M 18s
295250K .......... .......... .......... .......... .......... 58% 36.2M 18s
295300K .......... .......... .......... .......... .......... 58% 20.6M 18s
295350K .......... .......... .......... .......... .......... 58% 21.8M 18s
295400K .......... .......... .......... .......... .......... 58% 22.7M 18s
295450K .......... .......... .......... .......... .......... 58% 16.8M 18s
295500K .......... .......... .......... .......... .......... 58% 21.7M 18s
295550K .......... .......... .......... .......... .......... 58% 18.2M 18s
295600K .......... .......... .......... .......... .......... 58% 17.8M 18s
295650K .......... .......... .......... .......... .......... 58% 15.5M 18s
295700K .......... .......... .......... .......... .......... 58% 17.3M 18s
295750K .......... .......... .......... .......... .......... 58% 16.6M 18s
295800K .......... .......... .......... .......... .......... 58% 20.7M 18s
295850K .......... .......... .......... .......... .......... 58% 14.5M 18s
295900K .......... .......... .......... .......... .......... 58% 16.2M 18s
295950K .......... .......... .......... .......... .......... 58% 17.8M 18s
296000K .......... .......... .......... .......... .......... 58% 17.6M 18s
296050K .......... .......... .......... .......... .......... 58% 10.4M 18s
296100K .......... .......... .......... .......... .......... 58% 31.3M 18s
296150K .......... .......... .......... .......... .......... 58% 20.8M 18s
296200K .......... .......... .......... .......... .......... 58% 11.1M 18s
296250K .......... .......... .......... .......... .......... 58% 12.8M 18s
296300K .......... .......... .......... .......... .......... 58% 14.6M 18s
296350K .......... .......... .......... .......... .......... 58% 12.5M 18s
296400K .......... .......... .......... .......... .......... 58% 12.9M 18s
296450K .......... .......... .......... .......... .......... 58% 14.4M 18s
296500K .......... .......... .......... .......... .......... 58% 15.2M 18s
296550K .......... .......... .......... .......... .......... 58% 15.4M 18s
296600K .......... .......... .......... .......... .......... 58% 10.2M 18s
296650K .......... .......... .......... .......... .......... 58% 19.0M 18s
296700K .......... .......... .......... .......... .......... 58% 14.2M 18s
296750K .......... .......... .......... .......... .......... 58% 12.3M 18s
296800K .......... .......... .......... .......... .......... 58% 38.1M 18s
296850K .......... .......... .......... .......... .......... 58% 24.1M 18s
296900K .......... .......... .......... .......... .......... 58% 37.4M 18s
296950K .......... .......... .......... .......... .......... 58% 28.4M 18s
297000K .......... .......... .......... .......... .......... 58% 25.1M 18s
297050K .......... .......... .......... .......... .......... 58% 55.2M 18s
297100K .......... .......... .......... .......... .......... 58% 48.6M 18s
297150K .......... .......... .......... .......... .......... 58% 36.5M 18s
297200K .......... .......... .......... .......... .......... 58% 40.8M 18s
297250K .......... .......... .......... .......... .......... 58% 56.0M 18s
297300K .......... .......... .......... .......... .......... 58% 37.0M 18s
297350K .......... .......... .......... .......... .......... 58% 20.9M 18s
297400K .......... .......... .......... .......... .......... 58%  189M 18s
297450K .......... .......... .......... .......... .......... 58% 38.9M 18s
297500K .......... .......... .......... .......... .......... 58% 46.8M 18s
297550K .......... .......... .......... .......... .......... 58% 50.4M 18s
297600K .......... .......... .......... .......... .......... 58% 45.4M 18s
297650K .......... .......... .......... .......... .......... 58% 35.3M 18s
297700K .......... .......... .......... .......... .......... 58% 45.3M 18s
297750K .......... .......... .......... .......... .......... 58% 26.6M 18s
297800K .......... .......... .......... .......... .......... 58% 53.1M 18s
297850K .......... .......... .......... .......... .......... 58% 38.9M 18s
297900K .......... .......... .......... .......... .......... 58% 52.3M 18s
297950K .......... .......... .......... .......... .......... 58% 33.2M 18s
298000K .......... .......... .......... .......... .......... 58% 48.9M 18s
298050K .......... .......... .......... .......... .......... 58% 35.6M 18s
298100K .......... .......... .......... .......... .......... 58% 43.4M 18s
298150K .......... .......... .......... .......... .......... 58% 53.8M 18s
298200K .......... .......... .......... .......... .......... 58% 32.9M 18s
298250K .......... .......... .......... .......... .......... 58% 38.0M 18s
298300K .......... .......... .......... .......... .......... 58% 50.1M 18s
298350K .......... .......... .......... .......... .......... 58% 25.8M 18s
298400K .......... .......... .......... .......... .......... 58%  108M 18s
298450K .......... .......... .......... .......... .......... 58% 42.2M 18s
298500K .......... .......... .......... .......... .......... 58% 22.8M 18s
298550K .......... .......... .......... .......... .......... 58%  144M 18s
298600K .......... .......... .......... .......... .......... 58%  166M 18s
298650K .......... .......... .......... .......... .......... 58% 29.3M 18s
298700K .......... .......... .......... .......... .......... 58% 52.8M 18s
298750K .......... .......... .......... .......... .......... 58% 51.8M 18s
298800K .......... .......... .......... .......... .......... 58% 35.5M 18s
298850K .......... .......... .......... .......... .......... 58% 39.0M 18s
298900K .......... .......... .......... .......... .......... 58% 26.9M 18s
298950K .......... .......... .......... .......... .......... 58% 35.9M 18s
299000K .......... .......... .......... .......... .......... 58% 9.80M 18s
299050K .......... .......... .......... .......... .......... 58%  149M 18s
299100K .......... .......... .......... .......... .......... 58%  145M 18s
299150K .......... .......... .......... .......... .......... 58% 40.1M 18s
299200K .......... .......... .......... .......... .......... 58% 25.7M 18s
299250K .......... .......... .......... .......... .......... 58% 29.7M 18s
299300K .......... .......... .......... .......... .......... 58% 29.5M 18s
299350K .......... .......... .......... .......... .......... 58% 24.6M 18s
299400K .......... .......... .......... .......... .......... 58% 23.0M 18s
299450K .......... .......... .......... .......... .......... 58% 33.7M 18s
299500K .......... .......... .......... .......... .......... 58% 39.8M 18s
299550K .......... .......... .......... .......... .......... 58% 23.1M 18s
299600K .......... .......... .......... .......... .......... 58% 29.0M 18s
299650K .......... .......... .......... .......... .......... 58% 36.5M 18s
299700K .......... .......... .......... .......... .......... 58% 19.0M 18s
299750K .......... .......... .......... .......... .......... 58% 36.1M 18s
299800K .......... .......... .......... .......... .......... 58% 18.8M 18s
299850K .......... .......... .......... .......... .......... 58% 9.33M 18s
299900K .......... .......... .......... .......... .......... 58% 13.1M 18s
299950K .......... .......... .......... .......... .......... 59% 9.34M 18s
300000K .......... .......... .......... .......... .......... 59% 14.6M 18s
300050K .......... .......... .......... .......... .......... 59% 15.6M 18s
300100K .......... .......... .......... .......... .......... 59% 13.5M 18s
300150K .......... .......... .......... .......... .......... 59% 16.0M 18s
300200K .......... .......... .......... .......... .......... 59% 11.4M 18s
300250K .......... .......... .......... .......... .......... 59% 14.3M 18s
300300K .......... .......... .......... .......... .......... 59% 16.4M 18s
300350K .......... .......... .......... .......... .......... 59% 10.4M 18s
300400K .......... .......... .......... .......... .......... 59% 6.66M 18s
300450K .......... .......... .......... .......... .......... 59% 12.5M 18s
300500K .......... .......... .......... .......... .......... 59% 82.5M 18s
300550K .......... .......... .......... .......... .......... 59% 12.8M 18s
300600K .......... .......... .......... .......... .......... 59% 13.6M 18s
300650K .......... .......... .......... .......... .......... 59% 15.0M 18s
300700K .......... .......... .......... .......... .......... 59% 11.8M 18s
300750K .......... .......... .......... .......... .......... 59% 16.5M 18s
300800K .......... .......... .......... .......... .......... 59% 15.3M 18s
300850K .......... .......... .......... .......... .......... 59% 14.4M 18s
300900K .......... .......... .......... .......... .......... 59% 12.6M 18s
300950K .......... .......... .......... .......... .......... 59% 13.6M 18s
301000K .......... .......... .......... .......... .......... 59% 13.8M 18s
301050K .......... .......... .......... .......... .......... 59% 10.8M 18s
301100K .......... .......... .......... .......... .......... 59% 7.01M 18s
301150K .......... .......... .......... .......... .......... 59% 28.0M 18s
301200K .......... .......... .......... .......... .......... 59% 11.3M 18s
301250K .......... .......... .......... .......... .......... 59% 18.0M 18s
301300K .......... .......... .......... .......... .......... 59% 24.2M 18s
301350K .......... .......... .......... .......... .......... 59% 15.8M 18s
301400K .......... .......... .......... .......... .......... 59% 19.4M 18s
301450K .......... .......... .......... .......... .......... 59% 20.6M 18s
301500K .......... .......... .......... .......... .......... 59% 23.4M 18s
301550K .......... .......... .......... .......... .......... 59% 18.2M 18s
301600K .......... .......... .......... .......... .......... 59% 16.6M 18s
301650K .......... .......... .......... .......... .......... 59% 28.1M 18s
301700K .......... .......... .......... .......... .......... 59% 18.4M 18s
301750K .......... .......... .......... .......... .......... 59% 19.2M 18s
301800K .......... .......... .......... .......... .......... 59% 22.7M 18s
301850K .......... .......... .......... .......... .......... 59% 17.0M 18s
301900K .......... .......... .......... .......... .......... 59% 23.4M 18s
301950K .......... .......... .......... .......... .......... 59% 10.7M 18s
302000K .......... .......... .......... .......... .......... 59% 63.0M 18s
302050K .......... .......... .......... .......... .......... 59% 11.6M 18s
302100K .......... .......... .......... .......... .......... 59% 18.0M 18s
302150K .......... .......... .......... .......... .......... 59% 13.2M 18s
302200K .......... .......... .......... .......... .......... 59% 15.1M 18s
302250K .......... .......... .......... .......... .......... 59% 15.3M 18s
302300K .......... .......... .......... .......... .......... 59% 15.0M 18s
302350K .......... .......... .......... .......... .......... 59% 15.9M 18s
302400K .......... .......... .......... .......... .......... 59% 17.0M 18s
302450K .......... .......... .......... .......... .......... 59% 10.5M 18s
302500K .......... .......... .......... .......... .......... 59% 21.1M 18s
302550K .......... .......... .......... .......... .......... 59% 15.0M 18s
302600K .......... .......... .......... .......... .......... 59% 10.9M 18s
302650K .......... .......... .......... .......... .......... 59% 13.0M 18s
302700K .......... .......... .......... .......... .......... 59% 11.8M 18s
302750K .......... .......... .......... .......... .......... 59% 13.2M 18s
302800K .......... .......... .......... .......... .......... 59% 13.8M 18s
302850K .......... .......... .......... .......... .......... 59% 11.1M 18s
302900K .......... .......... .......... .......... .......... 59% 14.9M 18s
302950K .......... .......... .......... .......... .......... 59% 9.65M 18s
303000K .......... .......... .......... .......... .......... 59% 15.9M 18s
303050K .......... .......... .......... .......... .......... 59% 14.6M 18s
303100K .......... .......... .......... .......... .......... 59% 9.48M 18s
303150K .......... .......... .......... .......... .......... 59% 31.7M 18s
303200K .......... .......... .......... .......... .......... 59% 12.2M 18s
303250K .......... .......... .......... .......... .......... 59% 18.9M 18s
303300K .......... .......... .......... .......... .......... 59% 14.6M 17s
303350K .......... .......... .......... .......... .......... 59% 14.8M 17s
303400K .......... .......... .......... .......... .......... 59% 14.1M 17s
303450K .......... .......... .......... .......... .......... 59% 11.1M 17s
303500K .......... .......... .......... .......... .......... 59% 10.4M 17s
303550K .......... .......... .......... .......... .......... 59% 14.0M 17s
303600K .......... .......... .......... .......... .......... 59% 10.4M 17s
303650K .......... .......... .......... .......... .......... 59% 9.39M 17s
303700K .......... .......... .......... .......... .......... 59% 11.7M 17s
303750K .......... .......... .......... .......... .......... 59% 8.24M 17s
303800K .......... .......... .......... .......... .......... 59% 11.9M 17s
303850K .......... .......... .......... .......... .......... 59% 11.0M 17s
303900K .......... .......... .......... .......... .......... 59% 20.0M 17s
303950K .......... .......... .......... .......... .......... 59% 31.4M 17s
304000K .......... .......... .......... .......... .......... 59% 19.3M 17s
304050K .......... .......... .......... .......... .......... 59% 28.3M 17s
304100K .......... .......... .......... .......... .......... 59%  126M 17s
304150K .......... .......... .......... .......... .......... 59% 30.7M 17s
304200K .......... .......... .......... .......... .......... 59% 16.5M 17s
304250K .......... .......... .......... .......... .......... 59% 21.5M 17s
304300K .......... .......... .......... .......... .......... 59% 19.3M 17s
304350K .......... .......... .......... .......... .......... 59% 18.9M 17s
304400K .......... .......... .......... .......... .......... 59% 17.2M 17s
304450K .......... .......... .......... .......... .......... 59% 16.3M 17s
304500K .......... .......... .......... .......... .......... 59% 11.6M 17s
304550K .......... .......... .......... .......... .......... 59% 33.2M 17s
304600K .......... .......... .......... .......... .......... 59% 18.3M 17s
304650K .......... .......... .......... .......... .......... 59% 22.8M 17s
304700K .......... .......... .......... .......... .......... 59% 17.8M 17s
304750K .......... .......... .......... .......... .......... 59% 18.8M 17s
304800K .......... .......... .......... .......... .......... 59% 18.4M 17s
304850K .......... .......... .......... .......... .......... 59% 15.9M 17s
304900K .......... .......... .......... .......... .......... 59% 23.9M 17s
304950K .......... .......... .......... .......... .......... 59% 10.2M 17s
305000K .......... .......... .......... .......... .......... 59%  163M 17s
305050K .......... .......... .......... .......... .......... 60% 30.7M 17s
305100K .......... .......... .......... .......... .......... 60% 16.7M 17s
305150K .......... .......... .......... .......... .......... 60% 30.6M 17s
305200K .......... .......... .......... .......... .......... 60% 21.6M 17s
305250K .......... .......... .......... .......... .......... 60% 25.9M 17s
305300K .......... .......... .......... .......... .......... 60% 22.0M 17s
305350K .......... .......... .......... .......... .......... 60% 16.5M 17s
305400K .......... .......... .......... .......... .......... 60% 24.9M 17s
305450K .......... .......... .......... .......... .......... 60% 28.2M 17s
305500K .......... .......... .......... .......... .......... 60% 26.0M 17s
305550K .......... .......... .......... .......... .......... 60% 18.8M 17s
305600K .......... .......... .......... .......... .......... 60% 25.8M 17s
305650K .......... .......... .......... .......... .......... 60% 28.3M 17s
305700K .......... .......... .......... .......... .......... 60% 23.1M 17s
305750K .......... .......... .......... .......... .......... 60% 24.4M 17s
305800K .......... .......... .......... .......... .......... 60% 21.7M 17s
305850K .......... .......... .......... .......... .......... 60% 30.1M 17s
305900K .......... .......... .......... .......... .......... 60% 23.4M 17s
305950K .......... .......... .......... .......... .......... 60% 23.8M 17s
306000K .......... .......... .......... .......... .......... 60% 19.2M 17s
306050K .......... .......... .......... .......... .......... 60% 14.8M 17s
306100K .......... .......... .......... .......... .......... 60% 13.5M 17s
306150K .......... .......... .......... .......... .......... 60% 16.3M 17s
306200K .......... .......... .......... .......... .......... 60% 15.7M 17s
306250K .......... .......... .......... .......... .......... 60% 14.1M 17s
306300K .......... .......... .......... .......... .......... 60% 15.1M 17s
306350K .......... .......... .......... .......... .......... 60% 15.1M 17s
306400K .......... .......... .......... .......... .......... 60% 16.5M 17s
306450K .......... .......... .......... .......... .......... 60% 15.9M 17s
306500K .......... .......... .......... .......... .......... 60% 14.9M 17s
306550K .......... .......... .......... .......... .......... 60% 14.6M 17s
306600K .......... .......... .......... .......... .......... 60% 90.8M 17s
306650K .......... .......... .......... .......... .......... 60% 44.3M 17s
306700K .......... .......... .......... .......... .......... 60% 21.3M 17s
306750K .......... .......... .......... .......... .......... 60%  142M 17s
306800K .......... .......... .......... .......... .......... 60% 40.8M 17s
306850K .......... .......... .......... .......... .......... 60% 23.6M 17s
306900K .......... .......... .......... .......... .......... 60%  107M 17s
306950K .......... .......... .......... .......... .......... 60% 33.4M 17s
307000K .......... .......... .......... .......... .......... 60% 33.1M 17s
307050K .......... .......... .......... .......... .......... 60% 36.1M 17s
307100K .......... .......... .......... .......... .......... 60% 27.0M 17s
307150K .......... .......... .......... .......... .......... 60% 44.6M 17s
307200K .......... .......... .......... .......... .......... 60% 27.0M 17s
307250K .......... .......... .......... .......... .......... 60% 46.2M 17s
307300K .......... .......... .......... .......... .......... 60% 30.8M 17s
307350K .......... .......... .......... .......... .......... 60% 22.9M 17s
307400K .......... .......... .......... .......... .......... 60% 44.9M 17s
307450K .......... .......... .......... .......... .......... 60% 32.2M 17s
307500K .......... .......... .......... .......... .......... 60% 26.6M 17s
307550K .......... .......... .......... .......... .......... 60% 40.9M 17s
307600K .......... .......... .......... .......... .......... 60% 23.4M 17s
307650K .......... .......... .......... .......... .......... 60% 29.7M 17s
307700K .......... .......... .......... .......... .......... 60% 34.9M 17s
307750K .......... .......... .......... .......... .......... 60% 30.7M 17s
307800K .......... .......... .......... .......... .......... 60% 31.0M 17s
307850K .......... .......... .......... .......... .......... 60% 30.6M 17s
307900K .......... .......... .......... .......... .......... 60% 46.2M 17s
307950K .......... .......... .......... .......... .......... 60% 28.8M 17s
308000K .......... .......... .......... .......... .......... 60% 35.1M 17s
308050K .......... .......... .......... .......... .......... 60% 32.7M 17s
308100K .......... .......... .......... .......... .......... 60% 25.8M 17s
308150K .......... .......... .......... .......... .......... 60% 9.56M 17s
308200K .......... .......... .......... .......... .......... 60%  132M 17s
308250K .......... .......... .......... .......... .......... 60%  222M 17s
308300K .......... .......... .......... .......... .......... 60%  175M 17s
308350K .......... .......... .......... .......... .......... 60% 59.5M 17s
308400K .......... .......... .......... .......... .......... 60% 23.9M 17s
308450K .......... .......... .......... .......... .......... 60% 21.4M 17s
308500K .......... .......... .......... .......... .......... 60% 25.1M 17s
308550K .......... .......... .......... .......... .......... 60% 24.0M 17s
308600K .......... .......... .......... .......... .......... 60% 12.7M 17s
308650K .......... .......... .......... .......... .......... 60% 13.9M 17s
308700K .......... .......... .......... .......... .......... 60% 14.9M 17s
308750K .......... .......... .......... .......... .......... 60% 15.0M 17s
308800K .......... .......... .......... .......... .......... 60% 15.1M 17s
308850K .......... .......... .......... .......... .......... 60% 12.8M 17s
308900K .......... .......... .......... .......... .......... 60% 14.3M 17s
308950K .......... .......... .......... .......... .......... 60% 13.2M 17s
309000K .......... .......... .......... .......... .......... 60% 15.8M 17s
309050K .......... .......... .......... .......... .......... 60% 15.8M 17s
309100K .......... .......... .......... .......... .......... 60% 12.5M 17s
309150K .......... .......... .......... .......... .......... 60% 15.9M 17s
309200K .......... .......... .......... .......... .......... 60% 18.2M 17s
309250K .......... .......... .......... .......... .......... 60% 27.9M 17s
309300K .......... .......... .......... .......... .......... 60% 18.5M 17s
309350K .......... .......... .......... .......... .......... 60% 23.4M 17s
309400K .......... .......... .......... .......... .......... 60% 49.3M 17s
309450K .......... .......... .......... .......... .......... 60% 16.9M 17s
309500K .......... .......... .......... .......... .......... 60% 22.3M 17s
309550K .......... .......... .......... .......... .......... 60% 20.4M 17s
309600K .......... .......... .......... .......... .......... 60% 15.1M 17s
309650K .......... .......... .......... .......... .......... 60% 18.3M 17s
309700K .......... .......... .......... .......... .......... 60% 23.4M 17s
309750K .......... .......... .......... .......... .......... 60% 23.7M 17s
309800K .......... .......... .......... .......... .......... 60% 24.9M 17s
309850K .......... .......... .......... .......... .......... 60% 21.1M 17s
309900K .......... .......... .......... .......... .......... 60% 22.4M 17s
309950K .......... .......... .......... .......... .......... 60% 20.2M 17s
310000K .......... .......... .......... .......... .......... 60% 19.0M 17s
310050K .......... .......... .......... .......... .......... 60% 28.1M 17s
310100K .......... .......... .......... .......... .......... 61% 17.1M 17s
310150K .......... .......... .......... .......... .......... 61% 27.4M 17s
310200K .......... .......... .......... .......... .......... 61% 10.4M 17s
310250K .......... .......... .......... .......... .......... 61% 28.1M 17s
310300K .......... .......... .......... .......... .......... 61% 22.4M 17s
310350K .......... .......... .......... .......... .......... 61% 27.5M 17s
310400K .......... .......... .......... .......... .......... 61% 20.6M 17s
310450K .......... .......... .......... .......... .......... 61% 20.1M 17s
310500K .......... .......... .......... .......... .......... 61% 16.0M 17s
310550K .......... .......... .......... .......... .......... 61% 16.6M 17s
310600K .......... .......... .......... .......... .......... 61% 16.2M 17s
310650K .......... .......... .......... .......... .......... 61% 9.73M 17s
310700K .......... .......... .......... .......... .......... 61% 18.4M 17s
310750K .......... .......... .......... .......... .......... 61% 21.9M 17s
310800K .......... .......... .......... .......... .......... 61% 18.6M 17s
310850K .......... .......... .......... .......... .......... 61% 13.9M 17s
310900K .......... .......... .......... .......... .......... 61% 14.4M 17s
310950K .......... .......... .......... .......... .......... 61% 13.0M 17s
311000K .......... .......... .......... .......... .......... 61% 56.7M 17s
311050K .......... .......... .......... .......... .......... 61% 20.2M 17s
311100K .......... .......... .......... .......... .......... 61% 10.1M 17s
311150K .......... .......... .......... .......... .......... 61% 22.3M 17s
311200K .......... .......... .......... .......... .......... 61% 14.0M 17s
311250K .......... .......... .......... .......... .......... 61% 8.79M 17s
311300K .......... .......... .......... .......... .......... 61% 21.1M 17s
311350K .......... .......... .......... .......... .......... 61% 7.54M 17s
311400K .......... .......... .......... .......... .......... 61% 26.7M 17s
311450K .......... .......... .......... .......... .......... 61% 9.53M 17s
311500K .......... .......... .......... .......... .......... 61% 14.5M 17s
311550K .......... .......... .......... .......... .......... 61% 8.80M 17s
311600K .......... .......... .......... .......... .......... 61% 11.2M 17s
311650K .......... .......... .......... .......... .......... 61% 12.1M 17s
311700K .......... .......... .......... .......... .......... 61% 9.64M 17s
311750K .......... .......... .......... .......... .......... 61% 11.2M 17s
311800K .......... .......... .......... .......... .......... 61% 16.5M 17s
311850K .......... .......... .......... .......... .......... 61% 6.69M 17s
311900K .......... .......... .......... .......... .......... 61% 14.2M 17s
311950K .......... .......... .......... .......... .......... 61% 12.5M 17s
312000K .......... .......... .......... .......... .......... 61% 10.5M 17s
312050K .......... .......... .......... .......... .......... 61% 13.9M 17s
312100K .......... .......... .......... .......... .......... 61% 11.1M 17s
312150K .......... .......... .......... .......... .......... 61% 9.40M 17s
312200K .......... .......... .......... .......... .......... 61% 13.3M 17s
312250K .......... .......... .......... .......... .......... 61% 21.7M 17s
312300K .......... .......... .......... .......... .......... 61% 12.3M 17s
312350K .......... .......... .......... .......... .......... 61% 11.3M 17s
312400K .......... .......... .......... .......... .......... 61% 12.5M 17s
312450K .......... .......... .......... .......... .......... 61% 14.5M 17s
312500K .......... .......... .......... .......... .......... 61% 13.2M 17s
312550K .......... .......... .......... .......... .......... 61% 15.0M 17s
312600K .......... .......... .......... .......... .......... 61% 9.53M 17s
312650K .......... .......... .......... .......... .......... 61% 12.5M 17s
312700K .......... .......... .......... .......... .......... 61% 11.8M 17s
312750K .......... .......... .......... .......... .......... 61% 10.3M 17s
312800K .......... .......... .......... .......... .......... 61% 7.03M 17s
312850K .......... .......... .......... .......... .......... 61% 5.48M 17s
312900K .......... .......... .......... .......... .......... 61% 9.69M 17s
312950K .......... .......... .......... .......... .......... 61% 7.41M 17s
313000K .......... .......... .......... .......... .......... 61% 9.82M 16s
313050K .......... .......... .......... .......... .......... 61% 10.2M 16s
313100K .......... .......... .......... .......... .......... 61% 11.2M 16s
313150K .......... .......... .......... .......... .......... 61% 13.8M 16s
313200K .......... .......... .......... .......... .......... 61% 12.1M 16s
313250K .......... .......... .......... .......... .......... 61% 27.6M 16s
313300K .......... .......... .......... .......... .......... 61% 16.0M 16s
313350K .......... .......... .......... .......... .......... 61% 25.7M 16s
313400K .......... .......... .......... .......... .......... 61% 26.3M 16s
313450K .......... .......... .......... .......... .......... 61% 14.0M 16s
313500K .......... .......... .......... .......... .......... 61% 23.5M 16s
313550K .......... .......... .......... .......... .......... 61% 23.5M 16s
313600K .......... .......... .......... .......... .......... 61% 18.3M 16s
313650K .......... .......... .......... .......... .......... 61% 21.8M 16s
313700K .......... .......... .......... .......... .......... 61% 17.7M 16s
313750K .......... .......... .......... .......... .......... 61% 22.2M 16s
313800K .......... .......... .......... .......... .......... 61% 17.0M 16s
313850K .......... .......... .......... .......... .......... 61% 10.9M 16s
313900K .......... .......... .......... .......... .......... 61% 12.3M 16s
313950K .......... .......... .......... .......... .......... 61% 10.2M 16s
314000K .......... .......... .......... .......... .......... 61% 8.37M 16s
314050K .......... .......... .......... .......... .......... 61% 7.59M 16s
314100K .......... .......... .......... .......... .......... 61% 6.28M 16s
314150K .......... .......... .......... .......... .......... 61% 11.7M 16s
314200K .......... .......... .......... .......... .......... 61% 12.8M 16s
314250K .......... .......... .......... .......... .......... 61% 15.0M 16s
314300K .......... .......... .......... .......... .......... 61% 32.9M 16s
314350K .......... .......... .......... .......... .......... 61% 16.7M 16s
314400K .......... .......... .......... .......... .......... 61% 17.2M 16s
314450K .......... .......... .......... .......... .......... 61% 18.7M 16s
314500K .......... .......... .......... .......... .......... 61% 18.7M 16s
314550K .......... .......... .......... .......... .......... 61% 18.3M 16s
314600K .......... .......... .......... .......... .......... 61% 15.6M 16s
314650K .......... .......... .......... .......... .......... 61% 14.6M 16s
314700K .......... .......... .......... .......... .......... 61% 16.8M 16s
314750K .......... .......... .......... .......... .......... 61% 16.7M 16s
314800K .......... .......... .......... .......... .......... 61% 22.9M 16s
314850K .......... .......... .......... .......... .......... 61% 14.3M 16s
314900K .......... .......... .......... .......... .......... 61% 19.0M 16s
314950K .......... .......... .......... .......... .......... 61% 12.3M 16s
315000K .......... .......... .......... .......... .......... 61% 14.3M 16s
315050K .......... .......... .......... .......... .......... 61% 36.1M 16s
315100K .......... .......... .......... .......... .......... 61% 18.5M 16s
315150K .......... .......... .......... .......... .......... 61% 15.3M 16s
315200K .......... .......... .......... .......... .......... 62% 28.9M 16s
315250K .......... .......... .......... .......... .......... 62% 16.6M 16s
315300K .......... .......... .......... .......... .......... 62% 14.1M 16s
315350K .......... .......... .......... .......... .......... 62% 15.1M 16s
315400K .......... .......... .......... .......... .......... 62% 16.4M 16s
315450K .......... .......... .......... .......... .......... 62% 11.3M 16s
315500K .......... .......... .......... .......... .......... 62% 9.26M 16s
315550K .......... .......... .......... .......... .......... 62% 10.3M 16s
315600K .......... .......... .......... .......... .......... 62% 7.39M 16s
315650K .......... .......... .......... .......... .......... 62% 9.13M 16s
315700K .......... .......... .......... .......... .......... 62% 5.77M 16s
315750K .......... .......... .......... .......... .......... 62% 6.46M 16s
315800K .......... .......... .......... .......... .......... 62% 15.2M 16s
315850K .......... .......... .......... .......... .......... 62% 11.5M 16s
315900K .......... .......... .......... .......... .......... 62% 15.9M 16s
315950K .......... .......... .......... .......... .......... 62% 10.3M 16s
316000K .......... .......... .......... .......... .......... 62% 12.8M 16s
316050K .......... .......... .......... .......... .......... 62% 13.1M 16s
316100K .......... .......... .......... .......... .......... 62% 13.0M 16s
316150K .......... .......... .......... .......... .......... 62% 12.7M 16s
316200K .......... .......... .......... .......... .......... 62% 12.5M 16s
316250K .......... .......... .......... .......... .......... 62% 11.7M 16s
316300K .......... .......... .......... .......... .......... 62% 11.0M 16s
316350K .......... .......... .......... .......... .......... 62% 7.70M 16s
316400K .......... .......... .......... .......... .......... 62% 12.3M 16s
316450K .......... .......... .......... .......... .......... 62% 12.7M 16s
316500K .......... .......... .......... .......... .......... 62% 12.5M 16s
316550K .......... .......... .......... .......... .......... 62% 15.2M 16s
316600K .......... .......... .......... .......... .......... 62% 11.1M 16s
316650K .......... .......... .......... .......... .......... 62% 17.4M 16s
316700K .......... .......... .......... .......... .......... 62% 12.4M 16s
316750K .......... .......... .......... .......... .......... 62% 25.2M 16s
316800K .......... .......... .......... .......... .......... 62% 17.0M 16s
316850K .......... .......... .......... .......... .......... 62%  136M 16s
316900K .......... .......... .......... .......... .......... 62% 78.5M 16s
316950K .......... .......... .......... .......... .......... 62% 27.1M 16s
317000K .......... .......... .......... .......... .......... 62%  143M 16s
317050K .......... .......... .......... .......... .......... 62% 31.3M 16s
317100K .......... .......... .......... .......... .......... 62% 29.0M 16s
317150K .......... .......... .......... .......... .......... 62% 20.3M 16s
317200K .......... .......... .......... .......... .......... 62% 98.8M 16s
317250K .......... .......... .......... .......... .......... 62% 29.3M 16s
317300K .......... .......... .......... .......... .......... 62% 40.3M 16s
317350K .......... .......... .......... .......... .......... 62% 30.6M 16s
317400K .......... .......... .......... .......... .......... 62% 35.8M 16s
317450K .......... .......... .......... .......... .......... 62% 26.9M 16s
317500K .......... .......... .......... .......... .......... 62% 32.3M 16s
317550K .......... .......... .......... .......... .......... 62% 42.1M 16s
317600K .......... .......... .......... .......... .......... 62% 29.9M 16s
317650K .......... .......... .......... .......... .......... 62% 29.5M 16s
317700K .......... .......... .......... .......... .......... 62% 35.2M 16s
317750K .......... .......... .......... .......... .......... 62% 35.0M 16s
317800K .......... .......... .......... .......... .......... 62% 30.3M 16s
317850K .......... .......... .......... .......... .......... 62% 25.0M 16s
317900K .......... .......... .......... .......... .......... 62% 43.3M 16s
317950K .......... .......... .......... .......... .......... 62% 23.5M 16s
318000K .......... .......... .......... .......... .......... 62% 33.2M 16s
318050K .......... .......... .......... .......... .......... 62% 34.3M 16s
318100K .......... .......... .......... .......... .......... 62% 21.9M 16s
318150K .......... .......... .......... .......... .......... 62% 16.4M 16s
318200K .......... .......... .......... .......... .......... 62% 19.2M 16s
318250K .......... .......... .......... .......... .......... 62% 16.3M 16s
318300K .......... .......... .......... .......... .......... 62% 27.9M 16s
318350K .......... .......... .......... .......... .......... 62% 15.5M 16s
318400K .......... .......... .......... .......... .......... 62% 18.5M 16s
318450K .......... .......... .......... .......... .......... 62% 17.1M 16s
318500K .......... .......... .......... .......... .......... 62% 25.8M 16s
318550K .......... .......... .......... .......... .......... 62% 17.2M 16s
318600K .......... .......... .......... .......... .......... 62% 15.9M 16s
318650K .......... .......... .......... .......... .......... 62% 21.9M 16s
318700K .......... .......... .......... .......... .......... 62% 16.2M 16s
318750K .......... .......... .......... .......... .......... 62% 18.2M 16s
318800K .......... .......... .......... .......... .......... 62% 22.5M 16s
318850K .......... .......... .......... .......... .......... 62% 17.0M 16s
318900K .......... .......... .......... .......... .......... 62% 19.1M 16s
318950K .......... .......... .......... .......... .......... 62% 15.2M 16s
319000K .......... .......... .......... .......... .......... 62% 54.6M 16s
319050K .......... .......... .......... .......... .......... 62% 14.2M 16s
319100K .......... .......... .......... .......... .......... 62%  114M 16s
319150K .......... .......... .......... .......... .......... 62% 16.9M 16s
319200K .......... .......... .......... .......... .......... 62% 29.6M 16s
319250K .......... .......... .......... .......... .......... 62% 21.8M 16s
319300K .......... .......... .......... .......... .......... 62% 21.3M 16s
319350K .......... .......... .......... .......... .......... 62% 17.8M 16s
319400K .......... .......... .......... .......... .......... 62% 26.9M 16s
319450K .......... .......... .......... .......... .......... 62% 14.2M 16s
319500K .......... .......... .......... .......... .......... 62% 21.1M 16s
319550K .......... .......... .......... .......... .......... 62% 19.9M 16s
319600K .......... .......... .......... .......... .......... 62% 16.4M 16s
319650K .......... .......... .......... .......... .......... 62% 18.9M 16s
319700K .......... .......... .......... .......... .......... 62% 17.4M 16s
319750K .......... .......... .......... .......... .......... 62% 15.4M 16s
319800K .......... .......... .......... .......... .......... 62% 14.6M 16s
319850K .......... .......... .......... .......... .......... 62% 15.8M 16s
319900K .......... .......... .......... .......... .......... 62% 17.6M 16s
319950K .......... .......... .......... .......... .......... 62% 14.9M 16s
320000K .......... .......... .......... .......... .......... 62% 15.9M 16s
320050K .......... .......... .......... .......... .......... 62% 17.7M 16s
320100K .......... .......... .......... .......... .......... 62% 17.1M 16s
320150K .......... .......... .......... .......... .......... 62% 17.2M 16s
320200K .......... .......... .......... .......... .......... 62% 10.2M 16s
320250K .......... .......... .......... .......... .......... 62%  113M 16s
320300K .......... .......... .......... .......... .......... 63% 13.5M 16s
320350K .......... .......... .......... .......... .......... 63% 11.9M 16s
320400K .......... .......... .......... .......... .......... 63% 18.5M 16s
320450K .......... .......... .......... .......... .......... 63% 13.1M 16s
320500K .......... .......... .......... .......... .......... 63% 16.2M 16s
320550K .......... .......... .......... .......... .......... 63% 14.0M 16s
320600K .......... .......... .......... .......... .......... 63% 12.7M 16s
320650K .......... .......... .......... .......... .......... 63% 16.3M 16s
320700K .......... .......... .......... .......... .......... 63% 12.5M 16s
320750K .......... .......... .......... .......... .......... 63% 19.3M 16s
320800K .......... .......... .......... .......... .......... 63% 15.0M 16s
320850K .......... .......... .......... .......... .......... 63% 12.5M 16s
320900K .......... .......... .......... .......... .......... 63% 9.24M 16s
320950K .......... .......... .......... .......... .......... 63% 19.5M 16s
321000K .......... .......... .......... .......... .......... 63% 29.8M 16s
321050K .......... .......... .......... .......... .......... 63% 14.2M 16s
321100K .......... .......... .......... .......... .......... 63% 8.67M 16s
321150K .......... .......... .......... .......... .......... 63% 11.3M 16s
321200K .......... .......... .......... .......... .......... 63% 9.75M 16s
321250K .......... .......... .......... .......... .......... 63% 12.2M 16s
321300K .......... .......... .......... .......... .......... 63% 10.8M 16s
321350K .......... .......... .......... .......... .......... 63% 9.28M 16s
321400K .......... .......... .......... .......... .......... 63% 9.69M 16s
321450K .......... .......... .......... .......... .......... 63% 6.54M 16s
321500K .......... .......... .......... .......... .......... 63% 21.7M 16s
321550K .......... .......... .......... .......... .......... 63% 17.0M 16s
321600K .......... .......... .......... .......... .......... 63% 14.1M 16s
321650K .......... .......... .......... .......... .......... 63% 19.6M 16s
321700K .......... .......... .......... .......... .......... 63% 18.9M 16s
321750K .......... .......... .......... .......... .......... 63% 20.0M 16s
321800K .......... .......... .......... .......... .......... 63% 18.5M 16s
321850K .......... .......... .......... .......... .......... 63% 16.5M 16s
321900K .......... .......... .......... .......... .......... 63% 22.8M 16s
321950K .......... .......... .......... .......... .......... 63% 21.4M 16s
322000K .......... .......... .......... .......... .......... 63% 17.1M 16s
322050K .......... .......... .......... .......... .......... 63% 20.6M 16s
322100K .......... .......... .......... .......... .......... 63% 19.0M 16s
322150K .......... .......... .......... .......... .......... 63% 25.6M 16s
322200K .......... .......... .......... .......... .......... 63% 16.2M 16s
322250K .......... .......... .......... .......... .......... 63% 22.6M 16s
322300K .......... .......... .......... .......... .......... 63% 21.9M 16s
322350K .......... .......... .......... .......... .......... 63% 18.2M 16s
322400K .......... .......... .......... .......... .......... 63% 12.8M 16s
322450K .......... .......... .......... .......... .......... 63% 63.1M 16s
322500K .......... .......... .......... .......... .......... 63% 20.0M 16s
322550K .......... .......... .......... .......... .......... 63% 22.7M 16s
322600K .......... .......... .......... .......... .......... 63% 12.7M 16s
322650K .......... .......... .......... .......... .......... 63% 19.8M 16s
322700K .......... .......... .......... .......... .......... 63% 14.1M 16s
322750K .......... .......... .......... .......... .......... 63% 19.9M 16s
322800K .......... .......... .......... .......... .......... 63% 16.1M 16s
322850K .......... .......... .......... .......... .......... 63% 17.6M 16s
322900K .......... .......... .......... .......... .......... 63% 17.9M 16s
322950K .......... .......... .......... .......... .......... 63% 14.9M 16s
323000K .......... .......... .......... .......... .......... 63% 24.3M 16s
323050K .......... .......... .......... .......... .......... 63% 19.0M 16s
323100K .......... .......... .......... .......... .......... 63% 15.3M 16s
323150K .......... .......... .......... .......... .......... 63% 17.7M 16s
323200K .......... .......... .......... .......... .......... 63% 11.3M 15s
323250K .......... .......... .......... .......... .......... 63% 13.5M 15s
323300K .......... .......... .......... .......... .......... 63% 11.2M 15s
323350K .......... .......... .......... .......... .......... 63% 9.79M 15s
323400K .......... .......... .......... .......... .......... 63% 11.7M 15s
323450K .......... .......... .......... .......... .......... 63% 10.2M 15s
323500K .......... .......... .......... .......... .......... 63% 10.2M 15s
323550K .......... .......... .......... .......... .......... 63% 10.4M 15s
323600K .......... .......... .......... .......... .......... 63% 10.4M 15s
323650K .......... .......... .......... .......... .......... 63% 11.8M 15s
323700K .......... .......... .......... .......... .......... 63% 8.09M 15s
323750K .......... .......... .......... .......... .......... 63% 8.43M 15s
323800K .......... .......... .......... .......... .......... 63% 10.4M 15s
323850K .......... .......... .......... .......... .......... 63% 8.02M 15s
323900K .......... .......... .......... .......... .......... 63% 5.04M 15s
323950K .......... .......... .......... .......... .......... 63% 6.26M 15s
324000K .......... .......... .......... .......... .......... 63% 24.5M 15s
324050K .......... .......... .......... .......... .......... 63% 11.7M 15s
324100K .......... .......... .......... .......... .......... 63% 10.7M 15s
324150K .......... .......... .......... .......... .......... 63% 12.0M 15s
324200K .......... .......... .......... .......... .......... 63% 10.8M 15s
324250K .......... .......... .......... .......... .......... 63% 13.4M 15s
324300K .......... .......... .......... .......... .......... 63% 11.0M 15s
324350K .......... .......... .......... .......... .......... 63% 8.93M 15s
324400K .......... .......... .......... .......... .......... 63% 13.2M 15s
324450K .......... .......... .......... .......... .......... 63% 6.96M 15s
324500K .......... .......... .......... .......... .......... 63% 22.3M 15s
324550K .......... .......... .......... .......... .......... 63% 26.3M 15s
324600K .......... .......... .......... .......... .......... 63% 17.4M 15s
324650K .......... .......... .......... .......... .......... 63% 15.9M 15s
324700K .......... .......... .......... .......... .......... 63% 17.5M 15s
324750K .......... .......... .......... .......... .......... 63% 21.8M 15s
324800K .......... .......... .......... .......... .......... 63% 19.9M 15s
324850K .......... .......... .......... .......... .......... 63% 15.9M 15s
324900K .......... .......... .......... .......... .......... 63% 13.6M 15s
324950K .......... .......... .......... .......... .......... 63% 16.6M 15s
325000K .......... .......... .......... .......... .......... 63% 18.0M 15s
325050K .......... .......... .......... .......... .......... 63% 15.1M 15s
325100K .......... .......... .......... .......... .......... 63% 14.8M 15s
325150K .......... .......... .......... .......... .......... 63% 49.0M 15s
325200K .......... .......... .......... .......... .......... 63% 34.1M 15s
325250K .......... .......... .......... .......... .......... 63% 20.6M 15s
325300K .......... .......... .......... .......... .......... 63% 85.4M 15s
325350K .......... .......... .......... .......... .......... 64% 29.4M 15s
325400K .......... .......... .......... .......... .......... 64% 24.0M 15s
325450K .......... .......... .......... .......... .......... 64% 17.6M 15s
325500K .......... .......... .......... .......... .......... 64% 23.4M 15s
325550K .......... .......... .......... .......... .......... 64% 18.6M 15s
325600K .......... .......... .......... .......... .......... 64% 19.0M 15s
325650K .......... .......... .......... .......... .......... 64% 23.7M 15s
325700K .......... .......... .......... .......... .......... 64% 22.2M 15s
325750K .......... .......... .......... .......... .......... 64% 24.0M 15s
325800K .......... .......... .......... .......... .......... 64% 17.5M 15s
325850K .......... .......... .......... .......... .......... 64% 18.3M 15s
325900K .......... .......... .......... .......... .......... 64% 21.8M 15s
325950K .......... .......... .......... .......... .......... 64% 21.1M 15s
326000K .......... .......... .......... .......... .......... 64% 14.3M 15s
326050K .......... .......... .......... .......... .......... 64% 47.8M 15s
326100K .......... .......... .......... .......... .......... 64% 16.0M 15s
326150K .......... .......... .......... .......... .......... 64% 17.7M 15s
326200K .......... .......... .......... .......... .......... 64% 7.53M 15s
326250K .......... .......... .......... .......... .......... 64% 20.7M 15s
326300K .......... .......... .......... .......... .......... 64% 20.9M 15s
326350K .......... .......... .......... .......... .......... 64% 14.4M 15s
326400K .......... .......... .......... .......... .......... 64% 16.7M 15s
326450K .......... .......... .......... .......... .......... 64% 16.9M 15s
326500K .......... .......... .......... .......... .......... 64% 24.7M 15s
326550K .......... .......... .......... .......... .......... 64% 19.1M 15s
326600K .......... .......... .......... .......... .......... 64% 17.1M 15s
326650K .......... .......... .......... .......... .......... 64% 20.4M 15s
326700K .......... .......... .......... .......... .......... 64% 20.8M 15s
326750K .......... .......... .......... .......... .......... 64% 25.7M 15s
326800K .......... .......... .......... .......... .......... 64% 18.9M 15s
326850K .......... .......... .......... .......... .......... 64% 15.6M 15s
326900K .......... .......... .......... .......... .......... 64% 15.6M 15s
326950K .......... .......... .......... .......... .......... 64% 15.8M 15s
327000K .......... .......... .......... .......... .......... 64% 9.53M 15s
327050K .......... .......... .......... .......... .......... 64% 23.0M 15s
327100K .......... .......... .......... .......... .......... 64% 12.1M 15s
327150K .......... .......... .......... .......... .......... 64% 19.7M 15s
327200K .......... .......... .......... .......... .......... 64% 14.2M 15s
327250K .......... .......... .......... .......... .......... 64% 16.8M 15s
327300K .......... .......... .......... .......... .......... 64% 17.4M 15s
327350K .......... .......... .......... .......... .......... 64% 14.7M 15s
327400K .......... .......... .......... .......... .......... 64% 14.3M 15s
327450K .......... .......... .......... .......... .......... 64% 17.1M 15s
327500K .......... .......... .......... .......... .......... 64% 15.9M 15s
327550K .......... .......... .......... .......... .......... 64% 14.1M 15s
327600K .......... .......... .......... .......... .......... 64% 14.3M 15s
327650K .......... .......... .......... .......... .......... 64% 15.4M 15s
327700K .......... .......... .......... .......... .......... 64% 13.2M 15s
327750K .......... .......... .......... .......... .......... 64% 16.2M 15s
327800K .......... .......... .......... .......... .......... 64% 25.7M 15s
327850K .......... .......... .......... .......... .......... 64% 13.7M 15s
327900K .......... .......... .......... .......... .......... 64% 19.7M 15s
327950K .......... .......... .......... .......... .......... 64% 17.4M 15s
328000K .......... .......... .......... .......... .......... 64% 30.0M 15s
328050K .......... .......... .......... .......... .......... 64% 13.9M 15s
328100K .......... .......... .......... .......... .......... 64% 24.1M 15s
328150K .......... .......... .......... .......... .......... 64% 18.1M 15s
328200K .......... .......... .......... .......... .......... 64% 18.9M 15s
328250K .......... .......... .......... .......... .......... 64% 24.3M 15s
328300K .......... .......... .......... .......... .......... 64% 22.3M 15s
328350K .......... .......... .......... .......... .......... 64% 17.9M 15s
328400K .......... .......... .......... .......... .......... 64% 24.4M 15s
328450K .......... .......... .......... .......... .......... 64% 14.9M 15s
328500K .......... .......... .......... .......... .......... 64% 22.7M 15s
328550K .......... .......... .......... .......... .......... 64% 21.4M 15s
328600K .......... .......... .......... .......... .......... 64% 18.3M 15s
328650K .......... .......... .......... .......... .......... 64% 22.9M 15s
328700K .......... .......... .......... .......... .......... 64% 16.9M 15s
328750K .......... .......... .......... .......... .......... 64% 33.3M 15s
328800K .......... .......... .......... .......... .......... 64% 26.6M 15s
328850K .......... .......... .......... .......... .......... 64% 11.7M 15s
328900K .......... .......... .......... .......... .......... 64% 27.6M 15s
328950K .......... .......... .......... .......... .......... 64% 43.4M 15s
329000K .......... .......... .......... .......... .......... 64% 16.5M 15s
329050K .......... .......... .......... .......... .......... 64% 24.5M 15s
329100K .......... .......... .......... .......... .......... 64% 22.7M 15s
329150K .......... .......... .......... .......... .......... 64% 20.8M 15s
329200K .......... .......... .......... .......... .......... 64% 19.2M 15s
329250K .......... .......... .......... .......... .......... 64% 24.1M 15s
329300K .......... .......... .......... .......... .......... 64% 21.8M 15s
329350K .......... .......... .......... .......... .......... 64% 20.3M 15s
329400K .......... .......... .......... .......... .......... 64% 22.9M 15s
329450K .......... .......... .......... .......... .......... 64% 19.2M 15s
329500K .......... .......... .......... .......... .......... 64% 17.6M 15s
329550K .......... .......... .......... .......... .......... 64% 21.6M 15s
329600K .......... .......... .......... .......... .......... 64% 19.4M 15s
329650K .......... .......... .......... .......... .......... 64% 15.2M 15s
329700K .......... .......... .......... .......... .......... 64% 15.1M 15s
329750K .......... .......... .......... .......... .......... 64% 15.7M 15s
329800K .......... .......... .......... .......... .......... 64% 12.5M 15s
329850K .......... .......... .......... .......... .......... 64% 9.98M 15s
329900K .......... .......... .......... .......... .......... 64% 8.67M 15s
329950K .......... .......... .......... .......... .......... 64% 16.0M 15s
330000K .......... .......... .......... .......... .......... 64% 10.8M 15s
330050K .......... .......... .......... .......... .......... 64% 13.1M 15s
330100K .......... .......... .......... .......... .......... 64% 9.29M 15s
330150K .......... .......... .......... .......... .......... 64% 15.4M 15s
330200K .......... .......... .......... .......... .......... 64% 9.83M 15s
330250K .......... .......... .......... .......... .......... 64% 7.42M 15s
330300K .......... .......... .......... .......... .......... 64% 7.64M 15s
330350K .......... .......... .......... .......... .......... 64% 10.6M 15s
330400K .......... .......... .......... .......... .......... 64% 11.0M 15s
330450K .......... .......... .......... .......... .......... 65% 9.57M 15s
330500K .......... .......... .......... .......... .......... 65% 15.3M 15s
330550K .......... .......... .......... .......... .......... 65% 11.1M 15s
330600K .......... .......... .......... .......... .......... 65% 8.86M 15s
330650K .......... .......... .......... .......... .......... 65% 12.5M 15s
330700K .......... .......... .......... .......... .......... 65% 15.6M 15s
330750K .......... .......... .......... .......... .......... 65% 31.8M 15s
330800K .......... .......... .......... .......... .......... 65% 19.8M 15s
330850K .......... .......... .......... .......... .......... 65% 32.4M 15s
330900K .......... .......... .......... .......... .......... 65% 11.0M 15s
330950K .......... .......... .......... .......... .......... 65% 18.1M 15s
331000K .......... .......... .......... .......... .......... 65% 14.8M 15s
331050K .......... .......... .......... .......... .......... 65% 13.6M 15s
331100K .......... .......... .......... .......... .......... 65% 11.2M 15s
331150K .......... .......... .......... .......... .......... 65% 14.2M 15s
331200K .......... .......... .......... .......... .......... 65% 11.9M 15s
331250K .......... .......... .......... .......... .......... 65% 15.1M 15s
331300K .......... .......... .......... .......... .......... 65% 12.4M 15s
331350K .......... .......... .......... .......... .......... 65% 14.0M 15s
331400K .......... .......... .......... .......... .......... 65% 10.5M 15s
331450K .......... .......... .......... .......... .......... 65% 17.4M 15s
331500K .......... .......... .......... .......... .......... 65% 70.7M 15s
331550K .......... .......... .......... .......... .......... 65% 16.2M 15s
331600K .......... .......... .......... .......... .......... 65% 31.9M 15s
331650K .......... .......... .......... .......... .......... 65% 41.8M 15s
331700K .......... .......... .......... .......... .......... 65% 15.1M 15s
331750K .......... .......... .......... .......... .......... 65% 17.9M 15s
331800K .......... .......... .......... .......... .......... 65% 20.6M 15s
331850K .......... .......... .......... .......... .......... 65% 17.3M 15s
331900K .......... .......... .......... .......... .......... 65% 21.5M 15s
331950K .......... .......... .......... .......... .......... 65% 19.2M 15s
332000K .......... .......... .......... .......... .......... 65% 22.8M 15s
332050K .......... .......... .......... .......... .......... 65% 20.2M 15s
332100K .......... .......... .......... .......... .......... 65% 19.5M 15s
332150K .......... .......... .......... .......... .......... 65% 15.1M 15s
332200K .......... .......... .......... .......... .......... 65% 40.0M 15s
332250K .......... .......... .......... .......... .......... 65% 17.2M 15s
332300K .......... .......... .......... .......... .......... 65% 29.8M 15s
332350K .......... .......... .......... .......... .......... 65% 17.9M 15s
332400K .......... .......... .......... .......... .......... 65% 21.7M 15s
332450K .......... .......... .......... .......... .......... 65% 16.9M 15s
332500K .......... .......... .......... .......... .......... 65% 33.8M 15s
332550K .......... .......... .......... .......... .......... 65% 52.1M 15s
332600K .......... .......... .......... .......... .......... 65% 20.2M 15s
332650K .......... .......... .......... .......... .......... 65%  162M 15s
332700K .......... .......... .......... .......... .......... 65% 23.5M 15s
332750K .......... .......... .......... .......... .......... 65% 42.5M 15s
332800K .......... .......... .......... .......... .......... 65% 33.5M 15s
332850K .......... .......... .......... .......... .......... 65% 21.2M 15s
332900K .......... .......... .......... .......... .......... 65% 29.0M 15s
332950K .......... .......... .......... .......... .......... 65% 17.8M 15s
333000K .......... .......... .......... .......... .......... 65% 23.8M 15s
333050K .......... .......... .......... .......... .......... 65% 21.2M 15s
333100K .......... .......... .......... .......... .......... 65% 17.2M 15s
333150K .......... .......... .......... .......... .......... 65% 17.8M 15s
333200K .......... .......... .......... .......... .......... 65% 16.4M 15s
333250K .......... .......... .......... .......... .......... 65% 18.0M 15s
333300K .......... .......... .......... .......... .......... 65% 14.9M 15s
333350K .......... .......... .......... .......... .......... 65% 13.3M 15s
333400K .......... .......... .......... .......... .......... 65% 15.1M 15s
333450K .......... .......... .......... .......... .......... 65% 14.2M 15s
333500K .......... .......... .......... .......... .......... 65% 9.65M 15s
333550K .......... .......... .......... .......... .......... 65% 11.6M 15s
333600K .......... .......... .......... .......... .......... 65% 10.5M 15s
333650K .......... .......... .......... .......... .......... 65% 13.4M 15s
333700K .......... .......... .......... .......... .......... 65% 11.9M 14s
333750K .......... .......... .......... .......... .......... 65% 11.8M 14s
333800K .......... .......... .......... .......... .......... 65% 17.6M 14s
333850K .......... .......... .......... .......... .......... 65% 10.0M 14s
333900K .......... .......... .......... .......... .......... 65% 10.7M 14s
333950K .......... .......... .......... .......... .......... 65% 12.3M 14s
334000K .......... .......... .......... .......... .......... 65% 35.1M 14s
334050K .......... .......... .......... .......... .......... 65% 15.3M 14s
334100K .......... .......... .......... .......... .......... 65% 33.7M 14s
334150K .......... .......... .......... .......... .......... 65% 27.2M 14s
334200K .......... .......... .......... .......... .......... 65% 12.6M 14s
334250K .......... .......... .......... .......... .......... 65% 51.0M 14s
334300K .......... .......... .......... .......... .......... 65% 13.9M 14s
334350K .......... .......... .......... .......... .......... 65% 14.5M 14s
334400K .......... .......... .......... .......... .......... 65% 16.2M 14s
334450K .......... .......... .......... .......... .......... 65% 10.4M 14s
334500K .......... .......... .......... .......... .......... 65% 11.4M 14s
334550K .......... .......... .......... .......... .......... 65% 12.9M 14s
334600K .......... .......... .......... .......... .......... 65% 9.76M 14s
334650K .......... .......... .......... .......... .......... 65% 12.8M 14s
334700K .......... .......... .......... .......... .......... 65% 12.6M 14s
334750K .......... .......... .......... .......... .......... 65% 9.19M 14s
334800K .......... .......... .......... .......... .......... 65% 10.5M 14s
334850K .......... .......... .......... .......... .......... 65% 6.80M 14s
334900K .......... .......... .......... .......... .......... 65% 19.6M 14s
334950K .......... .......... .......... .......... .......... 65% 9.30M 14s
335000K .......... .......... .......... .......... .......... 65% 14.8M 14s
335050K .......... .......... .......... .......... .......... 65% 14.2M 14s
335100K .......... .......... .......... .......... .......... 65% 18.3M 14s
335150K .......... .......... .......... .......... .......... 65% 19.8M 14s
335200K .......... .......... .......... .......... .......... 65% 14.8M 14s
335250K .......... .......... .......... .......... .......... 65% 15.5M 14s
335300K .......... .......... .......... .......... .......... 65% 18.5M 14s
335350K .......... .......... .......... .......... .......... 65% 19.7M 14s
335400K .......... .......... .......... .......... .......... 65% 19.9M 14s
335450K .......... .......... .......... .......... .......... 65% 17.6M 14s
335500K .......... .......... .......... .......... .......... 65% 23.8M 14s
335550K .......... .......... .......... .......... .......... 66% 15.6M 14s
335600K .......... .......... .......... .......... .......... 66% 22.4M 14s
335650K .......... .......... .......... .......... .......... 66% 18.0M 14s
335700K .......... .......... .......... .......... .......... 66% 9.41M 14s
335750K .......... .......... .......... .......... .......... 66%  139M 14s
335800K .......... .......... .......... .......... .......... 66%  222M 14s
335850K .......... .......... .......... .......... .......... 66% 19.8M 14s
335900K .......... .......... .......... .......... .......... 66% 26.7M 14s
335950K .......... .......... .......... .......... .......... 66% 13.2M 14s
336000K .......... .......... .......... .......... .......... 66% 16.8M 14s
336050K .......... .......... .......... .......... .......... 66% 15.1M 14s
336100K .......... .......... .......... .......... .......... 66% 15.7M 14s
336150K .......... .......... .......... .......... .......... 66% 13.8M 14s
336200K .......... .......... .......... .......... .......... 66% 14.2M 14s
336250K .......... .......... .......... .......... .......... 66% 14.6M 14s
336300K .......... .......... .......... .......... .......... 66% 13.7M 14s
336350K .......... .......... .......... .......... .......... 66% 12.3M 14s
336400K .......... .......... .......... .......... .......... 66% 13.3M 14s
336450K .......... .......... .......... .......... .......... 66% 7.00M 14s
336500K .......... .......... .......... .......... .......... 66% 9.80M 14s
336550K .......... .......... .......... .......... .......... 66% 11.9M 14s
336600K .......... .......... .......... .......... .......... 66% 9.56M 14s
336650K .......... .......... .......... .......... .......... 66% 10.4M 14s
336700K .......... .......... .......... .......... .......... 66% 9.85M 14s
336750K .......... .......... .......... .......... .......... 66% 12.5M 14s
336800K .......... .......... .......... .......... .......... 66% 9.74M 14s
336850K .......... .......... .......... .......... .......... 66% 10.5M 14s
336900K .......... .......... .......... .......... .......... 66% 13.3M 14s
336950K .......... .......... .......... .......... .......... 66% 18.6M 14s
337000K .......... .......... .......... .......... .......... 66% 16.2M 14s
337050K .......... .......... .......... .......... .......... 66% 19.4M 14s
337100K .......... .......... .......... .......... .......... 66% 11.1M 14s
337150K .......... .......... .......... .......... .......... 66% 12.2M 14s
337200K .......... .......... .......... .......... .......... 66% 23.5M 14s
337250K .......... .......... .......... .......... .......... 66% 17.1M 14s
337300K .......... .......... .......... .......... .......... 66% 17.9M 14s
337350K .......... .......... .......... .......... .......... 66% 18.2M 14s
337400K .......... .......... .......... .......... .......... 66% 18.8M 14s
337450K .......... .......... .......... .......... .......... 66% 18.4M 14s
337500K .......... .......... .......... .......... .......... 66% 22.5M 14s
337550K .......... .......... .......... .......... .......... 66% 23.6M 14s
337600K .......... .......... .......... .......... .......... 66% 21.9M 14s
337650K .......... .......... .......... .......... .......... 66% 26.7M 14s
337700K .......... .......... .......... .......... .......... 66% 19.6M 14s
337750K .......... .......... .......... .......... .......... 66% 18.5M 14s
337800K .......... .......... .......... .......... .......... 66% 24.4M 14s
337850K .......... .......... .......... .......... .......... 66% 25.9M 14s
337900K .......... .......... .......... .......... .......... 66% 22.8M 14s
337950K .......... .......... .......... .......... .......... 66% 22.7M 14s
338000K .......... .......... .......... .......... .......... 66% 28.8M 14s
338050K .......... .......... .......... .......... .......... 66% 81.7M 14s
338100K .......... .......... .......... .......... .......... 66% 36.4M 14s
338150K .......... .......... .......... .......... .......... 66% 56.3M 14s
338200K .......... .......... .......... .......... .......... 66% 14.9M 14s
338250K .......... .......... .......... .......... .......... 66%  241M 14s
338300K .......... .......... .......... .......... .......... 66% 46.2M 14s
338350K .......... .......... .......... .......... .......... 66%  148M 14s
338400K .......... .......... .......... .......... .......... 66%  149M 14s
338450K .......... .......... .......... .......... .......... 66% 45.7M 14s
338500K .......... .......... .......... .......... .......... 66% 88.8M 14s
338550K .......... .......... .......... .......... .......... 66% 48.6M 14s
338600K .......... .......... .......... .......... .......... 66% 31.2M 14s
338650K .......... .......... .......... .......... .......... 66% 48.0M 14s
338700K .......... .......... .......... .......... .......... 66% 29.3M 14s
338750K .......... .......... .......... .......... .......... 66% 36.7M 14s
338800K .......... .......... .......... .......... .......... 66% 36.6M 14s
338850K .......... .......... .......... .......... .......... 66% 31.8M 14s
338900K .......... .......... .......... .......... .......... 66% 37.8M 14s
338950K .......... .......... .......... .......... .......... 66% 36.5M 14s
339000K .......... .......... .......... .......... .......... 66% 36.3M 14s
339050K .......... .......... .......... .......... .......... 66% 30.4M 14s
339100K .......... .......... .......... .......... .......... 66% 38.0M 14s
339150K .......... .......... .......... .......... .......... 66% 33.6M 14s
339200K .......... .......... .......... .......... .......... 66% 39.5M 14s
339250K .......... .......... .......... .......... .......... 66% 45.4M 14s
339300K .......... .......... .......... .......... .......... 66% 31.4M 14s
339350K .......... .......... .......... .......... .......... 66% 32.5M 14s
339400K .......... .......... .......... .......... .......... 66% 41.1M 14s
339450K .......... .......... .......... .......... .......... 66% 29.4M 14s
339500K .......... .......... .......... .......... .......... 66% 32.6M 14s
339550K .......... .......... .......... .......... .......... 66% 47.1M 14s
339600K .......... .......... .......... .......... .......... 66% 35.1M 14s
339650K .......... .......... .......... .......... .......... 66% 36.9M 14s
339700K .......... .......... .......... .......... .......... 66% 36.3M 14s
339750K .......... .......... .......... .......... .......... 66% 45.5M 14s
339800K .......... .......... .......... .......... .......... 66% 34.1M 14s
339850K .......... .......... .......... .......... .......... 66% 36.2M 14s
339900K .......... .......... .......... .......... .......... 66% 71.9M 14s
339950K .......... .......... .......... .......... .......... 66% 27.0M 14s
340000K .......... .......... .......... .......... .......... 66% 15.8M 14s
340050K .......... .......... .......... .......... .......... 66%  208M 14s
340100K .......... .......... .......... .......... .......... 66%  118M 14s
340150K .......... .......... .......... .......... .......... 66% 20.3M 14s
340200K .......... .......... .......... .......... .......... 66%  114M 14s
340250K .......... .......... .......... .......... .......... 66% 15.6M 14s
340300K .......... .......... .......... .......... .......... 66% 41.8M 14s
340350K .......... .......... .......... .......... .......... 66% 25.8M 14s
340400K .......... .......... .......... .......... .......... 66% 22.7M 14s
340450K .......... .......... .......... .......... .......... 66% 28.2M 14s
340500K .......... .......... .......... .......... .......... 66% 23.1M 14s
340550K .......... .......... .......... .......... .......... 66% 26.6M 14s
340600K .......... .......... .......... .......... .......... 67% 26.3M 14s
340650K .......... .......... .......... .......... .......... 67% 20.8M 14s
340700K .......... .......... .......... .......... .......... 67% 25.6M 14s
340750K .......... .......... .......... .......... .......... 67% 29.2M 14s
340800K .......... .......... .......... .......... .......... 67% 24.9M 14s
340850K .......... .......... .......... .......... .......... 67% 22.0M 14s
340900K .......... .......... .......... .......... .......... 67% 32.0M 14s
340950K .......... .......... .......... .......... .......... 67% 25.3M 14s
341000K .......... .......... .......... .......... .......... 67% 21.9M 14s
341050K .......... .......... .......... .......... .......... 67% 18.6M 14s
341100K .......... .......... .......... .......... .......... 67% 18.5M 14s
341150K .......... .......... .......... .......... .......... 67% 24.4M 14s
341200K .......... .......... .......... .......... .......... 67% 16.6M 14s
341250K .......... .......... .......... .......... .......... 67% 37.2M 14s
341300K .......... .......... .......... .......... .......... 67% 22.6M 14s
341350K .......... .......... .......... .......... .......... 67% 21.5M 14s
341400K .......... .......... .......... .......... .......... 67% 10.7M 14s
341450K .......... .......... .......... .......... .......... 67% 14.6M 14s
341500K .......... .......... .......... .......... .......... 67% 17.0M 14s
341550K .......... .......... .......... .......... .......... 67% 15.6M 14s
341600K .......... .......... .......... .......... .......... 67% 15.4M 14s
341650K .......... .......... .......... .......... .......... 67% 19.1M 14s
341700K .......... .......... .......... .......... .......... 67% 17.1M 14s
341750K .......... .......... .......... .......... .......... 67% 18.4M 14s
341800K .......... .......... .......... .......... .......... 67% 16.5M 14s
341850K .......... .......... .......... .......... .......... 67% 15.3M 14s
341900K .......... .......... .......... .......... .......... 67% 18.2M 14s
341950K .......... .......... .......... .......... .......... 67% 11.9M 14s
342000K .......... .......... .......... .......... .......... 67%  202M 14s
342050K .......... .......... .......... .......... .......... 67% 27.1M 14s
342100K .......... .......... .......... .......... .......... 67% 16.1M 14s
342150K .......... .......... .......... .......... .......... 67% 29.4M 14s
342200K .......... .......... .......... .......... .......... 67% 15.8M 14s
342250K .......... .......... .......... .......... .......... 67% 32.3M 14s
342300K .......... .......... .......... .......... .......... 67% 18.7M 14s
342350K .......... .......... .......... .......... .......... 67% 19.8M 14s
342400K .......... .......... .......... .......... .......... 67% 13.5M 14s
342450K .......... .......... .......... .......... .......... 67% 22.0M 14s
342500K .......... .......... .......... .......... .......... 67% 20.9M 14s
342550K .......... .......... .......... .......... .......... 67% 25.0M 14s
342600K .......... .......... .......... .......... .......... 67% 16.5M 14s
342650K .......... .......... .......... .......... .......... 67% 18.7M 14s
342700K .......... .......... .......... .......... .......... 67% 21.6M 14s
342750K .......... .......... .......... .......... .......... 67% 22.3M 14s
342800K .......... .......... .......... .......... .......... 67% 21.1M 14s
342850K .......... .......... .......... .......... .......... 67% 16.9M 14s
342900K .......... .......... .......... .......... .......... 67% 22.3M 14s
342950K .......... .......... .......... .......... .......... 67% 16.4M 14s
343000K .......... .......... .......... .......... .......... 67% 22.7M 14s
343050K .......... .......... .......... .......... .......... 67% 25.3M 14s
343100K .......... .......... .......... .......... .......... 67% 19.2M 14s
343150K .......... .......... .......... .......... .......... 67% 24.5M 14s
343200K .......... .......... .......... .......... .......... 67% 23.1M 14s
343250K .......... .......... .......... .......... .......... 67% 23.4M 14s
343300K .......... .......... .......... .......... .......... 67% 20.1M 14s
343350K .......... .......... .......... .......... .......... 67% 20.2M 14s
343400K .......... .......... .......... .......... .......... 67% 22.3M 14s
343450K .......... .......... .......... .......... .......... 67% 20.3M 14s
343500K .......... .......... .......... .......... .......... 67% 23.0M 14s
343550K .......... .......... .......... .......... .......... 67% 25.9M 14s
343600K .......... .......... .......... .......... .......... 67% 16.2M 14s
343650K .......... .......... .......... .......... .......... 67% 20.7M 14s
343700K .......... .......... .......... .......... .......... 67% 21.3M 14s
343750K .......... .......... .......... .......... .......... 67% 23.0M 14s
343800K .......... .......... .......... .......... .......... 67% 21.0M 14s
343850K .......... .......... .......... .......... .......... 67% 13.7M 13s
343900K .......... .......... .......... .......... .......... 67% 19.6M 13s
343950K .......... .......... .......... .......... .......... 67% 18.4M 13s
344000K .......... .......... .......... .......... .......... 67% 25.4M 13s
344050K .......... .......... .......... .......... .......... 67% 14.4M 13s
344100K .......... .......... .......... .......... .......... 67% 26.6M 13s
344150K .......... .......... .......... .......... .......... 67% 15.3M 13s
344200K .......... .......... .......... .......... .......... 67% 20.5M 13s
344250K .......... .......... .......... .......... .......... 67% 17.6M 13s
344300K .......... .......... .......... .......... .......... 67% 23.1M 13s
344350K .......... .......... .......... .......... .......... 67% 16.9M 13s
344400K .......... .......... .......... .......... .......... 67% 17.4M 13s
344450K .......... .......... .......... .......... .......... 67% 12.1M 13s
344500K .......... .......... .......... .......... .......... 67% 17.7M 13s
344550K .......... .......... .......... .......... .......... 67% 18.7M 13s
344600K .......... .......... .......... .......... .......... 67% 16.7M 13s
344650K .......... .......... .......... .......... .......... 67% 20.8M 13s
344700K .......... .......... .......... .......... .......... 67% 15.5M 13s
344750K .......... .......... .......... .......... .......... 67% 19.2M 13s
344800K .......... .......... .......... .......... .......... 67% 17.2M 13s
344850K .......... .......... .......... .......... .......... 67% 23.5M 13s
344900K .......... .......... .......... .......... .......... 67% 18.0M 13s
344950K .......... .......... .......... .......... .......... 67% 23.6M 13s
345000K .......... .......... .......... .......... .......... 67% 44.6M 13s
345050K .......... .......... .......... .......... .......... 67% 33.4M 13s
345100K .......... .......... .......... .......... .......... 67% 13.8M 13s
345150K .......... .......... .......... .......... .......... 67% 33.8M 13s
345200K .......... .......... .......... .......... .......... 67% 17.9M 13s
345250K .......... .......... .......... .......... .......... 67% 26.3M 13s
345300K .......... .......... .......... .......... .......... 67% 31.4M 13s
345350K .......... .......... .......... .......... .......... 67% 18.7M 13s
345400K .......... .......... .......... .......... .......... 67% 28.3M 13s
345450K .......... .......... .......... .......... .......... 67% 23.1M 13s
345500K .......... .......... .......... .......... .......... 67% 17.4M 13s
345550K .......... .......... .......... .......... .......... 67% 36.0M 13s
345600K .......... .......... .......... .......... .......... 67% 16.1M 13s
345650K .......... .......... .......... .......... .......... 67% 28.9M 13s
345700K .......... .......... .......... .......... .......... 68% 22.7M 13s
345750K .......... .......... .......... .......... .......... 68% 22.0M 13s
345800K .......... .......... .......... .......... .......... 68% 34.1M 13s
345850K .......... .......... .......... .......... .......... 68% 19.5M 13s
345900K .......... .......... .......... .......... .......... 68% 18.8M 13s
345950K .......... .......... .......... .......... .......... 68% 10.5M 13s
346000K .......... .......... .......... .......... .......... 68% 19.0M 13s
346050K .......... .......... .......... .......... .......... 68% 15.9M 13s
346100K .......... .......... .......... .......... .......... 68% 42.9M 13s
346150K .......... .......... .......... .......... .......... 68% 15.5M 13s
346200K .......... .......... .......... .......... .......... 68% 43.2M 13s
346250K .......... .......... .......... .......... .......... 68% 42.3M 13s
346300K .......... .......... .......... .......... .......... 68% 27.6M 13s
346350K .......... .......... .......... .......... .......... 68% 21.2M 13s
346400K .......... .......... .......... .......... .......... 68% 38.8M 13s
346450K .......... .......... .......... .......... .......... 68% 21.8M 13s
346500K .......... .......... .......... .......... .......... 68% 17.3M 13s
346550K .......... .......... .......... .......... .......... 68%  129M 13s
346600K .......... .......... .......... .......... .......... 68% 23.2M 13s
346650K .......... .......... .......... .......... .......... 68% 19.2M 13s
346700K .......... .......... .......... .......... .......... 68% 44.3M 13s
346750K .......... .......... .......... .......... .......... 68% 23.2M 13s
346800K .......... .......... .......... .......... .......... 68% 23.5M 13s
346850K .......... .......... .......... .......... .......... 68% 18.7M 13s
346900K .......... .......... .......... .......... .......... 68% 25.6M 13s
346950K .......... .......... .......... .......... .......... 68% 20.1M 13s
347000K .......... .......... .......... .......... .......... 68% 20.0M 13s
347050K .......... .......... .......... .......... .......... 68% 25.6M 13s
347100K .......... .......... .......... .......... .......... 68% 21.1M 13s
347150K .......... .......... .......... .......... .......... 68% 23.3M 13s
347200K .......... .......... .......... .......... .......... 68% 12.8M 13s
347250K .......... .......... .......... .......... .......... 68% 21.3M 13s
347300K .......... .......... .......... .......... .......... 68% 20.9M 13s
347350K .......... .......... .......... .......... .......... 68% 17.6M 13s
347400K .......... .......... .......... .......... .......... 68% 16.9M 13s
347450K .......... .......... .......... .......... .......... 68% 15.1M 13s
347500K .......... .......... .......... .......... .......... 68% 41.0M 13s
347550K .......... .......... .......... .......... .......... 68% 10.2M 13s
347600K .......... .......... .......... .......... .......... 68% 14.6M 13s
347650K .......... .......... .......... .......... .......... 68% 14.9M 13s
347700K .......... .......... .......... .......... .......... 68% 14.6M 13s
347750K .......... .......... .......... .......... .......... 68% 15.4M 13s
347800K .......... .......... .......... .......... .......... 68% 19.5M 13s
347850K .......... .......... .......... .......... .......... 68% 18.1M 13s
347900K .......... .......... .......... .......... .......... 68% 19.0M 13s
347950K .......... .......... .......... .......... .......... 68% 15.0M 13s
348000K .......... .......... .......... .......... .......... 68% 19.4M 13s
348050K .......... .......... .......... .......... .......... 68% 15.1M 13s
348100K .......... .......... .......... .......... .......... 68% 13.8M 13s
348150K .......... .......... .......... .......... .......... 68% 19.4M 13s
348200K .......... .......... .......... .......... .......... 68% 12.0M 13s
348250K .......... .......... .......... .......... .......... 68% 13.7M 13s
348300K .......... .......... .......... .......... .......... 68% 9.80M 13s
348350K .......... .......... .......... .......... .......... 68% 7.61M 13s
348400K .......... .......... .......... .......... .......... 68% 9.85M 13s
348450K .......... .......... .......... .......... .......... 68% 7.91M 13s
348500K .......... .......... .......... .......... .......... 68% 9.52M 13s
348550K .......... .......... .......... .......... .......... 68% 10.6M 13s
348600K .......... .......... .......... .......... .......... 68% 15.2M 13s
348650K .......... .......... .......... .......... .......... 68% 16.8M 13s
348700K .......... .......... .......... .......... .......... 68% 11.4M 13s
348750K .......... .......... .......... .......... .......... 68% 11.3M 13s
348800K .......... .......... .......... .......... .......... 68% 12.8M 13s
348850K .......... .......... .......... .......... .......... 68% 12.2M 13s
348900K .......... .......... .......... .......... .......... 68% 15.3M 13s
348950K .......... .......... .......... .......... .......... 68% 10.2M 13s
349000K .......... .......... .......... .......... .......... 68% 13.1M 13s
349050K .......... .......... .......... .......... .......... 68% 14.2M 13s
349100K .......... .......... .......... .......... .......... 68% 13.2M 13s
349150K .......... .......... .......... .......... .......... 68% 19.0M 13s
349200K .......... .......... .......... .......... .......... 68% 32.1M 13s
349250K .......... .......... .......... .......... .......... 68% 59.9M 13s
349300K .......... .......... .......... .......... .......... 68% 30.8M 13s
349350K .......... .......... .......... .......... .......... 68% 24.4M 13s
349400K .......... .......... .......... .......... .......... 68% 80.8M 13s
349450K .......... .......... .......... .......... .......... 68% 39.2M 13s
349500K .......... .......... .......... .......... .......... 68% 21.6M 13s
349550K .......... .......... .......... .......... .......... 68% 33.3M 13s
349600K .......... .......... .......... .......... .......... 68% 12.3M 13s
349650K .......... .......... .......... .......... .......... 68% 34.0M 13s
349700K .......... .......... .......... .......... .......... 68% 17.9M 13s
349750K .......... .......... .......... .......... .......... 68% 36.5M 13s
349800K .......... .......... .......... .......... .......... 68% 25.3M 13s
349850K .......... .......... .......... .......... .......... 68% 30.4M 13s
349900K .......... .......... .......... .......... .......... 68% 20.6M 13s
349950K .......... .......... .......... .......... .......... 68% 33.7M 13s
350000K .......... .......... .......... .......... .......... 68% 22.3M 13s
350050K .......... .......... .......... .......... .......... 68% 28.9M 13s
350100K .......... .......... .......... .......... .......... 68% 24.0M 13s
350150K .......... .......... .......... .......... .......... 68% 32.4M 13s
350200K .......... .......... .......... .......... .......... 68% 21.4M 13s
350250K .......... .......... .......... .......... .......... 68% 26.5M 13s
350300K .......... .......... .......... .......... .......... 68% 23.2M 13s
350350K .......... .......... .......... .......... .......... 68% 21.2M 13s
350400K .......... .......... .......... .......... .......... 68% 19.3M 13s
350450K .......... .......... .......... .......... .......... 68% 20.6M 13s
350500K .......... .......... .......... .......... .......... 68% 33.4M 13s
350550K .......... .......... .......... .......... .......... 68% 22.1M 13s
350600K .......... .......... .......... .......... .......... 68% 12.3M 13s
350650K .......... .......... .......... .......... .......... 68% 15.0M 13s
350700K .......... .......... .......... .......... .......... 68% 14.9M 13s
350750K .......... .......... .......... .......... .......... 68% 14.4M 13s
350800K .......... .......... .......... .......... .......... 69% 18.4M 13s
350850K .......... .......... .......... .......... .......... 69% 12.6M 13s
350900K .......... .......... .......... .......... .......... 69% 17.0M 13s
350950K .......... .......... .......... .......... .......... 69% 13.7M 13s
351000K .......... .......... .......... .......... .......... 69% 12.4M 13s
351050K .......... .......... .......... .......... .......... 69% 13.7M 13s
351100K .......... .......... .......... .......... .......... 69% 11.3M 13s
351150K .......... .......... .......... .......... .......... 69% 16.3M 13s
351200K .......... .......... .......... .......... .......... 69% 13.7M 13s
351250K .......... .......... .......... .......... .......... 69% 14.0M 13s
351300K .......... .......... .......... .......... .......... 69% 13.1M 13s
351350K .......... .......... .......... .......... .......... 69% 11.2M 13s
351400K .......... .......... .......... .......... .......... 69% 15.3M 13s
351450K .......... .......... .......... .......... .......... 69% 11.2M 13s
351500K .......... .......... .......... .......... .......... 69% 7.83M 13s
351550K .......... .......... .......... .......... .......... 69%  223M 13s
351600K .......... .......... .......... .......... .......... 69% 8.17M 13s
351650K .......... .......... .......... .......... .......... 69% 23.0M 13s
351700K .......... .......... .......... .......... .......... 69% 11.7M 13s
351750K .......... .......... .......... .......... .......... 69% 19.1M 13s
351800K .......... .......... .......... .......... .......... 69% 16.6M 13s
351850K .......... .......... .......... .......... .......... 69% 17.2M 13s
351900K .......... .......... .......... .......... .......... 69% 17.1M 13s
351950K .......... .......... .......... .......... .......... 69% 12.9M 13s
352000K .......... .......... .......... .......... .......... 69% 17.0M 13s
352050K .......... .......... .......... .......... .......... 69% 14.4M 13s
352100K .......... .......... .......... .......... .......... 69% 14.4M 13s
352150K .......... .......... .......... .......... .......... 69% 11.6M 13s
352200K .......... .......... .......... .......... .......... 69% 8.35M 13s
352250K .......... .......... .......... .......... .......... 69% 12.4M 13s
352300K .......... .......... .......... .......... .......... 69% 13.1M 13s
352350K .......... .......... .......... .......... .......... 69% 12.5M 13s
352400K .......... .......... .......... .......... .......... 69% 16.8M 13s
352450K .......... .......... .......... .......... .......... 69% 11.6M 13s
352500K .......... .......... .......... .......... .......... 69% 14.1M 13s
352550K .......... .......... .......... .......... .......... 69% 16.5M 13s
352600K .......... .......... .......... .......... .......... 69% 12.5M 13s
352650K .......... .......... .......... .......... .......... 69% 9.65M 13s
352700K .......... .......... .......... .......... .......... 69% 16.1M 13s
352750K .......... .......... .......... .......... .......... 69% 32.0M 13s
352800K .......... .......... .......... .......... .......... 69% 18.8M 13s
352850K .......... .......... .......... .......... .......... 69% 61.3M 13s
352900K .......... .......... .......... .......... .......... 69% 38.4M 13s
352950K .......... .......... .......... .......... .......... 69% 67.3M 13s
353000K .......... .......... .......... .......... .......... 69% 32.9M 13s
353050K .......... .......... .......... .......... .......... 69% 33.4M 13s
353100K .......... .......... .......... .......... .......... 69% 28.5M 13s
353150K .......... .......... .......... .......... .......... 69% 30.2M 13s
353200K .......... .......... .......... .......... .......... 69% 29.2M 13s
353250K .......... .......... .......... .......... .......... 69% 26.1M 13s
353300K .......... .......... .......... .......... .......... 69% 35.5M 13s
353350K .......... .......... .......... .......... .......... 69% 26.4M 13s
353400K .......... .......... .......... .......... .......... 69% 40.6M 13s
353450K .......... .......... .......... .......... .......... 69% 22.3M 13s
353500K .......... .......... .......... .......... .......... 69% 48.3M 13s
353550K .......... .......... .......... .......... .......... 69% 31.5M 13s
353600K .......... .......... .......... .......... .......... 69% 25.7M 13s
353650K .......... .......... .......... .......... .......... 69% 17.5M 13s
353700K .......... .......... .......... .......... .......... 69%  122M 13s
353750K .......... .......... .......... .......... .......... 69% 59.3M 13s
353800K .......... .......... .......... .......... .......... 69% 34.4M 13s
353850K .......... .......... .......... .......... .......... 69% 24.5M 13s
353900K .......... .......... .......... .......... .......... 69% 40.1M 13s
353950K .......... .......... .......... .......... .......... 69% 25.4M 13s
354000K .......... .......... .......... .......... .......... 69% 42.4M 13s
354050K .......... .......... .......... .......... .......... 69% 37.2M 13s
354100K .......... .......... .......... .......... .......... 69% 22.9M 13s
354150K .......... .......... .......... .......... .......... 69% 49.6M 13s
354200K .......... .......... .......... .......... .......... 69% 34.6M 13s
354250K .......... .......... .......... .......... .......... 69% 56.5M 13s
354300K .......... .......... .......... .......... .......... 69% 18.2M 13s
354350K .......... .......... .......... .......... .......... 69%  139M 13s
354400K .......... .......... .......... .......... .......... 69% 36.1M 12s
354450K .......... .......... .......... .......... .......... 69%  119M 12s
354500K .......... .......... .......... .......... .......... 69% 90.8M 12s
354550K .......... .......... .......... .......... .......... 69% 34.5M 12s
354600K .......... .......... .......... .......... .......... 69% 37.5M 12s
354650K .......... .......... .......... .......... .......... 69%  210M 12s
354700K .......... .......... .......... .......... .......... 69% 18.8M 12s
354750K .......... .......... .......... .......... .......... 69% 25.4M 12s
354800K .......... .......... .......... .......... .......... 69% 21.4M 12s
354850K .......... .......... .......... .......... .......... 69% 22.5M 12s
354900K .......... .......... .......... .......... .......... 69% 26.9M 12s
354950K .......... .......... .......... .......... .......... 69% 25.4M 12s
355000K .......... .......... .......... .......... .......... 69% 32.3M 12s
355050K .......... .......... .......... .......... .......... 69% 31.2M 12s
355100K .......... .......... .......... .......... .......... 69% 23.2M 12s
355150K .......... .......... .......... .......... .......... 69% 32.3M 12s
355200K .......... .......... .......... .......... .......... 69% 21.2M 12s
355250K .......... .......... .......... .......... .......... 69% 26.7M 12s
355300K .......... .......... .......... .......... .......... 69% 32.1M 12s
355350K .......... .......... .......... .......... .......... 69% 22.7M 12s
355400K .......... .......... .......... .......... .......... 69% 23.8M 12s
355450K .......... .......... .......... .......... .......... 69% 25.1M 12s
355500K .......... .......... .......... .......... .......... 69% 29.5M 12s
355550K .......... .......... .......... .......... .......... 69% 20.8M 12s
355600K .......... .......... .......... .......... .......... 69% 29.7M 12s
355650K .......... .......... .......... .......... .......... 69% 19.0M 12s
355700K .......... .......... .......... .......... .......... 69% 19.8M 12s
355750K .......... .......... .......... .......... .......... 69% 24.7M 12s
355800K .......... .......... .......... .......... .......... 69% 39.3M 12s
355850K .......... .......... .......... .......... .......... 69% 45.5M 12s
355900K .......... .......... .......... .......... .......... 70% 36.7M 12s
355950K .......... .......... .......... .......... .......... 70% 64.3M 12s
356000K .......... .......... .......... .......... .......... 70% 98.4M 12s
356050K .......... .......... .......... .......... .......... 70% 17.0M 12s
356100K .......... .......... .......... .......... .......... 70%  121M 12s
356150K .......... .......... .......... .......... .......... 70%  214M 12s
356200K .......... .......... .......... .......... .......... 70% 17.9M 12s
356250K .......... .......... .......... .......... .......... 70%  214M 12s
356300K .......... .......... .......... .......... .......... 70%  216M 12s
356350K .......... .......... .......... .......... .......... 70% 29.8M 12s
356400K .......... .......... .......... .......... .......... 70% 60.0M 12s
356450K .......... .......... .......... .......... .......... 70% 32.3M 12s
356500K .......... .......... .......... .......... .......... 70% 34.9M 12s
356550K .......... .......... .......... .......... .......... 70% 49.2M 12s
356600K .......... .......... .......... .......... .......... 70% 25.4M 12s
356650K .......... .......... .......... .......... .......... 70% 40.2M 12s
356700K .......... .......... .......... .......... .......... 70% 30.1M 12s
356750K .......... .......... .......... .......... .......... 70% 31.2M 12s
356800K .......... .......... .......... .......... .......... 70% 45.8M 12s
356850K .......... .......... .......... .......... .......... 70% 25.0M 12s
356900K .......... .......... .......... .......... .......... 70% 43.7M 12s
356950K .......... .......... .......... .......... .......... 70% 24.4M 12s
357000K .......... .......... .......... .......... .......... 70% 50.5M 12s
357050K .......... .......... .......... .......... .......... 70% 31.5M 12s
357100K .......... .......... .......... .......... .......... 70% 43.9M 12s
357150K .......... .......... .......... .......... .......... 70% 33.9M 12s
357200K .......... .......... .......... .......... .......... 70% 35.9M 12s
357250K .......... .......... .......... .......... .......... 70% 38.7M 12s
357300K .......... .......... .......... .......... .......... 70% 27.7M 12s
357350K .......... .......... .......... .......... .......... 70% 32.7M 12s
357400K .......... .......... .......... .......... .......... 70% 43.6M 12s
357450K .......... .......... .......... .......... .......... 70% 32.4M 12s
357500K .......... .......... .......... .......... .......... 70% 37.1M 12s
357550K .......... .......... .......... .......... .......... 70% 28.2M 12s
357600K .......... .......... .......... .......... .......... 70% 20.8M 12s
357650K .......... .......... .......... .......... .......... 70% 13.2M 12s
357700K .......... .......... .......... .......... .......... 70% 64.4M 12s
357750K .......... .......... .......... .......... .......... 70% 17.4M 12s
357800K .......... .......... .......... .......... .......... 70%  140M 12s
357850K .......... .......... .......... .......... .......... 70% 39.0M 12s
357900K .......... .......... .......... .......... .......... 70% 20.8M 12s
357950K .......... .......... .......... .......... .......... 70% 58.9M 12s
358000K .......... .......... .......... .......... .......... 70% 24.5M 12s
358050K .......... .......... .......... .......... .......... 70% 48.2M 12s
358100K .......... .......... .......... .......... .......... 70% 23.8M 12s
358150K .......... .......... .......... .......... .......... 70% 36.8M 12s
358200K .......... .......... .......... .......... .......... 70% 28.6M 12s
358250K .......... .......... .......... .......... .......... 70% 33.5M 12s
358300K .......... .......... .......... .......... .......... 70% 25.3M 12s
358350K .......... .......... .......... .......... .......... 70% 33.4M 12s
358400K .......... .......... .......... .......... .......... 70% 31.7M 12s
358450K .......... .......... .......... .......... .......... 70% 30.3M 12s
358500K .......... .......... .......... .......... .......... 70% 27.6M 12s
358550K .......... .......... .......... .......... .......... 70% 32.4M 12s
358600K .......... .......... .......... .......... .......... 70% 22.8M 12s
358650K .......... .......... .......... .......... .......... 70% 33.4M 12s
358700K .......... .......... .......... .......... .......... 70% 25.8M 12s
358750K .......... .......... .......... .......... .......... 70% 43.0M 12s
358800K .......... .......... .......... .......... .......... 70% 21.5M 12s
358850K .......... .......... .......... .......... .......... 70% 31.8M 12s
358900K .......... .......... .......... .......... .......... 70% 32.9M 12s
358950K .......... .......... .......... .......... .......... 70% 24.6M 12s
359000K .......... .......... .......... .......... .......... 70% 34.4M 12s
359050K .......... .......... .......... .......... .......... 70% 35.0M 12s
359100K .......... .......... .......... .......... .......... 70% 33.5M 12s
359150K .......... .......... .......... .......... .......... 70% 15.3M 12s
359200K .......... .......... .......... .......... .......... 70% 50.3M 12s
359250K .......... .......... .......... .......... .......... 70%  249M 12s
359300K .......... .......... .......... .......... .......... 70% 14.5M 12s
359350K .......... .......... .......... .......... .......... 70%  126M 12s
359400K .......... .......... .......... .......... .......... 70%  149M 12s
359450K .......... .......... .......... .......... .......... 70% 21.8M 12s
359500K .......... .......... .......... .......... .......... 70% 50.8M 12s
359550K .......... .......... .......... .......... .......... 70% 31.2M 12s
359600K .......... .......... .......... .......... .......... 70% 22.9M 12s
359650K .......... .......... .......... .......... .......... 70% 22.4M 12s
359700K .......... .......... .......... .......... .......... 70% 24.3M 12s
359750K .......... .......... .......... .......... .......... 70% 30.3M 12s
359800K .......... .......... .......... .......... .......... 70% 13.3M 12s
359850K .......... .......... .......... .......... .......... 70% 19.1M 12s
359900K .......... .......... .......... .......... .......... 70% 23.6M 12s
359950K .......... .......... .......... .......... .......... 70% 20.4M 12s
360000K .......... .......... .......... .......... .......... 70% 23.5M 12s
360050K .......... .......... .......... .......... .......... 70% 35.6M 12s
360100K .......... .......... .......... .......... .......... 70% 22.0M 12s
360150K .......... .......... .......... .......... .......... 70% 18.9M 12s
360200K .......... .......... .......... .......... .......... 70% 21.7M 12s
360250K .......... .......... .......... .......... .......... 70% 29.9M 12s
360300K .......... .......... .......... .......... .......... 70% 20.3M 12s
360350K .......... .......... .......... .......... .......... 70% 12.6M 12s
360400K .......... .......... .......... .......... .......... 70%  214M 12s
360450K .......... .......... .......... .......... .......... 70% 22.8M 12s
360500K .......... .......... .......... .......... .......... 70% 48.0M 12s
360550K .......... .......... .......... .......... .......... 70% 40.2M 12s
360600K .......... .......... .......... .......... .......... 70% 27.9M 12s
360650K .......... .......... .......... .......... .......... 70% 38.7M 12s
360700K .......... .......... .......... .......... .......... 70% 23.7M 12s
360750K .......... .......... .......... .......... .......... 70% 34.8M 12s
360800K .......... .......... .......... .......... .......... 70% 34.5M 12s
360850K .......... .......... .......... .......... .......... 70% 25.2M 12s
360900K .......... .......... .......... .......... .......... 70% 39.5M 12s
360950K .......... .......... .......... .......... .......... 71% 23.7M 12s
361000K .......... .......... .......... .......... .......... 71% 27.1M 12s
361050K .......... .......... .......... .......... .......... 71% 32.6M 12s
361100K .......... .......... .......... .......... .......... 71% 33.0M 12s
361150K .......... .......... .......... .......... .......... 71% 27.1M 12s
361200K .......... .......... .......... .......... .......... 71% 23.4M 12s
361250K .......... .......... .......... .......... .......... 71% 29.8M 12s
361300K .......... .......... .......... .......... .......... 71% 30.5M 12s
361350K .......... .......... .......... .......... .......... 71% 25.2M 12s
361400K .......... .......... .......... .......... .......... 71% 37.9M 12s
361450K .......... .......... .......... .......... .......... 71% 28.1M 12s
361500K .......... .......... .......... .......... .......... 71% 40.5M 12s
361550K .......... .......... .......... .......... .......... 71% 49.2M 12s
361600K .......... .......... .......... .......... .......... 71% 70.9M 12s
361650K .......... .......... .......... .......... .......... 71% 18.0M 12s
361700K .......... .......... .......... .......... .......... 71%  145M 12s
361750K .......... .......... .......... .......... .......... 71% 34.4M 12s
361800K .......... .......... .......... .......... .......... 71% 56.3M 12s
361850K .......... .......... .......... .......... .......... 71% 30.4M 12s
361900K .......... .......... .......... .......... .......... 71%  121M 12s
361950K .......... .......... .......... .......... .......... 71% 30.3M 12s
362000K .......... .......... .......... .......... .......... 71% 43.8M 12s
362050K .......... .......... .......... .......... .......... 71% 27.0M 12s
362100K .......... .......... .......... .......... .......... 71% 20.8M 12s
362150K .......... .......... .......... .......... .......... 71% 34.1M 12s
362200K .......... .......... .......... .......... .......... 71% 27.7M 12s
362250K .......... .......... .......... .......... .......... 71% 34.3M 12s
362300K .......... .......... .......... .......... .......... 71% 19.5M 12s
362350K .......... .......... .......... .......... .......... 71% 32.1M 12s
362400K .......... .......... .......... .......... .......... 71% 24.0M 12s
362450K .......... .......... .......... .......... .......... 71% 38.5M 12s
362500K .......... .......... .......... .......... .......... 71% 19.8M 12s
362550K .......... .......... .......... .......... .......... 71% 35.3M 12s
362600K .......... .......... .......... .......... .......... 71% 25.1M 12s
362650K .......... .......... .......... .......... .......... 71% 21.2M 12s
362700K .......... .......... .......... .......... .......... 71% 30.9M 12s
362750K .......... .......... .......... .......... .......... 71% 25.0M 12s
362800K .......... .......... .......... .......... .......... 71% 36.9M 12s
362850K .......... .......... .......... .......... .......... 71% 20.1M 12s
362900K .......... .......... .......... .......... .......... 71% 25.2M 12s
362950K .......... .......... .......... .......... .......... 71% 18.7M 12s
363000K .......... .......... .......... .......... .......... 71% 23.8M 12s
363050K .......... .......... .......... .......... .......... 71% 32.1M 12s
363100K .......... .......... .......... .......... .......... 71% 19.7M 12s
363150K .......... .......... .......... .......... .......... 71% 28.9M 12s
363200K .......... .......... .......... .......... .......... 71% 27.9M 12s
363250K .......... .......... .......... .......... .......... 71% 41.3M 12s
363300K .......... .......... .......... .......... .......... 71% 27.9M 12s
363350K .......... .......... .......... .......... .......... 71% 22.3M 12s
363400K .......... .......... .......... .......... .......... 71% 19.4M 12s
363450K .......... .......... .......... .......... .......... 71% 21.9M 12s
363500K .......... .......... .......... .......... .......... 71% 24.0M 12s
363550K .......... .......... .......... .......... .......... 71% 22.3M 12s
363600K .......... .......... .......... .......... .......... 71% 20.6M 12s
363650K .......... .......... .......... .......... .......... 71% 24.3M 12s
363700K .......... .......... .......... .......... .......... 71% 19.2M 12s
363750K .......... .......... .......... .......... .......... 71% 18.9M 12s
363800K .......... .......... .......... .......... .......... 71% 22.2M 12s
363850K .......... .......... .......... .......... .......... 71% 18.9M 12s
363900K .......... .......... .......... .......... .......... 71% 18.4M 12s
363950K .......... .......... .......... .......... .......... 71% 22.4M 12s
364000K .......... .......... .......... .......... .......... 71% 16.4M 12s
364050K .......... .......... .......... .......... .......... 71% 15.6M 12s
364100K .......... .......... .......... .......... .......... 71% 20.8M 12s
364150K .......... .......... .......... .......... .......... 71% 11.3M 12s
364200K .......... .......... .......... .......... .......... 71% 15.5M 12s
364250K .......... .......... .......... .......... .......... 71%  126M 12s
364300K .......... .......... .......... .......... .......... 71% 17.6M 12s
364350K .......... .......... .......... .......... .......... 71% 17.6M 12s
364400K .......... .......... .......... .......... .......... 71% 13.1M 12s
364450K .......... .......... .......... .......... .......... 71% 10.7M 11s
364500K .......... .......... .......... .......... .......... 71% 10.9M 11s
364550K .......... .......... .......... .......... .......... 71% 11.2M 11s
364600K .......... .......... .......... .......... .......... 71% 10.3M 11s
364650K .......... .......... .......... .......... .......... 71% 12.0M 11s
364700K .......... .......... .......... .......... .......... 71% 9.81M 11s
364750K .......... .......... .......... .......... .......... 71% 9.12M 11s
364800K .......... .......... .......... .......... .......... 71% 6.94M 11s
364850K .......... .......... .......... .......... .......... 71% 12.3M 11s
364900K .......... .......... .......... .......... .......... 71% 11.2M 11s
364950K .......... .......... .......... .......... .......... 71% 8.82M 11s
365000K .......... .......... .......... .......... .......... 71% 12.4M 11s
365050K .......... .......... .......... .......... .......... 71% 15.5M 11s
365100K .......... .......... .......... .......... .......... 71% 14.0M 11s
365150K .......... .......... .......... .......... .......... 71% 15.5M 11s
365200K .......... .......... .......... .......... .......... 71% 10.4M 11s
365250K .......... .......... .......... .......... .......... 71% 16.3M 11s
365300K .......... .......... .......... .......... .......... 71% 15.6M 11s
365350K .......... .......... .......... .......... .......... 71% 11.2M 11s
365400K .......... .......... .......... .......... .......... 71% 12.9M 11s
365450K .......... .......... .......... .......... .......... 71% 14.7M 11s
365500K .......... .......... .......... .......... .......... 71% 11.6M 11s
365550K .......... .......... .......... .......... .......... 71% 20.0M 11s
365600K .......... .......... .......... .......... .......... 71% 11.6M 11s
365650K .......... .......... .......... .......... .......... 71% 11.0M 11s
365700K .......... .......... .......... .......... .......... 71% 14.4M 11s
365750K .......... .......... .......... .......... .......... 71% 12.0M 11s
365800K .......... .......... .......... .......... .......... 71% 11.8M 11s
365850K .......... .......... .......... .......... .......... 71% 9.86M 11s
365900K .......... .......... .......... .......... .......... 71% 12.4M 11s
365950K .......... .......... .......... .......... .......... 71% 6.93M 11s
366000K .......... .......... .......... .......... .......... 71% 33.2M 11s
366050K .......... .......... .......... .......... .......... 72% 21.3M 11s
366100K .......... .......... .......... .......... .......... 72% 13.6M 11s
366150K .......... .......... .......... .......... .......... 72% 17.3M 11s
366200K .......... .......... .......... .......... .......... 72% 23.5M 11s
366250K .......... .......... .......... .......... .......... 72% 20.0M 11s
366300K .......... .......... .......... .......... .......... 72% 17.5M 11s
366350K .......... .......... .......... .......... .......... 72% 23.1M 11s
366400K .......... .......... .......... .......... .......... 72% 18.3M 11s
366450K .......... .......... .......... .......... .......... 72% 11.5M 11s
366500K .......... .......... .......... .......... .......... 72% 16.6M 11s
366550K .......... .......... .......... .......... .......... 72% 13.6M 11s
366600K .......... .......... .......... .......... .......... 72% 9.00M 11s
366650K .......... .......... .......... .......... .......... 72% 7.36M 11s
366700K .......... .......... .......... .......... .......... 72% 16.0M 11s
366750K .......... .......... .......... .......... .......... 72% 9.87M 11s
366800K .......... .......... .......... .......... .......... 72% 12.9M 11s
366850K .......... .......... .......... .......... .......... 72% 12.4M 11s
366900K .......... .......... .......... .......... .......... 72% 17.9M 11s
366950K .......... .......... .......... .......... .......... 72% 12.7M 11s
367000K .......... .......... .......... .......... .......... 72% 9.72M 11s
367050K .......... .......... .......... .......... .......... 72% 12.6M 11s
367100K .......... .......... .......... .......... .......... 72% 15.5M 11s
367150K .......... .......... .......... .......... .......... 72% 32.2M 11s
367200K .......... .......... .......... .......... .......... 72% 40.9M 11s
367250K .......... .......... .......... .......... .......... 72% 20.6M 11s
367300K .......... .......... .......... .......... .......... 72%  189M 11s
367350K .......... .......... .......... .......... .......... 72% 49.5M 11s
367400K .......... .......... .......... .......... .......... 72% 22.1M 11s
367450K .......... .......... .......... .......... .......... 72% 52.8M 11s
367500K .......... .......... .......... .......... .......... 72% 28.5M 11s
367550K .......... .......... .......... .......... .......... 72% 26.6M 11s
367600K .......... .......... .......... .......... .......... 72% 18.6M 11s
367650K .......... .......... .......... .......... .......... 72% 27.6M 11s
367700K .......... .......... .......... .......... .......... 72% 33.4M 11s
367750K .......... .......... .......... .......... .......... 72% 24.8M 11s
367800K .......... .......... .......... .......... .......... 72% 26.4M 11s
367850K .......... .......... .......... .......... .......... 72% 25.1M 11s
367900K .......... .......... .......... .......... .......... 72% 19.2M 11s
367950K .......... .......... .......... .......... .......... 72% 27.6M 11s
368000K .......... .......... .......... .......... .......... 72% 14.1M 11s
368050K .......... .......... .......... .......... .......... 72% 33.1M 11s
368100K .......... .......... .......... .......... .......... 72% 26.1M 11s
368150K .......... .......... .......... .......... .......... 72% 21.0M 11s
368200K .......... .......... .......... .......... .......... 72% 28.3M 11s
368250K .......... .......... .......... .......... .......... 72% 24.8M 11s
368300K .......... .......... .......... .......... .......... 72% 23.2M 11s
368350K .......... .......... .......... .......... .......... 72% 20.8M 11s
368400K .......... .......... .......... .......... .......... 72% 21.5M 11s
368450K .......... .......... .......... .......... .......... 72% 20.2M 11s
368500K .......... .......... .......... .......... .......... 72% 22.1M 11s
368550K .......... .......... .......... .......... .......... 72% 28.2M 11s
368600K .......... .......... .......... .......... .......... 72% 20.5M 11s
368650K .......... .......... .......... .......... .......... 72% 20.4M 11s
368700K .......... .......... .......... .......... .......... 72% 19.5M 11s
368750K .......... .......... .......... .......... .......... 72% 22.1M 11s
368800K .......... .......... .......... .......... .......... 72% 23.9M 11s
368850K .......... .......... .......... .......... .......... 72% 18.8M 11s
368900K .......... .......... .......... .......... .......... 72% 22.7M 11s
368950K .......... .......... .......... .......... .......... 72% 13.3M 11s
369000K .......... .......... .......... .......... .......... 72%  213M 11s
369050K .......... .......... .......... .......... .......... 72% 26.0M 11s
369100K .......... .......... .......... .......... .......... 72% 17.0M 11s
369150K .......... .......... .......... .......... .......... 72% 24.6M 11s
369200K .......... .......... .......... .......... .......... 72% 13.9M 11s
369250K .......... .......... .......... .......... .......... 72% 19.4M 11s
369300K .......... .......... .......... .......... .......... 72% 16.3M 11s
369350K .......... .......... .......... .......... .......... 72% 16.6M 11s
369400K .......... .......... .......... .......... .......... 72% 15.4M 11s
369450K .......... .......... .......... .......... .......... 72% 13.8M 11s
369500K .......... .......... .......... .......... .......... 72% 21.7M 11s
369550K .......... .......... .......... .......... .......... 72% 13.9M 11s
369600K .......... .......... .......... .......... .......... 72% 14.8M 11s
369650K .......... .......... .......... .......... .......... 72% 15.0M 11s
369700K .......... .......... .......... .......... .......... 72% 15.6M 11s
369750K .......... .......... .......... .......... .......... 72% 28.5M 11s
369800K .......... .......... .......... .......... .......... 72% 21.5M 11s
369850K .......... .......... .......... .......... .......... 72% 21.3M 11s
369900K .......... .......... .......... .......... .......... 72% 16.0M 11s
369950K .......... .......... .......... .......... .......... 72%  167M 11s
370000K .......... .......... .......... .......... .......... 72% 25.6M 11s
370050K .......... .......... .......... .......... .......... 72% 17.0M 11s
370100K .......... .......... .......... .......... .......... 72% 15.3M 11s
370150K .......... .......... .......... .......... .......... 72% 15.3M 11s
370200K .......... .......... .......... .......... .......... 72% 21.1M 11s
370250K .......... .......... .......... .......... .......... 72% 15.8M 11s
370300K .......... .......... .......... .......... .......... 72% 14.0M 11s
370350K .......... .......... .......... .......... .......... 72% 14.7M 11s
370400K .......... .......... .......... .......... .......... 72% 20.6M 11s
370450K .......... .......... .......... .......... .......... 72% 13.4M 11s
370500K .......... .......... .......... .......... .......... 72% 13.8M 11s
370550K .......... .......... .......... .......... .......... 72% 16.8M 11s
370600K .......... .......... .......... .......... .......... 72% 13.9M 11s
370650K .......... .......... .......... .......... .......... 72% 16.6M 11s
370700K .......... .......... .......... .......... .......... 72% 12.5M 11s
370750K .......... .......... .......... .......... .......... 72% 16.4M 11s
370800K .......... .......... .......... .......... .......... 72% 24.8M 11s
370850K .......... .......... .......... .......... .......... 72% 13.5M 11s
370900K .......... .......... .......... .......... .......... 72% 16.5M 11s
370950K .......... .......... .......... .......... .......... 72% 10.9M 11s
371000K .......... .......... .......... .......... .......... 72% 17.1M 11s
371050K .......... .......... .......... .......... .......... 72% 14.2M 11s
371100K .......... .......... .......... .......... .......... 72% 7.01M 11s
371150K .......... .......... .......... .......... .......... 73% 17.2M 11s
371200K .......... .......... .......... .......... .......... 73% 15.7M 11s
371250K .......... .......... .......... .......... .......... 73% 15.2M 11s
371300K .......... .......... .......... .......... .......... 73% 16.3M 11s
371350K .......... .......... .......... .......... .......... 73% 11.1M 11s
371400K .......... .......... .......... .......... .......... 73% 17.5M 11s
371450K .......... .......... .......... .......... .......... 73% 19.4M 11s
371500K .......... .......... .......... .......... .......... 73% 39.1M 11s
371550K .......... .......... .......... .......... .......... 73% 26.7M 11s
371600K .......... .......... .......... .......... .......... 73% 24.5M 11s
371650K .......... .......... .......... .......... .......... 73% 45.2M 11s
371700K .......... .......... .......... .......... .......... 73% 15.9M 11s
371750K .......... .......... .......... .......... .......... 73% 18.7M 11s
371800K .......... .......... .......... .......... .......... 73% 15.7M 11s
371850K .......... .......... .......... .......... .......... 73% 15.0M 11s
371900K .......... .......... .......... .......... .......... 73% 16.5M 11s
371950K .......... .......... .......... .......... .......... 73% 17.2M 11s
372000K .......... .......... .......... .......... .......... 73% 17.8M 11s
372050K .......... .......... .......... .......... .......... 73% 14.8M 11s
372100K .......... .......... .......... .......... .......... 73% 9.53M 11s
372150K .......... .......... .......... .......... .......... 73% 15.2M 11s
372200K .......... .......... .......... .......... .......... 73% 14.1M 11s
372250K .......... .......... .......... .......... .......... 73% 11.5M 11s
372300K .......... .......... .......... .......... .......... 73% 14.1M 11s
372350K .......... .......... .......... .......... .......... 73% 13.8M 11s
372400K .......... .......... .......... .......... .......... 73% 14.2M 11s
372450K .......... .......... .......... .......... .......... 73% 19.1M 11s
372500K .......... .......... .......... .......... .......... 73% 15.8M 11s
372550K .......... .......... .......... .......... .......... 73% 20.5M 11s
372600K .......... .......... .......... .......... .......... 73% 39.4M 11s
372650K .......... .......... .......... .......... .......... 73% 15.3M 11s
372700K .......... .......... .......... .......... .......... 73% 21.8M 11s
372750K .......... .......... .......... .......... .......... 73% 19.7M 11s
372800K .......... .......... .......... .......... .......... 73% 19.2M 11s
372850K .......... .......... .......... .......... .......... 73% 19.8M 11s
372900K .......... .......... .......... .......... .......... 73% 19.5M 11s
372950K .......... .......... .......... .......... .......... 73% 19.3M 11s
373000K .......... .......... .......... .......... .......... 73% 23.7M 11s
373050K .......... .......... .......... .......... .......... 73% 25.4M 11s
373100K .......... .......... .......... .......... .......... 73% 13.0M 11s
373150K .......... .......... .......... .......... .......... 73% 18.7M 11s
373200K .......... .......... .......... .......... .......... 73% 25.2M 11s
373250K .......... .......... .......... .......... .......... 73% 23.2M 11s
373300K .......... .......... .......... .......... .......... 73% 16.6M 11s
373350K .......... .......... .......... .......... .......... 73% 13.2M 11s
373400K .......... .......... .......... .......... .......... 73%  131M 11s
373450K .......... .......... .......... .......... .......... 73% 25.5M 11s
373500K .......... .......... .......... .......... .......... 73% 44.9M 11s
373550K .......... .......... .......... .......... .......... 73% 31.1M 11s
373600K .......... .......... .......... .......... .......... 73% 18.9M 11s
373650K .......... .......... .......... .......... .......... 73% 40.1M 11s
373700K .......... .......... .......... .......... .......... 73% 22.9M 11s
373750K .......... .......... .......... .......... .......... 73% 44.5M 11s
373800K .......... .......... .......... .......... .......... 73% 19.8M 11s
373850K .......... .......... .......... .......... .......... 73% 40.6M 11s
373900K .......... .......... .......... .......... .......... 73% 27.8M 11s
373950K .......... .......... .......... .......... .......... 73% 34.1M 11s
374000K .......... .......... .......... .......... .......... 73% 21.0M 11s
374050K .......... .......... .......... .......... .......... 73% 32.1M 11s
374100K .......... .......... .......... .......... .......... 73% 28.4M 11s
374150K .......... .......... .......... .......... .......... 73% 36.4M 11s
374200K .......... .......... .......... .......... .......... 73% 22.1M 11s
374250K .......... .......... .......... .......... .......... 73% 36.0M 11s
374300K .......... .......... .......... .......... .......... 73% 25.2M 11s
374350K .......... .......... .......... .......... .......... 73% 27.0M 11s
374400K .......... .......... .......... .......... .......... 73% 30.3M 11s
374450K .......... .......... .......... .......... .......... 73% 33.1M 11s
374500K .......... .......... .......... .......... .......... 73% 22.2M 11s
374550K .......... .......... .......... .......... .......... 73% 31.2M 11s
374600K .......... .......... .......... .......... .......... 73% 26.8M 11s
374650K .......... .......... .......... .......... .......... 73% 34.8M 11s
374700K .......... .......... .......... .......... .......... 73% 24.0M 11s
374750K .......... .......... .......... .......... .......... 73% 15.7M 11s
374800K .......... .......... .......... .......... .......... 73%  131M 11s
374850K .......... .......... .......... .......... .......... 73% 17.9M 11s
374900K .......... .......... .......... .......... .......... 73% 89.8M 11s
374950K .......... .......... .......... .......... .......... 73% 19.8M 11s
375000K .......... .......... .......... .......... .......... 73% 63.1M 11s
375050K .......... .......... .......... .......... .......... 73% 23.7M 11s
375100K .......... .......... .......... .......... .......... 73% 37.6M 11s
375150K .......... .......... .......... .......... .......... 73% 27.8M 11s
375200K .......... .......... .......... .......... .......... 73% 15.6M 11s
375250K .......... .......... .......... .......... .......... 73% 25.5M 11s
375300K .......... .......... .......... .......... .......... 73% 39.1M 11s
375350K .......... .......... .......... .......... .......... 73% 26.6M 11s
375400K .......... .......... .......... .......... .......... 73% 40.8M 11s
375450K .......... .......... .......... .......... .......... 73% 19.5M 11s
375500K .......... .......... .......... .......... .......... 73% 37.7M 11s
375550K .......... .......... .......... .......... .......... 73% 28.0M 11s
375600K .......... .......... .......... .......... .......... 73% 31.7M 11s
375650K .......... .......... .......... .......... .......... 73% 33.7M 11s
375700K .......... .......... .......... .......... .......... 73% 21.9M 10s
375750K .......... .......... .......... .......... .......... 73% 38.0M 10s
375800K .......... .......... .......... .......... .......... 73% 26.5M 10s
375850K .......... .......... .......... .......... .......... 73% 34.7M 10s
375900K .......... .......... .......... .......... .......... 73% 25.8M 10s
375950K .......... .......... .......... .......... .......... 73% 34.6M 10s
376000K .......... .......... .......... .......... .......... 73% 19.3M 10s
376050K .......... .......... .......... .......... .......... 73% 22.7M 10s
376100K .......... .......... .......... .......... .......... 73% 27.7M 10s
376150K .......... .......... .......... .......... .......... 73% 63.8M 10s
376200K .......... .......... .......... .......... .......... 74% 16.9M 10s
376250K .......... .......... .......... .......... .......... 74%  100M 10s
376300K .......... .......... .......... .......... .......... 74% 48.9M 10s
376350K .......... .......... .......... .......... .......... 74% 35.1M 10s
376400K .......... .......... .......... .......... .......... 74% 91.3M 10s
376450K .......... .......... .......... .......... .......... 74% 27.4M 10s
376500K .......... .......... .......... .......... .......... 74% 76.3M 10s
376550K .......... .......... .......... .......... .......... 74% 20.2M 10s
376600K .......... .......... .......... .......... .......... 74% 28.8M 10s
376650K .......... .......... .......... .......... .......... 74% 19.6M 10s
376700K .......... .......... .......... .......... .......... 74% 22.8M 10s
376750K .......... .......... .......... .......... .......... 74% 22.2M 10s
376800K .......... .......... .......... .......... .......... 74% 21.5M 10s
376850K .......... .......... .......... .......... .......... 74% 21.4M 10s
376900K .......... .......... .......... .......... .......... 74% 19.3M 10s
376950K .......... .......... .......... .......... .......... 74% 17.7M 10s
377000K .......... .......... .......... .......... .......... 74% 22.8M 10s
377050K .......... .......... .......... .......... .......... 74% 24.2M 10s
377100K .......... .......... .......... .......... .......... 74% 17.7M 10s
377150K .......... .......... .......... .......... .......... 74% 25.8M 10s
377200K .......... .......... .......... .......... .......... 74% 21.4M 10s
377250K .......... .......... .......... .......... .......... 74% 20.0M 10s
377300K .......... .......... .......... .......... .......... 74% 20.8M 10s
377350K .......... .......... .......... .......... .......... 74% 34.4M 10s
377400K .......... .......... .......... .......... .......... 74% 16.5M 10s
377450K .......... .......... .......... .......... .......... 74% 36.1M 10s
377500K .......... .......... .......... .......... .......... 74%  128M 10s
377550K .......... .......... .......... .......... .......... 74% 42.3M 10s
377600K .......... .......... .......... .......... .......... 74% 25.3M 10s
377650K .......... .......... .......... .......... .......... 74% 28.6M 10s
377700K .......... .......... .......... .......... .......... 74% 20.6M 10s
377750K .......... .......... .......... .......... .......... 74% 22.2M 10s
377800K .......... .......... .......... .......... .......... 74% 27.8M 10s
377850K .......... .......... .......... .......... .......... 74% 27.1M 10s
377900K .......... .......... .......... .......... .......... 74% 26.7M 10s
377950K .......... .......... .......... .......... .......... 74% 21.0M 10s
378000K .......... .......... .......... .......... .......... 74% 21.5M 10s
378050K .......... .......... .......... .......... .......... 74% 42.2M 10s
378100K .......... .......... .......... .......... .......... 74% 25.5M 10s
378150K .......... .......... .......... .......... .......... 74% 23.5M 10s
378200K .......... .......... .......... .......... .......... 74% 21.9M 10s
378250K .......... .......... .......... .......... .......... 74% 13.4M 10s
378300K .......... .......... .......... .......... .......... 74% 40.7M 10s
378350K .......... .......... .......... .......... .......... 74% 19.0M 10s
378400K .......... .......... .......... .......... .......... 74% 21.0M 10s
378450K .......... .......... .......... .......... .......... 74% 31.7M 10s
378500K .......... .......... .......... .......... .......... 74% 29.8M 10s
378550K .......... .......... .......... .......... .......... 74% 98.8M 10s
378600K .......... .......... .......... .......... .......... 74% 24.6M 10s
378650K .......... .......... .......... .......... .......... 74% 18.8M 10s
378700K .......... .......... .......... .......... .......... 74% 99.9M 10s
378750K .......... .......... .......... .......... .......... 74%  256M 10s
378800K .......... .......... .......... .......... .......... 74% 23.7M 10s
378850K .......... .......... .......... .......... .......... 74% 39.0M 10s
378900K .......... .......... .......... .......... .......... 74% 79.9M 10s
378950K .......... .......... .......... .......... .......... 74% 38.1M 10s
379000K .......... .......... .......... .......... .......... 74% 30.2M 10s
379050K .......... .......... .......... .......... .......... 74% 52.7M 10s
379100K .......... .......... .......... .......... .......... 74% 24.8M 10s
379150K .......... .......... .......... .......... .......... 74% 40.9M 10s
379200K .......... .......... .......... .......... .......... 74% 23.6M 10s
379250K .......... .......... .......... .......... .......... 74% 27.7M 10s
379300K .......... .......... .......... .......... .......... 74% 60.4M 10s
379350K .......... .......... .......... .......... .......... 74% 19.8M 10s
379400K .......... .......... .......... .......... .......... 74% 31.2M 10s
379450K .......... .......... .......... .......... .......... 74% 34.8M 10s
379500K .......... .......... .......... .......... .......... 74% 44.0M 10s
379550K .......... .......... .......... .......... .......... 74% 25.1M 10s
379600K .......... .......... .......... .......... .......... 74% 30.8M 10s
379650K .......... .......... .......... .......... .......... 74% 36.0M 10s
379700K .......... .......... .......... .......... .......... 74% 31.0M 10s
379750K .......... .......... .......... .......... .......... 74% 29.6M 10s
379800K .......... .......... .......... .......... .......... 74% 41.2M 10s
379850K .......... .......... .......... .......... .......... 74% 30.6M 10s
379900K .......... .......... .......... .......... .......... 74% 35.0M 10s
379950K .......... .......... .......... .......... .......... 74% 34.5M 10s
380000K .......... .......... .......... .......... .......... 74% 37.5M 10s
380050K .......... .......... .......... .......... .......... 74% 45.4M 10s
380100K .......... .......... .......... .......... .......... 74% 23.8M 10s
380150K .......... .......... .......... .......... .......... 74% 28.8M 10s
380200K .......... .......... .......... .......... .......... 74% 72.2M 10s
380250K .......... .......... .......... .......... .......... 74% 16.4M 10s
380300K .......... .......... .......... .......... .......... 74% 24.1M 10s
380350K .......... .......... .......... .......... .......... 74% 67.1M 10s
380400K .......... .......... .......... .......... .......... 74%  178M 10s
380450K .......... .......... .......... .......... .......... 74% 19.7M 10s
380500K .......... .......... .......... .......... .......... 74%  171M 10s
380550K .......... .......... .......... .......... .......... 74% 36.5M 10s
380600K .......... .......... .......... .......... .......... 74% 62.4M 10s
380650K .......... .......... .......... .......... .......... 74% 25.5M 10s
380700K .......... .......... .......... .......... .......... 74% 24.0M 10s
380750K .......... .......... .......... .......... .......... 74% 26.2M 10s
380800K .......... .......... .......... .......... .......... 74% 38.6M 10s
380850K .......... .......... .......... .......... .......... 74% 23.0M 10s
380900K .......... .......... .......... .......... .......... 74% 27.0M 10s
380950K .......... .......... .......... .......... .......... 74% 28.7M 10s
381000K .......... .......... .......... .......... .......... 74% 22.6M 10s
381050K .......... .......... .......... .......... .......... 74% 30.3M 10s
381100K .......... .......... .......... .......... .......... 74% 23.6M 10s
381150K .......... .......... .......... .......... .......... 74% 22.8M 10s
381200K .......... .......... .......... .......... .......... 74% 24.4M 10s
381250K .......... .......... .......... .......... .......... 74% 46.6M 10s
381300K .......... .......... .......... .......... .......... 75% 18.0M 10s
381350K .......... .......... .......... .......... .......... 75% 24.3M 10s
381400K .......... .......... .......... .......... .......... 75% 22.0M 10s
381450K .......... .......... .......... .......... .......... 75% 23.6M 10s
381500K .......... .......... .......... .......... .......... 75% 33.4M 10s
381550K .......... .......... .......... .......... .......... 75% 35.4M 10s
381600K .......... .......... .......... .......... .......... 75% 24.2M 10s
381650K .......... .......... .......... .......... .......... 75% 22.6M 10s
381700K .......... .......... .......... .......... .......... 75% 38.4M 10s
381750K .......... .......... .......... .......... .......... 75% 23.4M 10s
381800K .......... .......... .......... .......... .......... 75%  181M 10s
381850K .......... .......... .......... .......... .......... 75% 24.8M 10s
381900K .......... .......... .......... .......... .......... 75% 26.6M 10s
381950K .......... .......... .......... .......... .......... 75% 21.6M 10s
382000K .......... .......... .......... .......... .......... 75% 27.4M 10s
382050K .......... .......... .......... .......... .......... 75% 43.1M 10s
382100K .......... .......... .......... .......... .......... 75% 20.7M 10s
382150K .......... .......... .......... .......... .......... 75% 23.6M 10s
382200K .......... .......... .......... .......... .......... 75% 34.0M 10s
382250K .......... .......... .......... .......... .......... 75% 22.1M 10s
382300K .......... .......... .......... .......... .......... 75% 25.5M 10s
382350K .......... .......... .......... .......... .......... 75% 24.7M 10s
382400K .......... .......... .......... .......... .......... 75% 26.2M 10s
382450K .......... .......... .......... .......... .......... 75% 24.3M 10s
382500K .......... .......... .......... .......... .......... 75% 26.5M 10s
382550K .......... .......... .......... .......... .......... 75% 26.7M 10s
382600K .......... .......... .......... .......... .......... 75% 31.9M 10s
382650K .......... .......... .......... .......... .......... 75% 24.7M 10s
382700K .......... .......... .......... .......... .......... 75% 22.8M 10s
382750K .......... .......... .......... .......... .......... 75% 45.1M 10s
382800K .......... .......... .......... .......... .......... 75% 38.7M 10s
382850K .......... .......... .......... .......... .......... 75% 12.8M 10s
382900K .......... .......... .......... .......... .......... 75% 71.5M 10s
382950K .......... .......... .......... .......... .......... 75% 22.5M 10s
383000K .......... .......... .......... .......... .......... 75% 26.8M 10s
383050K .......... .......... .......... .......... .......... 75%  107M 10s
383100K .......... .......... .......... .......... .......... 75% 19.5M 10s
383150K .......... .......... .......... .......... .......... 75% 21.5M 10s
383200K .......... .......... .......... .......... .......... 75% 22.1M 10s
383250K .......... .......... .......... .......... .......... 75% 14.5M 10s
383300K .......... .......... .......... .......... .......... 75% 16.3M 10s
383350K .......... .......... .......... .......... .......... 75% 9.72M 10s
383400K .......... .......... .......... .......... .......... 75% 22.1M 10s
383450K .......... .......... .......... .......... .......... 75% 13.6M 10s
383500K .......... .......... .......... .......... .......... 75% 22.1M 10s
383550K .......... .......... .......... .......... .......... 75% 15.7M 10s
383600K .......... .......... .......... .......... .......... 75% 15.6M 10s
383650K .......... .......... .......... .......... .......... 75% 15.5M 10s
383700K .......... .......... .......... .......... .......... 75% 15.6M 10s
383750K .......... .......... .......... .......... .......... 75% 15.3M 10s
383800K .......... .......... .......... .......... .......... 75% 18.3M 10s
383850K .......... .......... .......... .......... .......... 75% 21.0M 10s
383900K .......... .......... .......... .......... .......... 75% 42.8M 10s
383950K .......... .......... .......... .......... .......... 75% 16.9M 10s
384000K .......... .......... .......... .......... .......... 75% 53.1M 10s
384050K .......... .......... .......... .......... .......... 75% 27.9M 10s
384100K .......... .......... .......... .......... .......... 75% 76.9M 10s
384150K .......... .......... .......... .......... .......... 75% 20.9M 10s
384200K .......... .......... .......... .......... .......... 75% 15.5M 10s
384250K .......... .......... .......... .......... .......... 75% 33.5M 10s
384300K .......... .......... .......... .......... .......... 75% 19.2M 10s
384350K .......... .......... .......... .......... .......... 75% 16.7M 10s
384400K .......... .......... .......... .......... .......... 75% 12.6M 10s
384450K .......... .......... .......... .......... .......... 75% 20.8M 10s
384500K .......... .......... .......... .......... .......... 75% 17.0M 10s
384550K .......... .......... .......... .......... .......... 75% 20.1M 10s
384600K .......... .......... .......... .......... .......... 75% 15.5M 10s
384650K .......... .......... .......... .......... .......... 75% 20.1M 10s
384700K .......... .......... .......... .......... .......... 75% 15.7M 10s
384750K .......... .......... .......... .......... .......... 75% 25.7M 10s
384800K .......... .......... .......... .......... .......... 75% 17.0M 10s
384850K .......... .......... .......... .......... .......... 75% 16.5M 10s
384900K .......... .......... .......... .......... .......... 75% 18.0M 10s
384950K .......... .......... .......... .......... .......... 75% 13.6M 10s
385000K .......... .......... .......... .......... .......... 75% 14.6M 10s
385050K .......... .......... .......... .......... .......... 75% 37.5M 10s
385100K .......... .......... .......... .......... .......... 75% 19.7M 10s
385150K .......... .......... .......... .......... .......... 75% 36.4M 10s
385200K .......... .......... .......... .......... .......... 75% 21.0M 10s
385250K .......... .......... .......... .......... .......... 75% 32.7M 10s
385300K .......... .......... .......... .......... .......... 75% 27.6M 10s
385350K .......... .......... .......... .......... .......... 75% 14.4M 10s
385400K .......... .......... .......... .......... .......... 75% 24.5M 10s
385450K .......... .......... .......... .......... .......... 75% 19.3M 10s
385500K .......... .......... .......... .......... .......... 75% 27.4M 10s
385550K .......... .......... .......... .......... .......... 75% 18.6M 10s
385600K .......... .......... .......... .......... .......... 75% 17.8M 10s
385650K .......... .......... .......... .......... .......... 75% 23.1M 10s
385700K .......... .......... .......... .......... .......... 75% 20.2M 10s
385750K .......... .......... .......... .......... .......... 75% 18.8M 10s
385800K .......... .......... .......... .......... .......... 75% 25.0M 10s
385850K .......... .......... .......... .......... .......... 75% 16.9M 10s
385900K .......... .......... .......... .......... .......... 75% 17.9M 10s
385950K .......... .......... .......... .......... .......... 75% 11.9M 10s
386000K .......... .......... .......... .......... .......... 75% 20.3M 10s
386050K .......... .......... .......... .......... .......... 75% 19.9M 10s
386100K .......... .......... .......... .......... .......... 75% 20.3M 10s
386150K .......... .......... .......... .......... .......... 75% 45.5M 10s
386200K .......... .......... .......... .......... .......... 75% 22.7M 10s
386250K .......... .......... .......... .......... .......... 75% 38.2M 10s
386300K .......... .......... .......... .......... .......... 75% 35.7M 10s
386350K .......... .......... .......... .......... .......... 75% 21.7M 10s
386400K .......... .......... .......... .......... .......... 76% 35.6M 10s
386450K .......... .......... .......... .......... .......... 76% 5.04M 10s
386500K .......... .......... .......... .......... .......... 76% 35.1M 10s
386550K .......... .......... .......... .......... .......... 76% 20.3M 10s
386600K .......... .......... .......... .......... .......... 76% 44.7M 10s
386650K .......... .......... .......... .......... .......... 76% 24.3M 9s
386700K .......... .......... .......... .......... .......... 76% 27.2M 9s
386750K .......... .......... .......... .......... .......... 76% 30.1M 9s
386800K .......... .......... .......... .......... .......... 76% 25.2M 9s
386850K .......... .......... .......... .......... .......... 76% 22.1M 9s
386900K .......... .......... .......... .......... .......... 76% 42.3M 9s
386950K .......... .......... .......... .......... .......... 76% 18.8M 9s
387000K .......... .......... .......... .......... .......... 76% 35.5M 9s
387050K .......... .......... .......... .......... .......... 76% 37.1M 9s
387100K .......... .......... .......... .......... .......... 76% 40.4M 9s
387150K .......... .......... .......... .......... .......... 76% 20.8M 9s
387200K .......... .......... .......... .......... .......... 76% 21.9M 9s
387250K .......... .......... .......... .......... .......... 76% 24.1M 9s
387300K .......... .......... .......... .......... .......... 76% 25.0M 9s
387350K .......... .......... .......... .......... .......... 76% 18.0M 9s
387400K .......... .......... .......... .......... .......... 76% 20.2M 9s
387450K .......... .......... .......... .......... .......... 76% 13.0M 9s
387500K .......... .......... .......... .......... .......... 76% 20.4M 9s
387550K .......... .......... .......... .......... .......... 76% 20.7M 9s
387600K .......... .......... .......... .......... .......... 76% 14.6M 9s
387650K .......... .......... .......... .......... .......... 76% 22.4M 9s
387700K .......... .......... .......... .......... .......... 76% 19.5M 9s
387750K .......... .......... .......... .......... .......... 76% 17.2M 9s
387800K .......... .......... .......... .......... .......... 76% 17.2M 9s
387850K .......... .......... .......... .......... .......... 76% 15.9M 9s
387900K .......... .......... .......... .......... .......... 76% 14.7M 9s
387950K .......... .......... .......... .......... .......... 76% 11.8M 9s
388000K .......... .......... .......... .......... .......... 76% 27.0M 9s
388050K .......... .......... .......... .......... .......... 76% 46.3M 9s
388100K .......... .......... .......... .......... .......... 76% 25.3M 9s
388150K .......... .......... .......... .......... .......... 76% 25.2M 9s
388200K .......... .......... .......... .......... .......... 76% 12.2M 9s
388250K .......... .......... .......... .......... .......... 76% 20.9M 9s
388300K .......... .......... .......... .......... .......... 76% 13.6M 9s
388350K .......... .......... .......... .......... .......... 76% 14.0M 9s
388400K .......... .......... .......... .......... .......... 76% 15.6M 9s
388450K .......... .......... .......... .......... .......... 76% 13.0M 9s
388500K .......... .......... .......... .......... .......... 76% 12.8M 9s
388550K .......... .......... .......... .......... .......... 76% 14.6M 9s
388600K .......... .......... .......... .......... .......... 76% 10.6M 9s
388650K .......... .......... .......... .......... .......... 76% 14.3M 9s
388700K .......... .......... .......... .......... .......... 76% 23.9M 9s
388750K .......... .......... .......... .......... .......... 76% 13.1M 9s
388800K .......... .......... .......... .......... .......... 76% 19.4M 9s
388850K .......... .......... .......... .......... .......... 76% 27.6M 9s
388900K .......... .......... .......... .......... .......... 76% 12.5M 9s
388950K .......... .......... .......... .......... .......... 76% 22.7M 9s
389000K .......... .......... .......... .......... .......... 76% 18.2M 9s
389050K .......... .......... .......... .......... .......... 76% 14.1M 9s
389100K .......... .......... .......... .......... .......... 76% 16.7M 9s
389150K .......... .......... .......... .......... .......... 76% 12.3M 9s
389200K .......... .......... .......... .......... .......... 76% 12.8M 9s
389250K .......... .......... .......... .......... .......... 76% 13.0M 9s
389300K .......... .......... .......... .......... .......... 76% 13.3M 9s
389350K .......... .......... .......... .......... .......... 76% 11.4M 9s
389400K .......... .......... .......... .......... .......... 76% 12.6M 9s
389450K .......... .......... .......... .......... .......... 76% 12.3M 9s
389500K .......... .......... .......... .......... .......... 76% 13.4M 9s
389550K .......... .......... .......... .......... .......... 76% 6.92M 9s
389600K .......... .......... .......... .......... .......... 76% 8.57M 9s
389650K .......... .......... .......... .......... .......... 76% 15.2M 9s
389700K .......... .......... .......... .......... .......... 76% 9.99M 9s
389750K .......... .......... .......... .......... .......... 76% 14.0M 9s
389800K .......... .......... .......... .......... .......... 76% 14.4M 9s
389850K .......... .......... .......... .......... .......... 76% 10.4M 9s
389900K .......... .......... .......... .......... .......... 76% 13.2M 9s
389950K .......... .......... .......... .......... .......... 76% 11.0M 9s
390000K .......... .......... .......... .......... .......... 76% 12.0M 9s
390050K .......... .......... .......... .......... .......... 76% 38.3M 9s
390100K .......... .......... .......... .......... .......... 76% 27.9M 9s
390150K .......... .......... .......... .......... .......... 76% 13.9M 9s
390200K .......... .......... .......... .......... .......... 76%  116M 9s
390250K .......... .......... .......... .......... .......... 76% 18.3M 9s
390300K .......... .......... .......... .......... .......... 76% 15.3M 9s
390350K .......... .......... .......... .......... .......... 76% 17.1M 9s
390400K .......... .......... .......... .......... .......... 76% 17.3M 9s
390450K .......... .......... .......... .......... .......... 76% 16.5M 9s
390500K .......... .......... .......... .......... .......... 76% 19.7M 9s
390550K .......... .......... .......... .......... .......... 76% 21.5M 9s
390600K .......... .......... .......... .......... .......... 76% 16.2M 9s
390650K .......... .......... .......... .......... .......... 76% 15.0M 9s
390700K .......... .......... .......... .......... .......... 76% 15.5M 9s
390750K .......... .......... .......... .......... .......... 76% 23.3M 9s
390800K .......... .......... .......... .......... .......... 76% 16.8M 9s
390850K .......... .......... .......... .......... .......... 76% 13.8M 9s
390900K .......... .......... .......... .......... .......... 76% 22.8M 9s
390950K .......... .......... .......... .......... .......... 76% 18.0M 9s
391000K .......... .......... .......... .......... .......... 76% 16.2M 9s
391050K .......... .......... .......... .......... .......... 76% 23.0M 9s
391100K .......... .......... .......... .......... .......... 76% 25.5M 9s
391150K .......... .......... .......... .......... .......... 76% 29.6M 9s
391200K .......... .......... .......... .......... .......... 76% 16.1M 9s
391250K .......... .......... .......... .......... .......... 76% 38.1M 9s
391300K .......... .......... .......... .......... .......... 76% 63.1M 9s
391350K .......... .......... .......... .......... .......... 76% 22.7M 9s
391400K .......... .......... .......... .......... .......... 76% 30.5M 9s
391450K .......... .......... .......... .......... .......... 77% 24.4M 9s
391500K .......... .......... .......... .......... .......... 77% 26.9M 9s
391550K .......... .......... .......... .......... .......... 77% 26.5M 9s
391600K .......... .......... .......... .......... .......... 77% 22.4M 9s
391650K .......... .......... .......... .......... .......... 77% 22.6M 9s
391700K .......... .......... .......... .......... .......... 77% 21.9M 9s
391750K .......... .......... .......... .......... .......... 77% 33.9M 9s
391800K .......... .......... .......... .......... .......... 77% 20.9M 9s
391850K .......... .......... .......... .......... .......... 77% 21.6M 9s
391900K .......... .......... .......... .......... .......... 77% 24.0M 9s
391950K .......... .......... .......... .......... .......... 77% 21.0M 9s
392000K .......... .......... .......... .......... .......... 77% 27.6M 9s
392050K .......... .......... .......... .......... .......... 77% 18.5M 9s
392100K .......... .......... .......... .......... .......... 77% 16.7M 9s
392150K .......... .......... .......... .......... .......... 77% 17.1M 9s
392200K .......... .......... .......... .......... .......... 77% 6.96M 9s
392250K .......... .......... .......... .......... .......... 77% 10.5M 9s
392300K .......... .......... .......... .......... .......... 77% 10.3M 9s
392350K .......... .......... .......... .......... .......... 77% 12.3M 9s
392400K .......... .......... .......... .......... .......... 77% 9.66M 9s
392450K .......... .......... .......... .......... .......... 77% 10.7M 9s
392500K .......... .......... .......... .......... .......... 77% 9.21M 9s
392550K .......... .......... .......... .......... .......... 77% 11.3M 9s
392600K .......... .......... .......... .......... .......... 77% 9.42M 9s
392650K .......... .......... .......... .......... .......... 77% 41.3M 9s
392700K .......... .......... .......... .......... .......... 77% 27.9M 9s
392750K .......... .......... .......... .......... .......... 77% 33.4M 9s
392800K .......... .......... .......... .......... .......... 77% 16.7M 9s
392850K .......... .......... .......... .......... .......... 77%  115M 9s
392900K .......... .......... .......... .......... .......... 77% 24.0M 9s
392950K .......... .......... .......... .......... .......... 77% 14.5M 9s
393000K .......... .......... .......... .......... .......... 77% 83.2M 9s
393050K .......... .......... .......... .......... .......... 77% 23.4M 9s
393100K .......... .......... .......... .......... .......... 77% 19.6M 9s
393150K .......... .......... .......... .......... .......... 77% 20.8M 9s
393200K .......... .......... .......... .......... .......... 77% 22.2M 9s
393250K .......... .......... .......... .......... .......... 77% 21.5M 9s
393300K .......... .......... .......... .......... .......... 77% 20.9M 9s
393350K .......... .......... .......... .......... .......... 77% 20.8M 9s
393400K .......... .......... .......... .......... .......... 77% 26.6M 9s
393450K .......... .......... .......... .......... .......... 77% 17.1M 9s
393500K .......... .......... .......... .......... .......... 77% 17.8M 9s
393550K .......... .......... .......... .......... .......... 77% 21.8M 9s
393600K .......... .......... .......... .......... .......... 77% 11.4M 9s
393650K .......... .......... .......... .......... .......... 77% 14.2M 9s
393700K .......... .......... .......... .......... .......... 77% 14.3M 9s
393750K .......... .......... .......... .......... .......... 77% 14.2M 9s
393800K .......... .......... .......... .......... .......... 77% 15.8M 9s
393850K .......... .......... .......... .......... .......... 77% 15.1M 9s
393900K .......... .......... .......... .......... .......... 77% 9.15M 9s
393950K .......... .......... .......... .......... .......... 77% 7.28M 9s
394000K .......... .......... .......... .......... .......... 77% 10.1M 9s
394050K .......... .......... .......... .......... .......... 77% 11.7M 9s
394100K .......... .......... .......... .......... .......... 77% 10.2M 9s
394150K .......... .......... .......... .......... .......... 77% 16.2M 9s
394200K .......... .......... .......... .......... .......... 77% 12.3M 9s
394250K .......... .......... .......... .......... .......... 77% 12.1M 9s
394300K .......... .......... .......... .......... .......... 77% 16.9M 9s
394350K .......... .......... .......... .......... .......... 77% 12.6M 9s
394400K .......... .......... .......... .......... .......... 77% 29.9M 9s
394450K .......... .......... .......... .......... .......... 77% 38.6M 9s
394500K .......... .......... .......... .......... .......... 77% 33.5M 9s
394550K .......... .......... .......... .......... .......... 77% 89.1M 9s
394600K .......... .......... .......... .......... .......... 77% 21.0M 9s
394650K .......... .......... .......... .......... .......... 77%  166M 9s
394700K .......... .......... .......... .......... .......... 77% 44.2M 9s
394750K .......... .......... .......... .......... .......... 77% 30.9M 9s
394800K .......... .......... .......... .......... .......... 77% 40.2M 9s
394850K .......... .......... .......... .......... .......... 77% 31.3M 9s
394900K .......... .......... .......... .......... .......... 77% 35.5M 9s
394950K .......... .......... .......... .......... .......... 77% 38.6M 9s
395000K .......... .......... .......... .......... .......... 77% 24.5M 9s
395050K .......... .......... .......... .......... .......... 77% 18.3M 9s
395100K .......... .......... .......... .......... .......... 77% 17.6M 9s
395150K .......... .......... .......... .......... .......... 77% 25.4M 9s
395200K .......... .......... .......... .......... .......... 77% 20.3M 9s
395250K .......... .......... .......... .......... .......... 77% 40.9M 9s
395300K .......... .......... .......... .......... .......... 77% 23.2M 9s
395350K .......... .......... .......... .......... .......... 77% 26.9M 9s
395400K .......... .......... .......... .......... .......... 77% 29.6M 9s
395450K .......... .......... .......... .......... .......... 77% 25.2M 9s
395500K .......... .......... .......... .......... .......... 77% 32.3M 9s
395550K .......... .......... .......... .......... .......... 77% 27.4M 9s
395600K .......... .......... .......... .......... .......... 77% 22.0M 9s
395650K .......... .......... .......... .......... .......... 77% 27.4M 9s
395700K .......... .......... .......... .......... .......... 77% 37.9M 9s
395750K .......... .......... .......... .......... .......... 77% 22.6M 9s
395800K .......... .......... .......... .......... .......... 77% 30.9M 9s
395850K .......... .......... .......... .......... .......... 77% 25.4M 9s
395900K .......... .......... .......... .......... .......... 77% 27.2M 9s
395950K .......... .......... .......... .......... .......... 77% 19.5M 9s
396000K .......... .......... .......... .......... .......... 77% 42.8M 9s
396050K .......... .......... .......... .......... .......... 77% 45.9M 9s
396100K .......... .......... .......... .......... .......... 77% 69.7M 9s
396150K .......... .......... .......... .......... .......... 77% 19.3M 9s
396200K .......... .......... .......... .......... .......... 77% 75.1M 9s
396250K .......... .......... .......... .......... .......... 77%  182M 9s
396300K .......... .......... .......... .......... .......... 77% 36.7M 9s
396350K .......... .......... .......... .......... .......... 77% 35.0M 9s
396400K .......... .......... .......... .......... .......... 77% 36.5M 9s
396450K .......... .......... .......... .......... .......... 77% 36.8M 9s
396500K .......... .......... .......... .......... .......... 77% 24.2M 9s
396550K .......... .......... .......... .......... .......... 78% 22.5M 9s
396600K .......... .......... .......... .......... .......... 78% 19.1M 9s
396650K .......... .......... .......... .......... .......... 78% 36.4M 9s
396700K .......... .......... .......... .......... .......... 78% 18.1M 9s
396750K .......... .......... .......... .......... .......... 78% 22.4M 9s
396800K .......... .......... .......... .......... .......... 78% 23.0M 9s
396850K .......... .......... .......... .......... .......... 78% 23.6M 9s
396900K .......... .......... .......... .......... .......... 78% 23.5M 9s
396950K .......... .......... .......... .......... .......... 78% 21.1M 9s
397000K .......... .......... .......... .......... .......... 78% 27.1M 9s
397050K .......... .......... .......... .......... .......... 78% 23.4M 9s
397100K .......... .......... .......... .......... .......... 78% 14.3M 9s
397150K .......... .......... .......... .......... .......... 78% 25.8M 9s
397200K .......... .......... .......... .......... .......... 78% 30.5M 9s
397250K .......... .......... .......... .......... .......... 78% 27.6M 9s
397300K .......... .......... .......... .......... .......... 78% 12.6M 9s
397350K .......... .......... .......... .......... .......... 78%  170M 9s
397400K .......... .......... .......... .......... .......... 78% 20.4M 9s
397450K .......... .......... .......... .......... .......... 78% 19.2M 9s
397500K .......... .......... .......... .......... .......... 78% 39.9M 9s
397550K .......... .......... .......... .......... .......... 78% 22.9M 9s
397600K .......... .......... .......... .......... .......... 78% 14.6M 9s
397650K .......... .......... .......... .......... .......... 78% 22.6M 9s
397700K .......... .......... .......... .......... .......... 78% 17.6M 9s
397750K .......... .......... .......... .......... .......... 78% 18.2M 9s
397800K .......... .......... .......... .......... .......... 78% 20.0M 9s
397850K .......... .......... .......... .......... .......... 78% 16.0M 9s
397900K .......... .......... .......... .......... .......... 78% 18.5M 9s
397950K .......... .......... .......... .......... .......... 78% 16.1M 9s
398000K .......... .......... .......... .......... .......... 78% 23.8M 9s
398050K .......... .......... .......... .......... .......... 78% 18.2M 9s
398100K .......... .......... .......... .......... .......... 78% 18.7M 9s
398150K .......... .......... .......... .......... .......... 78% 11.0M 9s
398200K .......... .......... .......... .......... .......... 78% 24.7M 9s
398250K .......... .......... .......... .......... .......... 78% 20.3M 9s
398300K .......... .......... .......... .......... .......... 78% 12.9M 9s
398350K .......... .......... .......... .......... .......... 78%  123M 9s
398400K .......... .......... .......... .......... .......... 78% 13.3M 8s
398450K .......... .......... .......... .......... .......... 78% 51.1M 8s
398500K .......... .......... .......... .......... .......... 78% 45.7M 8s
398550K .......... .......... .......... .......... .......... 78% 19.9M 8s
398600K .......... .......... .......... .......... .......... 78% 14.7M 8s
398650K .......... .......... .......... .......... .......... 78% 18.0M 8s
398700K .......... .......... .......... .......... .......... 78% 20.2M 8s
398750K .......... .......... .......... .......... .......... 78% 17.6M 8s
398800K .......... .......... .......... .......... .......... 78% 20.0M 8s
398850K .......... .......... .......... .......... .......... 78% 18.0M 8s
398900K .......... .......... .......... .......... .......... 78% 17.4M 8s
398950K .......... .......... .......... .......... .......... 78% 17.6M 8s
399000K .......... .......... .......... .......... .......... 78% 17.5M 8s
399050K .......... .......... .......... .......... .......... 78% 20.9M 8s
399100K .......... .......... .......... .......... .......... 78% 15.9M 8s
399150K .......... .......... .......... .......... .......... 78% 21.5M 8s
399200K .......... .......... .......... .......... .......... 78% 15.2M 8s
399250K .......... .......... .......... .......... .......... 78% 15.0M 8s
399300K .......... .......... .......... .......... .......... 78% 11.9M 8s
399350K .......... .......... .......... .......... .......... 78% 8.82M 8s
399400K .......... .......... .......... .......... .......... 78% 11.6M 8s
399450K .......... .......... .......... .......... .......... 78% 9.45M 8s
399500K .......... .......... .......... .......... .......... 78% 11.1M 8s
399550K .......... .......... .......... .......... .......... 78% 11.0M 8s
399600K .......... .......... .......... .......... .......... 78% 7.75M 8s
399650K .......... .......... .......... .......... .......... 78% 11.6M 8s
399700K .......... .......... .......... .......... .......... 78% 13.7M 8s
399750K .......... .......... .......... .......... .......... 78% 15.7M 8s
399800K .......... .......... .......... .......... .......... 78% 20.7M 8s
399850K .......... .......... .......... .......... .......... 78% 11.2M 8s
399900K .......... .......... .......... .......... .......... 78% 10.6M 8s
399950K .......... .......... .......... .......... .......... 78% 11.4M 8s
400000K .......... .......... .......... .......... .......... 78% 12.5M 8s
400050K .......... .......... .......... .......... .......... 78% 14.8M 8s
400100K .......... .......... .......... .......... .......... 78% 9.33M 8s
400150K .......... .......... .......... .......... .......... 78% 15.1M 8s
400200K .......... .......... .......... .......... .......... 78% 9.52M 8s
400250K .......... .......... .......... .......... .......... 78% 11.9M 8s
400300K .......... .......... .......... .......... .......... 78% 12.3M 8s
400350K .......... .......... .......... .......... .......... 78% 15.3M 8s
400400K .......... .......... .......... .......... .......... 78% 15.0M 8s
400450K .......... .......... .......... .......... .......... 78% 19.0M 8s
400500K .......... .......... .......... .......... .......... 78% 18.7M 8s
400550K .......... .......... .......... .......... .......... 78% 17.6M 8s
400600K .......... .......... .......... .......... .......... 78% 18.9M 8s
400650K .......... .......... .......... .......... .......... 78% 24.3M 8s
400700K .......... .......... .......... .......... .......... 78% 20.6M 8s
400750K .......... .......... .......... .......... .......... 78% 23.4M 8s
400800K .......... .......... .......... .......... .......... 78% 19.7M 8s
400850K .......... .......... .......... .......... .......... 78% 19.3M 8s
400900K .......... .......... .......... .......... .......... 78% 18.7M 8s
400950K .......... .......... .......... .......... .......... 78% 13.8M 8s
401000K .......... .......... .......... .......... .......... 78% 26.5M 8s
401050K .......... .......... .......... .......... .......... 78% 25.2M 8s
401100K .......... .......... .......... .......... .......... 78% 15.0M 8s
401150K .......... .......... .......... .......... .......... 78% 12.3M 8s
401200K .......... .......... .......... .......... .......... 78% 9.39M 8s
401250K .......... .......... .......... .......... .......... 78% 21.5M 8s
401300K .......... .......... .......... .......... .......... 78% 14.0M 8s
401350K .......... .......... .......... .......... .......... 78% 9.39M 8s
401400K .......... .......... .......... .......... .......... 78% 11.0M 8s
401450K .......... .......... .......... .......... .......... 78% 7.44M 8s
401500K .......... .......... .......... .......... .......... 78% 9.24M 8s
401550K .......... .......... .......... .......... .......... 78% 8.99M 8s
401600K .......... .......... .......... .......... .......... 78% 7.62M 8s
401650K .......... .......... .......... .......... .......... 79% 10.5M 8s
401700K .......... .......... .......... .......... .......... 79% 6.52M 8s
401750K .......... .......... .......... .......... .......... 79% 15.3M 8s
401800K .......... .......... .......... .......... .......... 79% 38.0M 8s
401850K .......... .......... .......... .......... .......... 79% 22.9M 8s
401900K .......... .......... .......... .......... .......... 79% 35.1M 8s
401950K .......... .......... .......... .......... .......... 79% 30.0M 8s
402000K .......... .......... .......... .......... .......... 79% 21.5M 8s
402050K .......... .......... .......... .......... .......... 79% 35.7M 8s
402100K .......... .......... .......... .......... .......... 79% 24.1M 8s
402150K .......... .......... .......... .......... .......... 79% 28.0M 8s
402200K .......... .......... .......... .......... .......... 79% 27.3M 8s
402250K .......... .......... .......... .......... .......... 79% 29.1M 8s
402300K .......... .......... .......... .......... .......... 79% 29.7M 8s
402350K .......... .......... .......... .......... .......... 79% 25.6M 8s
402400K .......... .......... .......... .......... .......... 79% 37.3M 8s
402450K .......... .......... .......... .......... .......... 79% 23.2M 8s
402500K .......... .......... .......... .......... .......... 79% 31.5M 8s
402550K .......... .......... .......... .......... .......... 79% 22.7M 8s
402600K .......... .......... .......... .......... .......... 79% 26.4M 8s
402650K .......... .......... .......... .......... .......... 79% 21.7M 8s
402700K .......... .......... .......... .......... .......... 79% 21.3M 8s
402750K .......... .......... .......... .......... .......... 79% 13.4M 8s
402800K .......... .......... .......... .......... .......... 79% 14.9M 8s
402850K .......... .......... .......... .......... .......... 79% 11.7M 8s
402900K .......... .......... .......... .......... .......... 79% 15.7M 8s
402950K .......... .......... .......... .......... .......... 79% 13.0M 8s
403000K .......... .......... .......... .......... .......... 79% 12.5M 8s
403050K .......... .......... .......... .......... .......... 79% 16.1M 8s
403100K .......... .......... .......... .......... .......... 79% 11.7M 8s
403150K .......... .......... .......... .......... .......... 79% 12.0M 8s
403200K .......... .......... .......... .......... .......... 79% 11.9M 8s
403250K .......... .......... .......... .......... .......... 79% 13.7M 8s
403300K .......... .......... .......... .......... .......... 79% 14.9M 8s
403350K .......... .......... .......... .......... .......... 79% 10.4M 8s
403400K .......... .......... .......... .......... .......... 79% 25.2M 8s
403450K .......... .......... .......... .......... .......... 79% 13.5M 8s
403500K .......... .......... .......... .......... .......... 79% 20.8M 8s
403550K .......... .......... .......... .......... .......... 79% 16.8M 8s
403600K .......... .......... .......... .......... .......... 79% 10.7M 8s
403650K .......... .......... .......... .......... .......... 79% 10.2M 8s
403700K .......... .......... .......... .......... .......... 79% 18.3M 8s
403750K .......... .......... .......... .......... .......... 79% 16.0M 8s
403800K .......... .......... .......... .......... .......... 79% 17.7M 8s
403850K .......... .......... .......... .......... .......... 79% 11.2M 8s
403900K .......... .......... .......... .......... .......... 79% 15.3M 8s
403950K .......... .......... .......... .......... .......... 79% 15.1M 8s
404000K .......... .......... .......... .......... .......... 79% 19.3M 8s
404050K .......... .......... .......... .......... .......... 79% 16.9M 8s
404100K .......... .......... .......... .......... .......... 79% 12.8M 8s
404150K .......... .......... .......... .......... .......... 79% 15.6M 8s
404200K .......... .......... .......... .......... .......... 79% 13.4M 8s
404250K .......... .......... .......... .......... .......... 79% 9.08M 8s
404300K .......... .......... .......... .......... .......... 79% 14.8M 8s
404350K .......... .......... .......... .......... .......... 79% 11.9M 8s
404400K .......... .......... .......... .......... .......... 79% 12.4M 8s
404450K .......... .......... .......... .......... .......... 79% 12.3M 8s
404500K .......... .......... .......... .......... .......... 79% 11.7M 8s
404550K .......... .......... .......... .......... .......... 79% 11.7M 8s
404600K .......... .......... .......... .......... .......... 79% 12.2M 8s
404650K .......... .......... .......... .......... .......... 79% 12.3M 8s
404700K .......... .......... .......... .......... .......... 79% 15.1M 8s
404750K .......... .......... .......... .......... .......... 79% 32.9M 8s
404800K .......... .......... .......... .......... .......... 79% 29.4M 8s
404850K .......... .......... .......... .......... .......... 79% 10.8M 8s
404900K .......... .......... .......... .......... .......... 79% 21.8M 8s
404950K .......... .......... .......... .......... .......... 79% 15.4M 8s
405000K .......... .......... .......... .......... .......... 79% 15.4M 8s
405050K .......... .......... .......... .......... .......... 79% 19.5M 8s
405100K .......... .......... .......... .......... .......... 79% 13.4M 8s
405150K .......... .......... .......... .......... .......... 79% 16.5M 8s
405200K .......... .......... .......... .......... .......... 79% 14.9M 8s
405250K .......... .......... .......... .......... .......... 79% 13.9M 8s
405300K .......... .......... .......... .......... .......... 79% 12.6M 8s
405350K .......... .......... .......... .......... .......... 79% 18.2M 8s
405400K .......... .......... .......... .......... .......... 79% 14.0M 8s
405450K .......... .......... .......... .......... .......... 79% 15.6M 8s
405500K .......... .......... .......... .......... .......... 79% 14.2M 8s
405550K .......... .......... .......... .......... .......... 79% 11.2M 8s
405600K .......... .......... .......... .......... .......... 79% 11.1M 8s
405650K .......... .......... .......... .......... .......... 79% 10.4M 8s
405700K .......... .......... .......... .......... .......... 79% 8.37M 8s
405750K .......... .......... .......... .......... .......... 79% 11.3M 8s
405800K .......... .......... .......... .......... .......... 79% 13.4M 8s
405850K .......... .......... .......... .......... .......... 79% 8.48M 8s
405900K .......... .......... .......... .......... .......... 79% 8.06M 8s
405950K .......... .......... .......... .......... .......... 79% 5.04M 8s
406000K .......... .......... .......... .......... .......... 79% 9.22M 8s
406050K .......... .......... .......... .......... .......... 79% 13.0M 8s
406100K .......... .......... .......... .......... .......... 79% 12.6M 8s
406150K .......... .......... .......... .......... .......... 79% 11.3M 8s
406200K .......... .......... .......... .......... .......... 79% 11.2M 8s
406250K .......... .......... .......... .......... .......... 79% 9.74M 8s
406300K .......... .......... .......... .......... .......... 79% 13.1M 8s
406350K .......... .......... .......... .......... .......... 79% 10.5M 8s
406400K .......... .......... .......... .......... .......... 79% 15.0M 8s
406450K .......... .......... .......... .......... .......... 79% 21.3M 8s
406500K .......... .......... .......... .......... .......... 79% 20.4M 8s
406550K .......... .......... .......... .......... .......... 79% 27.7M 8s
406600K .......... .......... .......... .......... .......... 79% 14.1M 8s
406650K .......... .......... .......... .......... .......... 79% 21.7M 8s
406700K .......... .......... .......... .......... .......... 80% 14.2M 8s
406750K .......... .......... .......... .......... .......... 80% 20.9M 8s
406800K .......... .......... .......... .......... .......... 80% 22.1M 8s
406850K .......... .......... .......... .......... .......... 80% 14.5M 8s
406900K .......... .......... .......... .......... .......... 80% 20.0M 8s
406950K .......... .......... .......... .......... .......... 80% 20.0M 8s
407000K .......... .......... .......... .......... .......... 80% 19.9M 8s
407050K .......... .......... .......... .......... .......... 80% 20.6M 8s
407100K .......... .......... .......... .......... .......... 80% 17.1M 8s
407150K .......... .......... .......... .......... .......... 80% 17.3M 8s
407200K .......... .......... .......... .......... .......... 80% 19.1M 8s
407250K .......... .......... .......... .......... .......... 80% 18.3M 8s
407300K .......... .......... .......... .......... .......... 80% 19.6M 8s
407350K .......... .......... .......... .......... .......... 80% 99.9M 8s
407400K .......... .......... .......... .......... .......... 80%  215M 8s
407450K .......... .......... .......... .......... .......... 80% 35.1M 8s
407500K .......... .......... .......... .......... .......... 80% 35.1M 8s
407550K .......... .......... .......... .......... .......... 80% 26.5M 8s
407600K .......... .......... .......... .......... .......... 80% 25.7M 8s
407650K .......... .......... .......... .......... .......... 80% 48.1M 8s
407700K .......... .......... .......... .......... .......... 80% 14.8M 8s
407750K .......... .......... .......... .......... .......... 80%  111M 8s
407800K .......... .......... .......... .......... .......... 80% 19.9M 8s
407850K .......... .......... .......... .......... .......... 80% 16.7M 8s
407900K .......... .......... .......... .......... .......... 80% 16.2M 8s
407950K .......... .......... .......... .......... .......... 80% 12.1M 8s
408000K .......... .......... .......... .......... .......... 80% 16.2M 8s
408050K .......... .......... .......... .......... .......... 80% 18.9M 8s
408100K .......... .......... .......... .......... .......... 80% 11.8M 8s
408150K .......... .......... .......... .......... .......... 80% 13.4M 8s
408200K .......... .......... .......... .......... .......... 80% 14.8M 8s
408250K .......... .......... .......... .......... .......... 80% 15.2M 8s
408300K .......... .......... .......... .......... .......... 80% 15.6M 8s
408350K .......... .......... .......... .......... .......... 80% 13.9M 8s
408400K .......... .......... .......... .......... .......... 80% 15.8M 8s
408450K .......... .......... .......... .......... .......... 80% 13.8M 8s
408500K .......... .......... .......... .......... .......... 80% 16.1M 8s
408550K .......... .......... .......... .......... .......... 80% 15.4M 8s
408600K .......... .......... .......... .......... .......... 80% 13.6M 8s
408650K .......... .......... .......... .......... .......... 80% 16.5M 8s
408700K .......... .......... .......... .......... .......... 80% 15.0M 8s
408750K .......... .......... .......... .......... .......... 80% 17.7M 8s
408800K .......... .......... .......... .......... .......... 80% 7.83M 8s
408850K .......... .......... .......... .......... .......... 80% 23.2M 8s
408900K .......... .......... .......... .......... .......... 80% 9.63M 8s
408950K .......... .......... .......... .......... .......... 80% 12.6M 8s
409000K .......... .......... .......... .......... .......... 80% 13.1M 8s
409050K .......... .......... .......... .......... .......... 80% 9.90M 8s
409100K .......... .......... .......... .......... .......... 80% 10.7M 8s
409150K .......... .......... .......... .......... .......... 80% 12.9M 8s
409200K .......... .......... .......... .......... .......... 80% 11.0M 8s
409250K .......... .......... .......... .......... .......... 80% 14.3M 8s
409300K .......... .......... .......... .......... .......... 80% 11.4M 8s
409350K .......... .......... .......... .......... .......... 80% 15.2M 8s
409400K .......... .......... .......... .......... .......... 80% 17.9M 8s
409450K .......... .......... .......... .......... .......... 80% 21.3M 8s
409500K .......... .......... .......... .......... .......... 80% 20.4M 8s
409550K .......... .......... .......... .......... .......... 80% 23.3M 8s
409600K .......... .......... .......... .......... .......... 80% 19.7M 8s
409650K .......... .......... .......... .......... .......... 80% 18.0M 8s
409700K .......... .......... .......... .......... .......... 80% 19.9M 8s
409750K .......... .......... .......... .......... .......... 80% 18.8M 8s
409800K .......... .......... .......... .......... .......... 80% 19.1M 8s
409850K .......... .......... .......... .......... .......... 80% 16.0M 8s
409900K .......... .......... .......... .......... .......... 80% 20.9M 8s
409950K .......... .......... .......... .......... .......... 80% 19.9M 8s
410000K .......... .......... .......... .......... .......... 80% 16.7M 8s
410050K .......... .......... .......... .......... .......... 80% 25.0M 8s
410100K .......... .......... .......... .......... .......... 80% 18.0M 8s
410150K .......... .......... .......... .......... .......... 80% 19.1M 8s
410200K .......... .......... .......... .......... .......... 80% 16.4M 8s
410250K .......... .......... .......... .......... .......... 80% 20.7M 8s
410300K .......... .......... .......... .......... .......... 80% 19.1M 8s
410350K .......... .......... .......... .......... .......... 80% 12.4M 8s
410400K .......... .......... .......... .......... .......... 80% 18.0M 8s
410450K .......... .......... .......... .......... .......... 80% 18.7M 8s
410500K .......... .......... .......... .......... .......... 80% 34.8M 8s
410550K .......... .......... .......... .......... .......... 80% 30.0M 8s
410600K .......... .......... .......... .......... .......... 80% 15.2M 8s
410650K .......... .......... .......... .......... .......... 80% 20.2M 8s
410700K .......... .......... .......... .......... .......... 80% 15.4M 8s
410750K .......... .......... .......... .......... .......... 80% 18.6M 8s
410800K .......... .......... .......... .......... .......... 80% 23.1M 8s
410850K .......... .......... .......... .......... .......... 80% 19.5M 7s
410900K .......... .......... .......... .......... .......... 80% 18.6M 7s
410950K .......... .......... .......... .......... .......... 80% 17.6M 7s
411000K .......... .......... .......... .......... .......... 80% 21.0M 7s
411050K .......... .......... .......... .......... .......... 80% 22.5M 7s
411100K .......... .......... .......... .......... .......... 80% 14.3M 7s
411150K .......... .......... .......... .......... .......... 80% 22.9M 7s
411200K .......... .......... .......... .......... .......... 80% 16.4M 7s
411250K .......... .......... .......... .......... .......... 80% 35.0M 7s
411300K .......... .......... .......... .......... .......... 80% 38.9M 7s
411350K .......... .......... .......... .......... .......... 80% 16.2M 7s
411400K .......... .......... .......... .......... .......... 80% 64.8M 7s
411450K .......... .......... .......... .......... .......... 80% 22.4M 7s
411500K .......... .......... .......... .......... .......... 80% 37.8M 7s
411550K .......... .......... .......... .......... .......... 80% 37.0M 7s
411600K .......... .......... .......... .......... .......... 80% 20.7M 7s
411650K .......... .......... .......... .......... .......... 80% 16.1M 7s
411700K .......... .......... .......... .......... .......... 80% 21.1M 7s
411750K .......... .......... .......... .......... .......... 80% 19.5M 7s
411800K .......... .......... .......... .......... .......... 81% 20.1M 7s
411850K .......... .......... .......... .......... .......... 81% 18.9M 7s
411900K .......... .......... .......... .......... .......... 81% 19.1M 7s
411950K .......... .......... .......... .......... .......... 81% 17.8M 7s
412000K .......... .......... .......... .......... .......... 81% 21.5M 7s
412050K .......... .......... .......... .......... .......... 81% 10.1M 7s
412100K .......... .......... .......... .......... .......... 81% 14.4M 7s
412150K .......... .......... .......... .......... .......... 81% 23.4M 7s
412200K .......... .......... .......... .......... .......... 81% 18.3M 7s
412250K .......... .......... .......... .......... .......... 81% 17.9M 7s
412300K .......... .......... .......... .......... .......... 81% 11.5M 7s
412350K .......... .......... .......... .......... .......... 81% 29.1M 7s
412400K .......... .......... .......... .......... .......... 81% 14.9M 7s
412450K .......... .......... .......... .......... .......... 81% 14.5M 7s
412500K .......... .......... .......... .......... .......... 81% 12.8M 7s
412550K .......... .......... .......... .......... .......... 81% 15.2M 7s
412600K .......... .......... .......... .......... .......... 81% 11.5M 7s
412650K .......... .......... .......... .......... .......... 81% 14.3M 7s
412700K .......... .......... .......... .......... .......... 81% 11.7M 7s
412750K .......... .......... .......... .......... .......... 81% 14.0M 7s
412800K .......... .......... .......... .......... .......... 81% 15.5M 7s
412850K .......... .......... .......... .......... .......... 81% 12.0M 7s
412900K .......... .......... .......... .......... .......... 81% 11.5M 7s
412950K .......... .......... .......... .......... .......... 81% 9.69M 7s
413000K .......... .......... .......... .......... .......... 81%  237M 7s
413050K .......... .......... .......... .......... .......... 81% 13.5M 7s
413100K .......... .......... .......... .......... .......... 81% 12.8M 7s
413150K .......... .......... .......... .......... .......... 81% 15.2M 7s
413200K .......... .......... .......... .......... .......... 81% 15.1M 7s
413250K .......... .......... .......... .......... .......... 81% 23.0M 7s
413300K .......... .......... .......... .......... .......... 81% 14.7M 7s
413350K .......... .......... .......... .......... .......... 81% 15.7M 7s
413400K .......... .......... .......... .......... .......... 81% 14.9M 7s
413450K .......... .......... .......... .......... .......... 81% 12.8M 7s
413500K .......... .......... .......... .......... .......... 81% 20.4M 7s
413550K .......... .......... .......... .......... .......... 81% 12.6M 7s
413600K .......... .......... .......... .......... .......... 81% 13.2M 7s
413650K .......... .......... .......... .......... .......... 81% 20.7M 7s
413700K .......... .......... .......... .......... .......... 81% 22.3M 7s
413750K .......... .......... .......... .......... .......... 81% 12.6M 7s
413800K .......... .......... .......... .......... .......... 81%  124M 7s
413850K .......... .......... .......... .......... .......... 81% 15.9M 7s
413900K .......... .......... .......... .......... .......... 81% 29.6M 7s
413950K .......... .......... .......... .......... .......... 81% 18.3M 7s
414000K .......... .......... .......... .......... .......... 81% 18.6M 7s
414050K .......... .......... .......... .......... .......... 81% 19.0M 7s
414100K .......... .......... .......... .......... .......... 81% 15.0M 7s
414150K .......... .......... .......... .......... .......... 81% 23.6M 7s
414200K .......... .......... .......... .......... .......... 81% 19.3M 7s
414250K .......... .......... .......... .......... .......... 81% 21.4M 7s
414300K .......... .......... .......... .......... .......... 81% 22.4M 7s
414350K .......... .......... .......... .......... .......... 81% 14.9M 7s
414400K .......... .......... .......... .......... .......... 81% 23.5M 7s
414450K .......... .......... .......... .......... .......... 81% 21.5M 7s
414500K .......... .......... .......... .......... .......... 81% 17.9M 7s
414550K .......... .......... .......... .......... .......... 81% 18.0M 7s
414600K .......... .......... .......... .......... .......... 81% 20.1M 7s
414650K .......... .......... .......... .......... .......... 81% 19.4M 7s
414700K .......... .......... .......... .......... .......... 81% 31.6M 7s
414750K .......... .......... .......... .......... .......... 81%  133M 7s
414800K .......... .......... .......... .......... .......... 81% 18.0M 7s
414850K .......... .......... .......... .......... .......... 81%  115M 7s
414900K .......... .......... .......... .......... .......... 81% 30.9M 7s
414950K .......... .......... .......... .......... .......... 81% 24.3M 7s
415000K .......... .......... .......... .......... .......... 81% 18.2M 7s
415050K .......... .......... .......... .......... .......... 81% 15.4M 7s
415100K .......... .......... .......... .......... .......... 81% 15.6M 7s
415150K .......... .......... .......... .......... .......... 81% 23.3M 7s
415200K .......... .......... .......... .......... .......... 81% 15.1M 7s
415250K .......... .......... .......... .......... .......... 81% 20.7M 7s
415300K .......... .......... .......... .......... .......... 81% 17.2M 7s
415350K .......... .......... .......... .......... .......... 81% 16.0M 7s
415400K .......... .......... .......... .......... .......... 81% 17.2M 7s
415450K .......... .......... .......... .......... .......... 81% 18.7M 7s
415500K .......... .......... .......... .......... .......... 81% 20.0M 7s
415550K .......... .......... .......... .......... .......... 81% 19.7M 7s
415600K .......... .......... .......... .......... .......... 81% 14.9M 7s
415650K .......... .......... .......... .......... .......... 81% 21.1M 7s
415700K .......... .......... .......... .......... .......... 81% 36.1M 7s
415750K .......... .......... .......... .......... .......... 81% 20.8M 7s
415800K .......... .......... .......... .......... .......... 81% 41.1M 7s
415850K .......... .......... .......... .......... .......... 81% 58.8M 7s
415900K .......... .......... .......... .......... .......... 81% 27.5M 7s
415950K .......... .......... .......... .......... .......... 81% 34.3M 7s
416000K .......... .......... .......... .......... .......... 81% 25.2M 7s
416050K .......... .......... .......... .......... .......... 81% 33.7M 7s
416100K .......... .......... .......... .......... .......... 81% 34.1M 7s
416150K .......... .......... .......... .......... .......... 81% 31.3M 7s
416200K .......... .......... .......... .......... .......... 81% 27.6M 7s
416250K .......... .......... .......... .......... .......... 81% 32.5M 7s
416300K .......... .......... .......... .......... .......... 81% 45.8M 7s
416350K .......... .......... .......... .......... .......... 81% 24.5M 7s
416400K .......... .......... .......... .......... .......... 81% 39.3M 7s
416450K .......... .......... .......... .......... .......... 81% 27.2M 7s
416500K .......... .......... .......... .......... .......... 81% 33.3M 7s
416550K .......... .......... .......... .......... .......... 81% 38.9M 7s
416600K .......... .......... .......... .......... .......... 81% 22.7M 7s
416650K .......... .......... .......... .......... .......... 81% 20.6M 7s
416700K .......... .......... .......... .......... .......... 81% 27.7M 7s
416750K .......... .......... .......... .......... .......... 81% 19.5M 7s
416800K .......... .......... .......... .......... .......... 81% 27.5M 7s
416850K .......... .......... .......... .......... .......... 81% 20.8M 7s
416900K .......... .......... .......... .......... .......... 82% 19.2M 7s
416950K .......... .......... .......... .......... .......... 82% 19.8M 7s
417000K .......... .......... .......... .......... .......... 82% 20.7M 7s
417050K .......... .......... .......... .......... .......... 82% 19.2M 7s
417100K .......... .......... .......... .......... .......... 82% 17.0M 7s
417150K .......... .......... .......... .......... .......... 82% 23.0M 7s
417200K .......... .......... .......... .......... .......... 82% 17.6M 7s
417250K .......... .......... .......... .......... .......... 82% 24.0M 7s
417300K .......... .......... .......... .......... .......... 82% 40.0M 7s
417350K .......... .......... .......... .......... .......... 82% 15.4M 7s
417400K .......... .......... .......... .......... .......... 82% 21.5M 7s
417450K .......... .......... .......... .......... .......... 82% 20.0M 7s
417500K .......... .......... .......... .......... .......... 82% 26.3M 7s
417550K .......... .......... .......... .......... .......... 82% 33.1M 7s
417600K .......... .......... .......... .......... .......... 82% 40.6M 7s
417650K .......... .......... .......... .......... .......... 82% 46.1M 7s
417700K .......... .......... .......... .......... .......... 82% 26.7M 7s
417750K .......... .......... .......... .......... .......... 82% 49.0M 7s
417800K .......... .......... .......... .......... .......... 82% 49.8M 7s
417850K .......... .......... .......... .......... .......... 82% 95.2M 7s
417900K .......... .......... .......... .......... .......... 82% 35.0M 7s
417950K .......... .......... .......... .......... .......... 82% 62.7M 7s
418000K .......... .......... .......... .......... .......... 82% 40.5M 7s
418050K .......... .......... .......... .......... .......... 82% 26.6M 7s
418100K .......... .......... .......... .......... .......... 82% 40.0M 7s
418150K .......... .......... .......... .......... .......... 82% 31.7M 7s
418200K .......... .......... .......... .......... .......... 82% 17.2M 7s
418250K .......... .......... .......... .......... .......... 82% 27.0M 7s
418300K .......... .......... .......... .......... .......... 82% 43.3M 7s
418350K .......... .......... .......... .......... .......... 82% 25.1M 7s
418400K .......... .......... .......... .......... .......... 82% 33.8M 7s
418450K .......... .......... .......... .......... .......... 82% 24.2M 7s
418500K .......... .......... .......... .......... .......... 82% 36.6M 7s
418550K .......... .......... .......... .......... .......... 82% 36.7M 7s
418600K .......... .......... .......... .......... .......... 82% 23.7M 7s
418650K .......... .......... .......... .......... .......... 82% 39.3M 7s
418700K .......... .......... .......... .......... .......... 82% 28.2M 7s
418750K .......... .......... .......... .......... .......... 82% 49.4M 7s
418800K .......... .......... .......... .......... .......... 82% 26.8M 7s
418850K .......... .......... .......... .......... .......... 82% 33.7M 7s
418900K .......... .......... .......... .......... .......... 82% 34.6M 7s
418950K .......... .......... .......... .......... .......... 82% 24.5M 7s
419000K .......... .......... .......... .......... .......... 82% 36.7M 7s
419050K .......... .......... .......... .......... .......... 82% 31.4M 7s
419100K .......... .......... .......... .......... .......... 82% 24.1M 7s
419150K .......... .......... .......... .......... .......... 82% 23.7M 7s
419200K .......... .......... .......... .......... .......... 82% 32.6M 7s
419250K .......... .......... .......... .......... .......... 82% 42.7M 7s
419300K .......... .......... .......... .......... .......... 82% 23.1M 7s
419350K .......... .......... .......... .......... .......... 82% 29.8M 7s
419400K .......... .......... .......... .......... .......... 82% 15.8M 7s
419450K .......... .......... .......... .......... .......... 82% 29.5M 7s
419500K .......... .......... .......... .......... .......... 82% 17.7M 7s
419550K .......... .......... .......... .......... .......... 82% 35.1M 7s
419600K .......... .......... .......... .......... .......... 82% 18.4M 7s
419650K .......... .......... .......... .......... .......... 82% 16.3M 7s
419700K .......... .......... .......... .......... .......... 82% 16.8M 7s
419750K .......... .......... .......... .......... .......... 82% 16.9M 7s
419800K .......... .......... .......... .......... .......... 82% 18.1M 7s
419850K .......... .......... .......... .......... .......... 82% 17.2M 7s
419900K .......... .......... .......... .......... .......... 82% 15.0M 7s
419950K .......... .......... .......... .......... .......... 82% 13.1M 7s
420000K .......... .......... .......... .......... .......... 82% 7.44M 7s
420050K .......... .......... .......... .......... .......... 82% 8.67M 7s
420100K .......... .......... .......... .......... .......... 82% 14.1M 7s
420150K .......... .......... .......... .......... .......... 82% 39.8M 7s
420200K .......... .......... .......... .......... .......... 82% 35.7M 7s
420250K .......... .......... .......... .......... .......... 82% 35.7M 7s
420300K .......... .......... .......... .......... .......... 82% 20.6M 7s
420350K .......... .......... .......... .......... .......... 82%  170M 7s
420400K .......... .......... .......... .......... .......... 82% 46.8M 7s
420450K .......... .......... .......... .......... .......... 82% 42.5M 7s
420500K .......... .......... .......... .......... .......... 82% 31.3M 7s
420550K .......... .......... .......... .......... .......... 82% 23.7M 7s
420600K .......... .......... .......... .......... .......... 82% 23.9M 7s
420650K .......... .......... .......... .......... .......... 82% 25.2M 7s
420700K .......... .......... .......... .......... .......... 82% 18.0M 7s
420750K .......... .......... .......... .......... .......... 82% 26.2M 7s
420800K .......... .......... .......... .......... .......... 82% 25.3M 7s
420850K .......... .......... .......... .......... .......... 82% 24.7M 7s
420900K .......... .......... .......... .......... .......... 82% 24.8M 7s
420950K .......... .......... .......... .......... .......... 82% 24.5M 7s
421000K .......... .......... .......... .......... .......... 82% 28.0M 7s
421050K .......... .......... .......... .......... .......... 82% 26.2M 7s
421100K .......... .......... .......... .......... .......... 82% 19.5M 7s
421150K .......... .......... .......... .......... .......... 82% 24.5M 7s
421200K .......... .......... .......... .......... .......... 82% 18.2M 7s
421250K .......... .......... .......... .......... .......... 82% 16.0M 7s
421300K .......... .......... .......... .......... .......... 82% 17.1M 7s
421350K .......... .......... .......... .......... .......... 82% 38.9M 7s
421400K .......... .......... .......... .......... .......... 82% 27.4M 7s
421450K .......... .......... .......... .......... .......... 82% 21.7M 7s
421500K .......... .......... .......... .......... .......... 82% 27.4M 7s
421550K .......... .......... .......... .......... .......... 82% 33.5M 7s
421600K .......... .......... .......... .......... .......... 82% 21.8M 7s
421650K .......... .......... .......... .......... .......... 82% 25.2M 7s
421700K .......... .......... .......... .......... .......... 82% 22.1M 7s
421750K .......... .......... .......... .......... .......... 82% 31.2M 7s
421800K .......... .......... .......... .......... .......... 82% 21.5M 7s
421850K .......... .......... .......... .......... .......... 82% 33.5M 7s
421900K .......... .......... .......... .......... .......... 82% 23.3M 7s
421950K .......... .......... .......... .......... .......... 83% 20.0M 7s
422000K .......... .......... .......... .......... .......... 83% 32.3M 7s
422050K .......... .......... .......... .......... .......... 83% 26.4M 7s
422100K .......... .......... .......... .......... .......... 83% 30.2M 7s
422150K .......... .......... .......... .......... .......... 83% 25.5M 7s
422200K .......... .......... .......... .......... .......... 83% 22.2M 7s
422250K .......... .......... .......... .......... .......... 83% 37.9M 7s
422300K .......... .......... .......... .......... .......... 83% 93.4M 7s
422350K .......... .......... .......... .......... .......... 83% 22.9M 7s
422400K .......... .......... .......... .......... .......... 83% 20.7M 7s
422450K .......... .......... .......... .......... .......... 83% 29.2M 7s
422500K .......... .......... .......... .......... .......... 83% 34.2M 7s
422550K .......... .......... .......... .......... .......... 83% 43.6M 7s
422600K .......... .......... .......... .......... .......... 83% 29.0M 7s
422650K .......... .......... .......... .......... .......... 83% 41.0M 7s
422700K .......... .......... .......... .......... .......... 83% 28.9M 7s
422750K .......... .......... .......... .......... .......... 83% 33.1M 7s
422800K .......... .......... .......... .......... .......... 83% 26.6M 7s
422850K .......... .......... .......... .......... .......... 83% 26.5M 6s
422900K .......... .......... .......... .......... .......... 83% 47.5M 6s
422950K .......... .......... .......... .......... .......... 83% 26.5M 6s
423000K .......... .......... .......... .......... .......... 83% 40.8M 6s
423050K .......... .......... .......... .......... .......... 83% 23.5M 6s
423100K .......... .......... .......... .......... .......... 83% 30.5M 6s
423150K .......... .......... .......... .......... .......... 83% 24.2M 6s
423200K .......... .......... .......... .......... .......... 83% 30.1M 6s
423250K .......... .......... .......... .......... .......... 83% 25.7M 6s
423300K .......... .......... .......... .......... .......... 83% 43.7M 6s
423350K .......... .......... .......... .......... .......... 83% 25.8M 6s
423400K .......... .......... .......... .......... .......... 83% 37.4M 6s
423450K .......... .......... .......... .......... .......... 83% 24.4M 6s
423500K .......... .......... .......... .......... .......... 83% 32.9M 6s
423550K .......... .......... .......... .......... .......... 83% 30.8M 6s
423600K .......... .......... .......... .......... .......... 83% 23.8M 6s
423650K .......... .......... .......... .......... .......... 83%  109M 6s
423700K .......... .......... .......... .......... .......... 83% 37.0M 6s
423750K .......... .......... .......... .......... .......... 83% 24.3M 6s
423800K .......... .......... .......... .......... .......... 83% 38.8M 6s
423850K .......... .......... .......... .......... .......... 83% 37.0M 6s
423900K .......... .......... .......... .......... .......... 83% 85.7M 6s
423950K .......... .......... .......... .......... .......... 83% 19.3M 6s
424000K .......... .......... .......... .......... .......... 83%  224M 6s
424050K .......... .......... .......... .......... .......... 83%  217M 6s
424100K .......... .......... .......... .......... .......... 83% 15.0M 6s
424150K .......... .......... .......... .......... .......... 83% 82.9M 6s
424200K .......... .......... .......... .......... .......... 83% 18.5M 6s
424250K .......... .......... .......... .......... .......... 83% 24.5M 6s
424300K .......... .......... .......... .......... .......... 83% 18.7M 6s
424350K .......... .......... .......... .......... .......... 83% 11.7M 6s
424400K .......... .......... .......... .......... .......... 83% 17.6M 6s
424450K .......... .......... .......... .......... .......... 83% 21.9M 6s
424500K .......... .......... .......... .......... .......... 83% 21.4M 6s
424550K .......... .......... .......... .......... .......... 83% 15.2M 6s
424600K .......... .......... .......... .......... .......... 83% 21.8M 6s
424650K .......... .......... .......... .......... .......... 83% 18.9M 6s
424700K .......... .......... .......... .......... .......... 83% 19.9M 6s
424750K .......... .......... .......... .......... .......... 83% 19.2M 6s
424800K .......... .......... .......... .......... .......... 83% 12.9M 6s
424850K .......... .......... .......... .......... .......... 83% 9.73M 6s
424900K .......... .......... .......... .......... .......... 83% 10.3M 6s
424950K .......... .......... .......... .......... .......... 83% 33.1M 6s
425000K .......... .......... .......... .......... .......... 83% 15.6M 6s
425050K .......... .......... .......... .......... .......... 83% 13.1M 6s
425100K .......... .......... .......... .......... .......... 83% 10.3M 6s
425150K .......... .......... .......... .......... .......... 83% 14.5M 6s
425200K .......... .......... .......... .......... .......... 83% 11.2M 6s
425250K .......... .......... .......... .......... .......... 83% 12.8M 6s
425300K .......... .......... .......... .......... .......... 83% 18.1M 6s
425350K .......... .......... .......... .......... .......... 83% 10.8M 6s
425400K .......... .......... .......... .......... .......... 83% 16.4M 6s
425450K .......... .......... .......... .......... .......... 83% 12.0M 6s
425500K .......... .......... .......... .......... .......... 83% 11.3M 6s
425550K .......... .......... .......... .......... .......... 83% 12.5M 6s
425600K .......... .......... .......... .......... .......... 83% 27.1M 6s
425650K .......... .......... .......... .......... .......... 83% 14.1M 6s
425700K .......... .......... .......... .......... .......... 83% 11.0M 6s
425750K .......... .......... .......... .......... .......... 83% 12.5M 6s
425800K .......... .......... .......... .......... .......... 83% 15.3M 6s
425850K .......... .......... .......... .......... .......... 83% 14.2M 6s
425900K .......... .......... .......... .......... .......... 83% 13.7M 6s
425950K .......... .......... .......... .......... .......... 83% 11.8M 6s
426000K .......... .......... .......... .......... .......... 83% 15.5M 6s
426050K .......... .......... .......... .......... .......... 83% 13.9M 6s
426100K .......... .......... .......... .......... .......... 83% 12.3M 6s
426150K .......... .......... .......... .......... .......... 83% 15.3M 6s
426200K .......... .......... .......... .......... .......... 83% 11.4M 6s
426250K .......... .......... .......... .......... .......... 83% 29.9M 6s
426300K .......... .......... .......... .......... .......... 83% 24.7M 6s
426350K .......... .......... .......... .......... .......... 83% 19.7M 6s
426400K .......... .......... .......... .......... .......... 83% 13.5M 6s
426450K .......... .......... .......... .......... .......... 83% 21.7M 6s
426500K .......... .......... .......... .......... .......... 83% 23.1M 6s
426550K .......... .......... .......... .......... .......... 83% 20.5M 6s
426600K .......... .......... .......... .......... .......... 83% 22.1M 6s
426650K .......... .......... .......... .......... .......... 83% 21.2M 6s
426700K .......... .......... .......... .......... .......... 83% 18.4M 6s
426750K .......... .......... .......... .......... .......... 83% 16.4M 6s
426800K .......... .......... .......... .......... .......... 83% 24.4M 6s
426850K .......... .......... .......... .......... .......... 83% 18.8M 6s
426900K .......... .......... .......... .......... .......... 83% 18.2M 6s
426950K .......... .......... .......... .......... .......... 83% 10.8M 6s
427000K .......... .......... .......... .......... .......... 83% 37.1M 6s
427050K .......... .......... .......... .......... .......... 84% 11.5M 6s
427100K .......... .......... .......... .......... .......... 84% 7.76M 6s
427150K .......... .......... .......... .......... .......... 84% 55.7M 6s
427200K .......... .......... .......... .......... .......... 84% 13.7M 6s
427250K .......... .......... .......... .......... .......... 84% 23.3M 6s
427300K .......... .......... .......... .......... .......... 84% 14.9M 6s
427350K .......... .......... .......... .......... .......... 84% 16.0M 6s
427400K .......... .......... .......... .......... .......... 84% 16.4M 6s
427450K .......... .......... .......... .......... .......... 84% 15.4M 6s
427500K .......... .......... .......... .......... .......... 84% 21.5M 6s
427550K .......... .......... .......... .......... .......... 84% 21.9M 6s
427600K .......... .......... .......... .......... .......... 84% 12.6M 6s
427650K .......... .......... .......... .......... .......... 84% 18.0M 6s
427700K .......... .......... .......... .......... .......... 84% 14.8M 6s
427750K .......... .......... .......... .......... .......... 84% 18.4M 6s
427800K .......... .......... .......... .......... .......... 84% 25.0M 6s
427850K .......... .......... .......... .......... .......... 84% 30.9M 6s
427900K .......... .......... .......... .......... .......... 84% 46.1M 6s
427950K .......... .......... .......... .......... .......... 84% 19.2M 6s
428000K .......... .......... .......... .......... .......... 84% 21.7M 6s
428050K .......... .......... .......... .......... .......... 84% 22.4M 6s
428100K .......... .......... .......... .......... .......... 84% 21.0M 6s
428150K .......... .......... .......... .......... .......... 84% 22.8M 6s
428200K .......... .......... .......... .......... .......... 84% 16.0M 6s
428250K .......... .......... .......... .......... .......... 84% 26.0M 6s
428300K .......... .......... .......... .......... .......... 84% 24.9M 6s
428350K .......... .......... .......... .......... .......... 84% 18.0M 6s
428400K .......... .......... .......... .......... .......... 84% 21.9M 6s
428450K .......... .......... .......... .......... .......... 84% 17.2M 6s
428500K .......... .......... .......... .......... .......... 84% 24.3M 6s
428550K .......... .......... .......... .......... .......... 84% 24.2M 6s
428600K .......... .......... .......... .......... .......... 84% 18.9M 6s
428650K .......... .......... .......... .......... .......... 84% 18.0M 6s
428700K .......... .......... .......... .......... .......... 84% 31.2M 6s
428750K .......... .......... .......... .......... .......... 84% 26.3M 6s
428800K .......... .......... .......... .......... .......... 84% 74.2M 6s
428850K .......... .......... .......... .......... .......... 84% 17.7M 6s
428900K .......... .......... .......... .......... .......... 84% 36.0M 6s
428950K .......... .......... .......... .......... .......... 84% 41.1M 6s
429000K .......... .......... .......... .......... .......... 84% 33.5M 6s
429050K .......... .......... .......... .......... .......... 84% 29.9M 6s
429100K .......... .......... .......... .......... .......... 84% 16.9M 6s
429150K .......... .......... .......... .......... .......... 84% 30.3M 6s
429200K .......... .......... .......... .......... .......... 84% 19.2M 6s
429250K .......... .......... .......... .......... .......... 84% 28.9M 6s
429300K .......... .......... .......... .......... .......... 84% 24.4M 6s
429350K .......... .......... .......... .......... .......... 84% 16.8M 6s
429400K .......... .......... .......... .......... .......... 84% 30.2M 6s
429450K .......... .......... .......... .......... .......... 84% 20.0M 6s
429500K .......... .......... .......... .......... .......... 84% 29.7M 6s
429550K .......... .......... .......... .......... .......... 84% 23.7M 6s
429600K .......... .......... .......... .......... .......... 84% 21.0M 6s
429650K .......... .......... .......... .......... .......... 84% 21.3M 6s
429700K .......... .......... .......... .......... .......... 84% 21.0M 6s
429750K .......... .......... .......... .......... .......... 84% 23.1M 6s
429800K .......... .......... .......... .......... .......... 84% 24.1M 6s
429850K .......... .......... .......... .......... .......... 84% 26.1M 6s
429900K .......... .......... .......... .......... .......... 84% 25.5M 6s
429950K .......... .......... .......... .......... .......... 84% 15.2M 6s
430000K .......... .......... .......... .......... .......... 84% 55.6M 6s
430050K .......... .......... .......... .......... .......... 84% 26.7M 6s
430100K .......... .......... .......... .......... .......... 84% 16.5M 6s
430150K .......... .......... .......... .......... .......... 84% 43.0M 6s
430200K .......... .......... .......... .......... .......... 84% 53.7M 6s
430250K .......... .......... .......... .......... .......... 84% 22.6M 6s
430300K .......... .......... .......... .......... .......... 84% 16.2M 6s
430350K .......... .......... .......... .......... .......... 84% 23.3M 6s
430400K .......... .......... .......... .......... .......... 84% 15.8M 6s
430450K .......... .......... .......... .......... .......... 84% 23.7M 6s
430500K .......... .......... .......... .......... .......... 84% 15.6M 6s
430550K .......... .......... .......... .......... .......... 84% 18.7M 6s
430600K .......... .......... .......... .......... .......... 84% 18.8M 6s
430650K .......... .......... .......... .......... .......... 84% 20.6M 6s
430700K .......... .......... .......... .......... .......... 84% 17.8M 6s
430750K .......... .......... .......... .......... .......... 84% 15.7M 6s
430800K .......... .......... .......... .......... .......... 84% 18.1M 6s
430850K .......... .......... .......... .......... .......... 84% 18.0M 6s
430900K .......... .......... .......... .......... .......... 84% 21.6M 6s
430950K .......... .......... .......... .......... .......... 84% 11.5M 6s
431000K .......... .......... .......... .......... .......... 84%  104M 6s
431050K .......... .......... .......... .......... .......... 84% 16.9M 6s
431100K .......... .......... .......... .......... .......... 84% 19.5M 6s
431150K .......... .......... .......... .......... .......... 84% 25.3M 6s
431200K .......... .......... .......... .......... .......... 84% 17.1M 6s
431250K .......... .......... .......... .......... .......... 84% 19.7M 6s
431300K .......... .......... .......... .......... .......... 84% 20.9M 6s
431350K .......... .......... .......... .......... .......... 84% 21.0M 6s
431400K .......... .......... .......... .......... .......... 84% 20.6M 6s
431450K .......... .......... .......... .......... .......... 84% 19.8M 6s
431500K .......... .......... .......... .......... .......... 84% 11.8M 6s
431550K .......... .......... .......... .......... .......... 84% 21.0M 6s
431600K .......... .......... .......... .......... .......... 84% 15.9M 6s
431650K .......... .......... .......... .......... .......... 84% 19.9M 6s
431700K .......... .......... .......... .......... .......... 84% 20.2M 6s
431750K .......... .......... .......... .......... .......... 84% 14.2M 6s
431800K .......... .......... .......... .......... .......... 84% 15.6M 6s
431850K .......... .......... .......... .......... .......... 84% 10.5M 6s
431900K .......... .......... .......... .......... .......... 84% 19.3M 6s
431950K .......... .......... .......... .......... .......... 84% 22.3M 6s
432000K .......... .......... .......... .......... .......... 84% 14.1M 6s
432050K .......... .......... .......... .......... .......... 84% 14.7M 6s
432100K .......... .......... .......... .......... .......... 84% 20.4M 6s
432150K .......... .......... .......... .......... .......... 85% 17.3M 6s
432200K .......... .......... .......... .......... .......... 85% 14.0M 6s
432250K .......... .......... .......... .......... .......... 85% 15.9M 6s
432300K .......... .......... .......... .......... .......... 85% 15.3M 6s
432350K .......... .......... .......... .......... .......... 85% 14.5M 6s
432400K .......... .......... .......... .......... .......... 85% 13.5M 6s
432450K .......... .......... .......... .......... .......... 85% 16.2M 6s
432500K .......... .......... .......... .......... .......... 85% 17.4M 6s
432550K .......... .......... .......... .......... .......... 85% 15.6M 6s
432600K .......... .......... .......... .......... .......... 85% 23.8M 6s
432650K .......... .......... .......... .......... .......... 85% 21.0M 6s
432700K .......... .......... .......... .......... .......... 85% 18.1M 6s
432750K .......... .......... .......... .......... .......... 85% 10.8M 6s
432800K .......... .......... .......... .......... .......... 85% 49.7M 6s
432850K .......... .......... .......... .......... .......... 85% 15.3M 6s
432900K .......... .......... .......... .......... .......... 85% 17.6M 6s
432950K .......... .......... .......... .......... .......... 85% 16.2M 6s
433000K .......... .......... .......... .......... .......... 85% 14.7M 6s
433050K .......... .......... .......... .......... .......... 85% 20.3M 6s
433100K .......... .......... .......... .......... .......... 85% 15.1M 6s
433150K .......... .......... .......... .......... .......... 85% 21.5M 6s
433200K .......... .......... .......... .......... .......... 85% 13.6M 6s
433250K .......... .......... .......... .......... .......... 85% 15.4M 6s
433300K .......... .......... .......... .......... .......... 85% 17.5M 6s
433350K .......... .......... .......... .......... .......... 85% 8.58M 6s
433400K .......... .......... .......... .......... .......... 85% 9.64M 6s
433450K .......... .......... .......... .......... .......... 85% 25.0M 6s
433500K .......... .......... .......... .......... .......... 85% 14.5M 6s
433550K .......... .......... .......... .......... .......... 85% 17.1M 6s
433600K .......... .......... .......... .......... .......... 85% 17.4M 6s
433650K .......... .......... .......... .......... .......... 85% 12.6M 6s
433700K .......... .......... .......... .......... .......... 85% 16.2M 6s
433750K .......... .......... .......... .......... .......... 85% 15.3M 6s
433800K .......... .......... .......... .......... .......... 85% 15.0M 6s
433850K .......... .......... .......... .......... .......... 85% 12.9M 6s
433900K .......... .......... .......... .......... .......... 85% 15.1M 6s
433950K .......... .......... .......... .......... .......... 85% 13.8M 6s
434000K .......... .......... .......... .......... .......... 85% 16.6M 6s
434050K .......... .......... .......... .......... .......... 85% 17.1M 6s
434100K .......... .......... .......... .......... .......... 85% 14.1M 6s
434150K .......... .......... .......... .......... .......... 85% 18.9M 6s
434200K .......... .......... .......... .......... .......... 85% 23.5M 6s
434250K .......... .......... .......... .......... .......... 85% 13.7M 6s
434300K .......... .......... .......... .......... .......... 85% 85.8M 6s
434350K .......... .......... .......... .......... .......... 85% 16.4M 6s
434400K .......... .......... .......... .......... .......... 85% 22.0M 6s
434450K .......... .......... .......... .......... .......... 85% 22.3M 6s
434500K .......... .......... .......... .......... .......... 85% 28.8M 6s
434550K .......... .......... .......... .......... .......... 85% 31.5M 6s
434600K .......... .......... .......... .......... .......... 85% 24.1M 6s
434650K .......... .......... .......... .......... .......... 85% 22.5M 6s
434700K .......... .......... .......... .......... .......... 85% 20.7M 6s
434750K .......... .......... .......... .......... .......... 85% 37.6M 6s
434800K .......... .......... .......... .......... .......... 85% 32.9M 6s
434850K .......... .......... .......... .......... .......... 85% 23.2M 6s
434900K .......... .......... .......... .......... .......... 85% 28.2M 6s
434950K .......... .......... .......... .......... .......... 85% 21.1M 6s
435000K .......... .......... .......... .......... .......... 85% 30.0M 6s
435050K .......... .......... .......... .......... .......... 85% 34.5M 6s
435100K .......... .......... .......... .......... .......... 85% 22.8M 6s
435150K .......... .......... .......... .......... .......... 85% 25.4M 6s
435200K .......... .......... .......... .......... .......... 85% 27.1M 6s
435250K .......... .......... .......... .......... .......... 85% 21.2M 6s
435300K .......... .......... .......... .......... .......... 85% 20.2M 5s
435350K .......... .......... .......... .......... .......... 85% 9.51M 5s
435400K .......... .......... .......... .......... .......... 85% 14.5M 5s
435450K .......... .......... .......... .......... .......... 85% 5.85M 5s
435500K .......... .......... .......... .......... .......... 85% 7.05M 5s
435550K .......... .......... .......... .......... .......... 85% 8.45M 5s
435600K .......... .......... .......... .......... .......... 85% 6.08M 5s
435650K .......... .......... .......... .......... .......... 85% 7.97M 5s
435700K .......... .......... .......... .......... .......... 85% 7.26M 5s
435750K .......... .......... .......... .......... .......... 85% 39.3M 5s
435800K .......... .......... .......... .......... .......... 85% 22.5M 5s
435850K .......... .......... .......... .......... .......... 85% 30.9M 5s
435900K .......... .......... .......... .......... .......... 85% 29.1M 5s
435950K .......... .......... .......... .......... .......... 85% 24.1M 5s
436000K .......... .......... .......... .......... .......... 85% 19.5M 5s
436050K .......... .......... .......... .......... .......... 85% 86.9M 5s
436100K .......... .......... .......... .......... .......... 85% 22.2M 5s
436150K .......... .......... .......... .......... .......... 85% 36.7M 5s
436200K .......... .......... .......... .......... .......... 85% 19.5M 5s
436250K .......... .......... .......... .......... .......... 85% 17.3M 5s
436300K .......... .......... .......... .......... .......... 85% 14.7M 5s
436350K .......... .......... .......... .......... .......... 85% 18.8M 5s
436400K .......... .......... .......... .......... .......... 85% 13.2M 5s
436450K .......... .......... .......... .......... .......... 85% 16.9M 5s
436500K .......... .......... .......... .......... .......... 85% 16.3M 5s
436550K .......... .......... .......... .......... .......... 85% 14.9M 5s
436600K .......... .......... .......... .......... .......... 85% 14.2M 5s
436650K .......... .......... .......... .......... .......... 85% 16.8M 5s
436700K .......... .......... .......... .......... .......... 85% 11.1M 5s
436750K .......... .......... .......... .......... .......... 85% 11.6M 5s
436800K .......... .......... .......... .......... .......... 85% 15.1M 5s
436850K .......... .......... .......... .......... .......... 85% 35.9M 5s
436900K .......... .......... .......... .......... .......... 85% 27.5M 5s
436950K .......... .......... .......... .......... .......... 85% 15.6M 5s
437000K .......... .......... .......... .......... .......... 85%  174M 5s
437050K .......... .......... .......... .......... .......... 85% 21.0M 5s
437100K .......... .......... .......... .......... .......... 85% 41.3M 5s
437150K .......... .......... .......... .......... .......... 85% 29.9M 5s
437200K .......... .......... .......... .......... .......... 85% 19.2M 5s
437250K .......... .......... .......... .......... .......... 86% 42.7M 5s
437300K .......... .......... .......... .......... .......... 86% 19.6M 5s
437350K .......... .......... .......... .......... .......... 86% 24.8M 5s
437400K .......... .......... .......... .......... .......... 86% 27.2M 5s
437450K .......... .......... .......... .......... .......... 86% 22.3M 5s
437500K .......... .......... .......... .......... .......... 86% 35.8M 5s
437550K .......... .......... .......... .......... .......... 86% 27.1M 5s
437600K .......... .......... .......... .......... .......... 86% 22.3M 5s
437650K .......... .......... .......... .......... .......... 86% 20.3M 5s
437700K .......... .......... .......... .......... .......... 86% 22.6M 5s
437750K .......... .......... .......... .......... .......... 86% 26.7M 5s
437800K .......... .......... .......... .......... .......... 86% 29.5M 5s
437850K .......... .......... .......... .......... .......... 86% 23.8M 5s
437900K .......... .......... .......... .......... .......... 86% 26.4M 5s
437950K .......... .......... .......... .......... .......... 86% 25.1M 5s
438000K .......... .......... .......... .......... .......... 86% 35.6M 5s
438050K .......... .......... .......... .......... .......... 86% 32.2M 5s
438100K .......... .......... .......... .......... .......... 86% 14.0M 5s
438150K .......... .......... .......... .......... .......... 86%  179M 5s
438200K .......... .......... .......... .......... .......... 86% 10.7M 5s
438250K .......... .......... .......... .......... .......... 86%  243M 5s
438300K .......... .......... .......... .......... .......... 86% 21.3M 5s
438350K .......... .......... .......... .......... .......... 86% 44.6M 5s
438400K .......... .......... .......... .......... .......... 86% 31.2M 5s
438450K .......... .......... .......... .......... .......... 86% 28.9M 5s
438500K .......... .......... .......... .......... .......... 86% 30.0M 5s
438550K .......... .......... .......... .......... .......... 86% 24.2M 5s
438600K .......... .......... .......... .......... .......... 86% 32.9M 5s
438650K .......... .......... .......... .......... .......... 86% 23.5M 5s
438700K .......... .......... .......... .......... .......... 86% 28.8M 5s
438750K .......... .......... .......... .......... .......... 86% 30.4M 5s
438800K .......... .......... .......... .......... .......... 86% 29.6M 5s
438850K .......... .......... .......... .......... .......... 86% 22.9M 5s
438900K .......... .......... .......... .......... .......... 86% 26.0M 5s
438950K .......... .......... .......... .......... .......... 86% 19.5M 5s
439000K .......... .......... .......... .......... .......... 86% 28.9M 5s
439050K .......... .......... .......... .......... .......... 86% 22.9M 5s
439100K .......... .......... .......... .......... .......... 86% 15.7M 5s
439150K .......... .......... .......... .......... .......... 86% 23.1M 5s
439200K .......... .......... .......... .......... .......... 86% 23.5M 5s
439250K .......... .......... .......... .......... .......... 86% 17.1M 5s
439300K .......... .......... .......... .......... .......... 86% 10.4M 5s
439350K .......... .......... .......... .......... .......... 86% 11.0M 5s
439400K .......... .......... .......... .......... .......... 86% 12.7M 5s
439450K .......... .......... .......... .......... .......... 86% 12.5M 5s
439500K .......... .......... .......... .......... .......... 86% 12.0M 5s
439550K .......... .......... .......... .......... .......... 86% 16.0M 5s
439600K .......... .......... .......... .......... .......... 86% 11.9M 5s
439650K .......... .......... .......... .......... .......... 86% 15.3M 5s
439700K .......... .......... .......... .......... .......... 86% 12.1M 5s
439750K .......... .......... .......... .......... .......... 86% 15.9M 5s
439800K .......... .......... .......... .......... .......... 86% 11.4M 5s
439850K .......... .......... .......... .......... .......... 86% 13.3M 5s
439900K .......... .......... .......... .......... .......... 86% 18.1M 5s
439950K .......... .......... .......... .......... .......... 86% 10.7M 5s
440000K .......... .......... .......... .......... .......... 86% 23.2M 5s
440050K .......... .......... .......... .......... .......... 86% 19.3M 5s
440100K .......... .......... .......... .......... .......... 86% 18.8M 5s
440150K .......... .......... .......... .......... .......... 86% 25.1M 5s
440200K .......... .......... .......... .......... .......... 86% 14.0M 5s
440250K .......... .......... .......... .......... .......... 86% 18.9M 5s
440300K .......... .......... .......... .......... .......... 86% 17.1M 5s
440350K .......... .......... .......... .......... .......... 86% 16.3M 5s
440400K .......... .......... .......... .......... .......... 86% 16.2M 5s
440450K .......... .......... .......... .......... .......... 86% 15.8M 5s
440500K .......... .......... .......... .......... .......... 86% 15.5M 5s
440550K .......... .......... .......... .......... .......... 86% 15.9M 5s
440600K .......... .......... .......... .......... .......... 86% 17.2M 5s
440650K .......... .......... .......... .......... .......... 86% 17.6M 5s
440700K .......... .......... .......... .......... .......... 86% 18.5M 5s
440750K .......... .......... .......... .......... .......... 86% 22.4M 5s
440800K .......... .......... .......... .......... .......... 86% 39.1M 5s
440850K .......... .......... .......... .......... .......... 86% 23.5M 5s
440900K .......... .......... .......... .......... .......... 86% 15.5M 5s
440950K .......... .......... .......... .......... .......... 86% 22.6M 5s
441000K .......... .......... .......... .......... .......... 86% 48.2M 5s
441050K .......... .......... .......... .......... .......... 86% 32.2M 5s
441100K .......... .......... .......... .......... .......... 86% 21.5M 5s
441150K .......... .......... .......... .......... .......... 86% 27.9M 5s
441200K .......... .......... .......... .......... .......... 86% 21.3M 5s
441250K .......... .......... .......... .......... .......... 86% 22.0M 5s
441300K .......... .......... .......... .......... .......... 86% 20.8M 5s
441350K .......... .......... .......... .......... .......... 86% 21.1M 5s
441400K .......... .......... .......... .......... .......... 86% 28.3M 5s
441450K .......... .......... .......... .......... .......... 86% 22.8M 5s
441500K .......... .......... .......... .......... .......... 86% 39.5M 5s
441550K .......... .......... .......... .......... .......... 86% 21.0M 5s
441600K .......... .......... .......... .......... .......... 86% 21.4M 5s
441650K .......... .......... .......... .......... .......... 86% 39.8M 5s
441700K .......... .......... .......... .......... .......... 86% 14.9M 5s
441750K .......... .......... .......... .......... .......... 86% 33.6M 5s
441800K .......... .......... .......... .......... .......... 86% 21.3M 5s
441850K .......... .......... .......... .......... .......... 86% 25.6M 5s
441900K .......... .......... .......... .......... .......... 86% 31.2M 5s
441950K .......... .......... .......... .......... .......... 86% 16.5M 5s
442000K .......... .......... .......... .......... .......... 86% 30.8M 5s
442050K .......... .......... .......... .......... .......... 86% 12.7M 5s
442100K .......... .......... .......... .......... .......... 86%  125M 5s
442150K .......... .......... .......... .......... .......... 86% 36.7M 5s
442200K .......... .......... .......... .......... .......... 86% 38.1M 5s
442250K .......... .......... .......... .......... .......... 86% 21.8M 5s
442300K .......... .......... .......... .......... .......... 87% 47.9M 5s
442350K .......... .......... .......... .......... .......... 87% 20.2M 5s
442400K .......... .......... .......... .......... .......... 87% 24.5M 5s
442450K .......... .......... .......... .......... .......... 87% 25.2M 5s
442500K .......... .......... .......... .......... .......... 87% 26.7M 5s
442550K .......... .......... .......... .......... .......... 87% 25.3M 5s
442600K .......... .......... .......... .......... .......... 87% 29.0M 5s
442650K .......... .......... .......... .......... .......... 87% 16.1M 5s
442700K .......... .......... .......... .......... .......... 87% 33.3M 5s
442750K .......... .......... .......... .......... .......... 87% 19.9M 5s
442800K .......... .......... .......... .......... .......... 87% 23.4M 5s
442850K .......... .......... .......... .......... .......... 87% 16.2M 5s
442900K .......... .......... .......... .......... .......... 87% 21.6M 5s
442950K .......... .......... .......... .......... .......... 87% 19.5M 5s
443000K .......... .......... .......... .......... .......... 87% 23.6M 5s
443050K .......... .......... .......... .......... .......... 87% 20.0M 5s
443100K .......... .......... .......... .......... .......... 87% 18.5M 5s
443150K .......... .......... .......... .......... .......... 87% 25.5M 5s
443200K .......... .......... .......... .......... .......... 87% 16.4M 5s
443250K .......... .......... .......... .......... .......... 87% 7.95M 5s
443300K .......... .......... .......... .......... .......... 87% 11.0M 5s
443350K .......... .......... .......... .......... .......... 87% 9.24M 5s
443400K .......... .......... .......... .......... .......... 87% 11.1M 5s
443450K .......... .......... .......... .......... .......... 87% 9.61M 5s
443500K .......... .......... .......... .......... .......... 87% 9.27M 5s
443550K .......... .......... .......... .......... .......... 87% 10.4M 5s
443600K .......... .......... .......... .......... .......... 87% 9.51M 5s
443650K .......... .......... .......... .......... .......... 87% 15.9M 5s
443700K .......... .......... .......... .......... .......... 87% 15.7M 5s
443750K .......... .......... .......... .......... .......... 87% 17.7M 5s
443800K .......... .......... .......... .......... .......... 87% 13.3M 5s
443850K .......... .......... .......... .......... .......... 87% 18.7M 5s
443900K .......... .......... .......... .......... .......... 87% 13.7M 5s
443950K .......... .......... .......... .......... .......... 87% 21.9M 5s
444000K .......... .......... .......... .......... .......... 87% 15.9M 5s
444050K .......... .......... .......... .......... .......... 87% 23.9M 5s
444100K .......... .......... .......... .......... .......... 87% 15.1M 5s
444150K .......... .......... .......... .......... .......... 87% 17.9M 5s
444200K .......... .......... .......... .......... .......... 87% 13.2M 5s
444250K .......... .......... .......... .......... .......... 87% 16.1M 5s
444300K .......... .......... .......... .......... .......... 87% 13.7M 5s
444350K .......... .......... .......... .......... .......... 87% 10.7M 5s
444400K .......... .......... .......... .......... .......... 87% 14.3M 5s
444450K .......... .......... .......... .......... .......... 87% 12.3M 5s
444500K .......... .......... .......... .......... .......... 87% 9.55M 5s
444550K .......... .......... .......... .......... .......... 87% 9.41M 5s
444600K .......... .......... .......... .......... .......... 87% 7.84M 5s
444650K .......... .......... .......... .......... .......... 87% 9.14M 5s
444700K .......... .......... .......... .......... .......... 87% 7.56M 5s
444750K .......... .......... .......... .......... .......... 87% 11.3M 5s
444800K .......... .......... .......... .......... .......... 87% 11.3M 5s
444850K .......... .......... .......... .......... .......... 87% 17.3M 5s
444900K .......... .......... .......... .......... .......... 87% 32.1M 5s
444950K .......... .......... .......... .......... .......... 87% 22.2M 5s
445000K .......... .......... .......... .......... .......... 87% 47.9M 5s
445050K .......... .......... .......... .......... .......... 87% 28.0M 5s
445100K .......... .......... .......... .......... .......... 87% 24.0M 5s
445150K .......... .......... .......... .......... .......... 87% 31.7M 5s
445200K .......... .......... .......... .......... .......... 87% 22.3M 5s
445250K .......... .......... .......... .......... .......... 87% 37.7M 5s
445300K .......... .......... .......... .......... .......... 87% 26.8M 5s
445350K .......... .......... .......... .......... .......... 87% 28.5M 5s
445400K .......... .......... .......... .......... .......... 87% 30.4M 5s
445450K .......... .......... .......... .......... .......... 87% 21.4M 5s
445500K .......... .......... .......... .......... .......... 87% 34.1M 5s
445550K .......... .......... .......... .......... .......... 87% 31.6M 5s
445600K .......... .......... .......... .......... .......... 87% 21.1M 5s
445650K .......... .......... .......... .......... .......... 87% 27.4M 5s
445700K .......... .......... .......... .......... .......... 87% 28.0M 5s
445750K .......... .......... .......... .......... .......... 87% 22.2M 5s
445800K .......... .......... .......... .......... .......... 87% 25.7M 5s
445850K .......... .......... .......... .......... .......... 87% 25.4M 5s
445900K .......... .......... .......... .......... .......... 87% 26.3M 5s
445950K .......... .......... .......... .......... .......... 87% 26.3M 5s
446000K .......... .......... .......... .......... .......... 87% 19.9M 5s
446050K .......... .......... .......... .......... .......... 87% 28.6M 5s
446100K .......... .......... .......... .......... .......... 87% 25.6M 5s
446150K .......... .......... .......... .......... .......... 87%  121M 5s
446200K .......... .......... .......... .......... .......... 87% 19.3M 5s
446250K .......... .......... .......... .......... .......... 87% 27.5M 5s
446300K .......... .......... .......... .......... .......... 87% 20.1M 5s
446350K .......... .......... .......... .......... .......... 87% 14.4M 5s
446400K .......... .......... .......... .......... .......... 87% 17.8M 5s
446450K .......... .......... .......... .......... .......... 87% 11.8M 5s
446500K .......... .......... .......... .......... .......... 87% 23.1M 5s
446550K .......... .......... .......... .......... .......... 87% 18.4M 5s
446600K .......... .......... .......... .......... .......... 87% 17.5M 5s
446650K .......... .......... .......... .......... .......... 87% 20.4M 5s
446700K .......... .......... .......... .......... .......... 87% 17.1M 5s
446750K .......... .......... .......... .......... .......... 87% 16.3M 5s
446800K .......... .......... .......... .......... .......... 87% 15.7M 5s
446850K .......... .......... .......... .......... .......... 87% 7.30M 5s
446900K .......... .......... .......... .......... .......... 87% 9.54M 5s
446950K .......... .......... .......... .......... .......... 87% 8.81M 5s
447000K .......... .......... .......... .......... .......... 87% 8.62M 5s
447050K .......... .......... .......... .......... .......... 87% 11.2M 5s
447100K .......... .......... .......... .......... .......... 87% 7.27M 5s
447150K .......... .......... .......... .......... .......... 87% 10.6M 5s
447200K .......... .......... .......... .......... .......... 87% 6.55M 5s
447250K .......... .......... .......... .......... .......... 87% 11.8M 5s
447300K .......... .......... .......... .......... .......... 87% 10.7M 5s
447350K .......... .......... .......... .......... .......... 87% 12.9M 5s
447400K .......... .......... .......... .......... .......... 88% 13.1M 5s
447450K .......... .......... .......... .......... .......... 88% 12.1M 5s
447500K .......... .......... .......... .......... .......... 88% 10.7M 5s
447550K .......... .......... .......... .......... .......... 88% 14.9M 5s
447600K .......... .......... .......... .......... .......... 88% 11.1M 5s
447650K .......... .......... .......... .......... .......... 88% 12.2M 5s
447700K .......... .......... .......... .......... .......... 88% 9.46M 5s
447750K .......... .......... .......... .......... .......... 88% 14.9M 5s
447800K .......... .......... .......... .......... .......... 88% 11.1M 5s
447850K .......... .......... .......... .......... .......... 88% 12.0M 5s
447900K .......... .......... .......... .......... .......... 88% 9.79M 5s
447950K .......... .......... .......... .......... .......... 88% 15.7M 5s
448000K .......... .......... .......... .......... .......... 88% 12.6M 5s
448050K .......... .......... .......... .......... .......... 88% 14.3M 5s
448100K .......... .......... .......... .......... .......... 88% 10.3M 5s
448150K .......... .......... .......... .......... .......... 88% 12.9M 5s
448200K .......... .......... .......... .......... .......... 88% 10.4M 4s
448250K .......... .......... .......... .......... .......... 88% 11.9M 4s
448300K .......... .......... .......... .......... .......... 88% 11.2M 4s
448350K .......... .......... .......... .......... .......... 88% 8.78M 4s
448400K .......... .......... .......... .......... .......... 88% 14.9M 4s
448450K .......... .......... .......... .......... .......... 88% 14.0M 4s
448500K .......... .......... .......... .......... .......... 88% 16.7M 4s
448550K .......... .......... .......... .......... .......... 88% 18.4M 4s
448600K .......... .......... .......... .......... .......... 88% 11.3M 4s
448650K .......... .......... .......... .......... .......... 88% 13.6M 4s
448700K .......... .......... .......... .......... .......... 88% 12.0M 4s
448750K .......... .......... .......... .......... .......... 88% 16.9M 4s
448800K .......... .......... .......... .......... .......... 88% 11.9M 4s
448850K .......... .......... .......... .......... .......... 88% 10.4M 4s
448900K .......... .......... .......... .......... .......... 88% 16.1M 4s
448950K .......... .......... .......... .......... .......... 88% 14.5M 4s
449000K .......... .......... .......... .......... .......... 88% 13.8M 4s
449050K .......... .......... .......... .......... .......... 88% 14.7M 4s
449100K .......... .......... .......... .......... .......... 88% 22.5M 4s
449150K .......... .......... .......... .......... .......... 88% 25.7M 4s
449200K .......... .......... .......... .......... .......... 88% 22.2M 4s
449250K .......... .......... .......... .......... .......... 88% 17.6M 4s
449300K .......... .......... .......... .......... .......... 88% 17.5M 4s
449350K .......... .......... .......... .......... .......... 88% 26.3M 4s
449400K .......... .......... .......... .......... .......... 88% 20.8M 4s
449450K .......... .......... .......... .......... .......... 88% 18.6M 4s
449500K .......... .......... .......... .......... .......... 88% 21.8M 4s
449550K .......... .......... .......... .......... .......... 88% 23.2M 4s
449600K .......... .......... .......... .......... .......... 88% 22.6M 4s
449650K .......... .......... .......... .......... .......... 88% 23.4M 4s
449700K .......... .......... .......... .......... .......... 88% 16.7M 4s
449750K .......... .......... .......... .......... .......... 88% 22.4M 4s
449800K .......... .......... .......... .......... .......... 88% 19.9M 4s
449850K .......... .......... .......... .......... .......... 88% 19.4M 4s
449900K .......... .......... .......... .......... .......... 88% 23.8M 4s
449950K .......... .......... .......... .......... .......... 88% 14.2M 4s
450000K .......... .......... .......... .......... .......... 88% 17.5M 4s
450050K .......... .......... .......... .......... .......... 88% 20.0M 4s
450100K .......... .......... .......... .......... .......... 88% 11.9M 4s
450150K .......... .......... .......... .......... .......... 88% 15.7M 4s
450200K .......... .......... .......... .......... .......... 88% 20.3M 4s
450250K .......... .......... .......... .......... .......... 88% 38.2M 4s
450300K .......... .......... .......... .......... .......... 88% 18.9M 4s
450350K .......... .......... .......... .......... .......... 88% 35.0M 4s
450400K .......... .......... .......... .......... .......... 88% 28.8M 4s
450450K .......... .......... .......... .......... .......... 88% 19.2M 4s
450500K .......... .......... .......... .......... .......... 88% 26.8M 4s
450550K .......... .......... .......... .......... .......... 88% 21.4M 4s
450600K .......... .......... .......... .......... .......... 88% 21.5M 4s
450650K .......... .......... .......... .......... .......... 88% 23.1M 4s
450700K .......... .......... .......... .......... .......... 88% 21.2M 4s
450750K .......... .......... .......... .......... .......... 88% 30.9M 4s
450800K .......... .......... .......... .......... .......... 88% 28.9M 4s
450850K .......... .......... .......... .......... .......... 88% 20.5M 4s
450900K .......... .......... .......... .......... .......... 88% 29.2M 4s
450950K .......... .......... .......... .......... .......... 88% 21.0M 4s
451000K .......... .......... .......... .......... .......... 88% 25.7M 4s
451050K .......... .......... .......... .......... .......... 88% 30.1M 4s
451100K .......... .......... .......... .......... .......... 88% 17.8M 4s
451150K .......... .......... .......... .......... .......... 88% 19.2M 4s
451200K .......... .......... .......... .......... .......... 88% 43.6M 4s
451250K .......... .......... .......... .......... .......... 88% 21.5M 4s
451300K .......... .......... .......... .......... .......... 88%  116M 4s
451350K .......... .......... .......... .......... .......... 88% 25.4M 4s
451400K .......... .......... .......... .......... .......... 88%  115M 4s
451450K .......... .......... .......... .......... .......... 88% 13.5M 4s
451500K .......... .......... .......... .......... .......... 88% 36.4M 4s
451550K .......... .......... .......... .......... .......... 88% 33.1M 4s
451600K .......... .......... .......... .......... .......... 88% 49.4M 4s
451650K .......... .......... .......... .......... .......... 88% 41.4M 4s
451700K .......... .......... .......... .......... .......... 88% 24.4M 4s
451750K .......... .......... .......... .......... .......... 88% 98.2M 4s
451800K .......... .......... .......... .......... .......... 88% 23.9M 4s
451850K .......... .......... .......... .......... .......... 88% 20.4M 4s
451900K .......... .......... .......... .......... .......... 88% 26.6M 4s
451950K .......... .......... .......... .......... .......... 88% 17.3M 4s
452000K .......... .......... .......... .......... .......... 88% 23.4M 4s
452050K .......... .......... .......... .......... .......... 88% 24.8M 4s
452100K .......... .......... .......... .......... .......... 88% 22.8M 4s
452150K .......... .......... .......... .......... .......... 88% 25.4M 4s
452200K .......... .......... .......... .......... .......... 88% 21.1M 4s
452250K .......... .......... .......... .......... .......... 88% 20.0M 4s
452300K .......... .......... .......... .......... .......... 88% 25.3M 4s
452350K .......... .......... .......... .......... .......... 88% 23.0M 4s
452400K .......... .......... .......... .......... .......... 88% 24.2M 4s
452450K .......... .......... .......... .......... .......... 88% 20.6M 4s
452500K .......... .......... .......... .......... .......... 89% 21.8M 4s
452550K .......... .......... .......... .......... .......... 89% 30.2M 4s
452600K .......... .......... .......... .......... .......... 89% 23.9M 4s
452650K .......... .......... .......... .......... .......... 89% 34.8M 4s
452700K .......... .......... .......... .......... .......... 89% 15.2M 4s
452750K .......... .......... .......... .......... .......... 89% 30.3M 4s
452800K .......... .......... .......... .......... .......... 89% 20.9M 4s
452850K .......... .......... .......... .......... .......... 89% 19.3M 4s
452900K .......... .......... .......... .......... .......... 89% 70.4M 4s
452950K .......... .......... .......... .......... .......... 89% 19.5M 4s
453000K .......... .......... .......... .......... .......... 89% 10.8M 4s
453050K .......... .......... .......... .......... .......... 89% 27.3M 4s
453100K .......... .......... .......... .......... .......... 89% 20.5M 4s
453150K .......... .......... .......... .......... .......... 89% 26.6M 4s
453200K .......... .......... .......... .......... .......... 89% 20.4M 4s
453250K .......... .......... .......... .......... .......... 89% 24.1M 4s
453300K .......... .......... .......... .......... .......... 89% 18.8M 4s
453350K .......... .......... .......... .......... .......... 89% 16.9M 4s
453400K .......... .......... .......... .......... .......... 89% 18.9M 4s
453450K .......... .......... .......... .......... .......... 89% 14.9M 4s
453500K .......... .......... .......... .......... .......... 89% 21.7M 4s
453550K .......... .......... .......... .......... .......... 89% 14.0M 4s
453600K .......... .......... .......... .......... .......... 89% 14.8M 4s
453650K .......... .......... .......... .......... .......... 89% 13.6M 4s
453700K .......... .......... .......... .......... .......... 89% 9.33M 4s
453750K .......... .......... .......... .......... .......... 89% 14.6M 4s
453800K .......... .......... .......... .......... .......... 89% 12.5M 4s
453850K .......... .......... .......... .......... .......... 89% 13.1M 4s
453900K .......... .......... .......... .......... .......... 89% 15.0M 4s
453950K .......... .......... .......... .......... .......... 89% 10.9M 4s
454000K .......... .......... .......... .......... .......... 89% 11.5M 4s
454050K .......... .......... .......... .......... .......... 89% 13.7M 4s
454100K .......... .......... .......... .......... .......... 89% 10.8M 4s
454150K .......... .......... .......... .......... .......... 89% 32.7M 4s
454200K .......... .......... .......... .......... .......... 89% 13.4M 4s
454250K .......... .......... .......... .......... .......... 89% 67.0M 4s
454300K .......... .......... .......... .......... .......... 89% 19.6M 4s
454350K .......... .......... .......... .......... .......... 89%  184M 4s
454400K .......... .......... .......... .......... .......... 89% 28.1M 4s
454450K .......... .......... .......... .......... .......... 89% 16.4M 4s
454500K .......... .......... .......... .......... .......... 89% 22.0M 4s
454550K .......... .......... .......... .......... .......... 89% 21.6M 4s
454600K .......... .......... .......... .......... .......... 89% 20.9M 4s
454650K .......... .......... .......... .......... .......... 89% 23.5M 4s
454700K .......... .......... .......... .......... .......... 89% 18.1M 4s
454750K .......... .......... .......... .......... .......... 89% 23.1M 4s
454800K .......... .......... .......... .......... .......... 89% 21.5M 4s
454850K .......... .......... .......... .......... .......... 89% 20.0M 4s
454900K .......... .......... .......... .......... .......... 89% 22.0M 4s
454950K .......... .......... .......... .......... .......... 89% 14.0M 4s
455000K .......... .......... .......... .......... .......... 89% 27.8M 4s
455050K .......... .......... .......... .......... .......... 89% 24.5M 4s
455100K .......... .......... .......... .......... .......... 89% 18.4M 4s
455150K .......... .......... .......... .......... .......... 89% 33.7M 4s
455200K .......... .......... .......... .......... .......... 89% 40.6M 4s
455250K .......... .......... .......... .......... .......... 89% 70.6M 4s
455300K .......... .......... .......... .......... .......... 89% 19.9M 4s
455350K .......... .......... .......... .......... .......... 89% 47.5M 4s
455400K .......... .......... .......... .......... .......... 89% 45.8M 4s
455450K .......... .......... .......... .......... .......... 89% 41.0M 4s
455500K .......... .......... .......... .......... .......... 89% 36.0M 4s
455550K .......... .......... .......... .......... .......... 89% 61.8M 4s
455600K .......... .......... .......... .......... .......... 89% 45.3M 4s
455650K .......... .......... .......... .......... .......... 89% 38.0M 4s
455700K .......... .......... .......... .......... .......... 89% 23.5M 4s
455750K .......... .......... .......... .......... .......... 89% 38.9M 4s
455800K .......... .......... .......... .......... .......... 89% 33.1M 4s
455850K .......... .......... .......... .......... .......... 89% 25.8M 4s
455900K .......... .......... .......... .......... .......... 89% 34.6M 4s
455950K .......... .......... .......... .......... .......... 89% 37.8M 4s
456000K .......... .......... .......... .......... .......... 89% 25.9M 4s
456050K .......... .......... .......... .......... .......... 89% 30.9M 4s
456100K .......... .......... .......... .......... .......... 89% 35.6M 4s
456150K .......... .......... .......... .......... .......... 89% 22.3M 4s
456200K .......... .......... .......... .......... .......... 89% 33.5M 4s
456250K .......... .......... .......... .......... .......... 89% 38.9M 4s
456300K .......... .......... .......... .......... .......... 89% 28.9M 4s
456350K .......... .......... .......... .......... .......... 89% 34.5M 4s
456400K .......... .......... .......... .......... .......... 89% 22.4M 4s
456450K .......... .......... .......... .......... .......... 89% 24.1M 4s
456500K .......... .......... .......... .......... .......... 89% 19.3M 4s
456550K .......... .......... .......... .......... .......... 89% 26.2M 4s
456600K .......... .......... .......... .......... .......... 89% 18.7M 4s
456650K .......... .......... .......... .......... .......... 89% 20.8M 4s
456700K .......... .......... .......... .......... .......... 89% 14.7M 4s
456750K .......... .......... .......... .......... .......... 89% 19.7M 4s
456800K .......... .......... .......... .......... .......... 89% 17.2M 4s
456850K .......... .......... .......... .......... .......... 89% 21.3M 4s
456900K .......... .......... .......... .......... .......... 89% 13.8M 4s
456950K .......... .......... .......... .......... .......... 89% 10.9M 4s
457000K .......... .......... .......... .......... .......... 89% 7.09M 4s
457050K .......... .......... .......... .......... .......... 89% 9.73M 4s
457100K .......... .......... .......... .......... .......... 89% 7.22M 4s
457150K .......... .......... .......... .......... .......... 89% 10.6M 4s
457200K .......... .......... .......... .......... .......... 89% 8.74M 4s
457250K .......... .......... .......... .......... .......... 89% 11.8M 4s
457300K .......... .......... .......... .......... .......... 89% 10.1M 4s
457350K .......... .......... .......... .......... .......... 89% 13.0M 4s
457400K .......... .......... .......... .......... .......... 89% 39.4M 4s
457450K .......... .......... .......... .......... .......... 89% 15.4M 4s
457500K .......... .......... .......... .......... .......... 89% 12.0M 4s
457550K .......... .......... .......... .......... .......... 90% 13.8M 4s
457600K .......... .......... .......... .......... .......... 90% 8.71M 4s
457650K .......... .......... .......... .......... .......... 90% 16.5M 4s
457700K .......... .......... .......... .......... .......... 90% 9.33M 4s
457750K .......... .......... .......... .......... .......... 90% 13.3M 4s
457800K .......... .......... .......... .......... .......... 90% 11.8M 4s
457850K .......... .......... .......... .......... .......... 90% 12.2M 4s
457900K .......... .......... .......... .......... .......... 90% 11.8M 4s
457950K .......... .......... .......... .......... .......... 90% 19.9M 4s
458000K .......... .......... .......... .......... .......... 90% 40.6M 4s
458050K .......... .......... .......... .......... .......... 90% 21.4M 4s
458100K .......... .......... .......... .......... .......... 90% 56.4M 4s
458150K .......... .......... .......... .......... .......... 90% 35.0M 4s
458200K .......... .......... .......... .......... .......... 90% 19.3M 4s
458250K .......... .......... .......... .......... .......... 90% 19.6M 4s
458300K .......... .......... .......... .......... .......... 90% 17.1M 4s
458350K .......... .......... .......... .......... .......... 90% 15.9M 4s
458400K .......... .......... .......... .......... .......... 90% 20.1M 4s
458450K .......... .......... .......... .......... .......... 90% 17.0M 4s
458500K .......... .......... .......... .......... .......... 90% 17.6M 4s
458550K .......... .......... .......... .......... .......... 90% 17.5M 4s
458600K .......... .......... .......... .......... .......... 90% 15.3M 4s
458650K .......... .......... .......... .......... .......... 90% 16.3M 4s
458700K .......... .......... .......... .......... .......... 90% 14.4M 4s
458750K .......... .......... .......... .......... .......... 90% 13.7M 4s
458800K .......... .......... .......... .......... .......... 90% 12.7M 4s
458850K .......... .......... .......... .......... .......... 90% 9.38M 4s
458900K .......... .......... .......... .......... .......... 90% 13.5M 4s
458950K .......... .......... .......... .......... .......... 90% 11.6M 4s
459000K .......... .......... .......... .......... .......... 90% 15.9M 4s
459050K .......... .......... .......... .......... .......... 90% 12.9M 4s
459100K .......... .......... .......... .......... .......... 90% 9.72M 4s
459150K .......... .......... .......... .......... .......... 90% 10.5M 4s
459200K .......... .......... .......... .......... .......... 90% 10.0M 4s
459250K .......... .......... .......... .......... .......... 90% 13.0M 4s
459300K .......... .......... .......... .......... .......... 90% 7.86M 4s
459350K .......... .......... .......... .......... .......... 90% 10.4M 4s
459400K .......... .......... .......... .......... .......... 90% 18.9M 4s
459450K .......... .......... .......... .......... .......... 90% 25.2M 4s
459500K .......... .......... .......... .......... .......... 90% 30.6M 4s
459550K .......... .......... .......... .......... .......... 90% 22.1M 4s
459600K .......... .......... .......... .......... .......... 90% 23.4M 4s
459650K .......... .......... .......... .......... .......... 90% 18.8M 4s
459700K .......... .......... .......... .......... .......... 90% 16.2M 4s
459750K .......... .......... .......... .......... .......... 90% 24.2M 4s
459800K .......... .......... .......... .......... .......... 90% 22.9M 4s
459850K .......... .......... .......... .......... .......... 90% 16.3M 4s
459900K .......... .......... .......... .......... .......... 90% 25.4M 4s
459950K .......... .......... .......... .......... .......... 90% 16.8M 4s
460000K .......... .......... .......... .......... .......... 90% 20.8M 4s
460050K .......... .......... .......... .......... .......... 90% 20.8M 4s
460100K .......... .......... .......... .......... .......... 90% 20.1M 4s
460150K .......... .......... .......... .......... .......... 90% 10.8M 4s
460200K .......... .......... .......... .......... .......... 90% 21.4M 4s
460250K .......... .......... .......... .......... .......... 90% 16.0M 4s
460300K .......... .......... .......... .......... .......... 90% 14.5M 4s
460350K .......... .......... .......... .......... .......... 90% 12.7M 4s
460400K .......... .......... .......... .......... .......... 90% 24.7M 4s
460450K .......... .......... .......... .......... .......... 90% 16.0M 4s
460500K .......... .......... .......... .......... .......... 90% 31.4M 4s
460550K .......... .......... .......... .......... .......... 90% 21.7M 4s
460600K .......... .......... .......... .......... .......... 90% 20.3M 4s
460650K .......... .......... .......... .......... .......... 90% 21.9M 4s
460700K .......... .......... .......... .......... .......... 90% 15.7M 4s
460750K .......... .......... .......... .......... .......... 90% 20.8M 4s
460800K .......... .......... .......... .......... .......... 90% 20.6M 4s
460850K .......... .......... .......... .......... .......... 90% 17.7M 4s
460900K .......... .......... .......... .......... .......... 90% 17.3M 4s
460950K .......... .......... .......... .......... .......... 90% 16.4M 4s
461000K .......... .......... .......... .......... .......... 90% 16.1M 4s
461050K .......... .......... .......... .......... .......... 90% 25.1M 4s
461100K .......... .......... .......... .......... .......... 90% 14.3M 4s
461150K .......... .......... .......... .......... .......... 90% 16.9M 4s
461200K .......... .......... .......... .......... .......... 90% 13.1M 3s
461250K .......... .......... .......... .......... .......... 90% 9.30M 3s
461300K .......... .......... .......... .......... .......... 90% 16.7M 3s
461350K .......... .......... .......... .......... .......... 90% 19.4M 3s
461400K .......... .......... .......... .......... .......... 90% 35.2M 3s
461450K .......... .......... .......... .......... .......... 90% 20.5M 3s
461500K .......... .......... .......... .......... .......... 90% 30.9M 3s
461550K .......... .......... .......... .......... .......... 90% 31.0M 3s
461600K .......... .......... .......... .......... .......... 90% 23.3M 3s
461650K .......... .......... .......... .......... .......... 90% 25.9M 3s
461700K .......... .......... .......... .......... .......... 90% 24.9M 3s
461750K .......... .......... .......... .......... .......... 90% 24.4M 3s
461800K .......... .......... .......... .......... .......... 90% 24.9M 3s
461850K .......... .......... .......... .......... .......... 90% 19.7M 3s
461900K .......... .......... .......... .......... .......... 90% 41.2M 3s
461950K .......... .......... .......... .......... .......... 90% 24.9M 3s
462000K .......... .......... .......... .......... .......... 90% 25.7M 3s
462050K .......... .......... .......... .......... .......... 90% 24.1M 3s
462100K .......... .......... .......... .......... .......... 90% 19.7M 3s
462150K .......... .......... .......... .......... .......... 90% 24.4M 3s
462200K .......... .......... .......... .......... .......... 90% 21.9M 3s
462250K .......... .......... .......... .......... .......... 90% 21.6M 3s
462300K .......... .......... .......... .......... .......... 90% 21.7M 3s
462350K .......... .......... .......... .......... .......... 90% 23.0M 3s
462400K .......... .......... .......... .......... .......... 90% 24.5M 3s
462450K .......... .......... .......... .......... .......... 90% 20.8M 3s
462500K .......... .......... .......... .......... .......... 90% 24.4M 3s
462550K .......... .......... .......... .......... .......... 90% 23.6M 3s
462600K .......... .......... .......... .......... .......... 90% 14.6M 3s
462650K .......... .......... .......... .......... .......... 91% 21.7M 3s
462700K .......... .......... .......... .......... .......... 91% 40.1M 3s
462750K .......... .......... .......... .......... .......... 91% 23.9M 3s
462800K .......... .......... .......... .......... .......... 91% 23.0M 3s
462850K .......... .......... .......... .......... .......... 91% 23.3M 3s
462900K .......... .......... .......... .......... .......... 91% 19.9M 3s
462950K .......... .......... .......... .......... .......... 91% 21.5M 3s
463000K .......... .......... .......... .......... .......... 91% 23.7M 3s
463050K .......... .......... .......... .......... .......... 91% 25.3M 3s
463100K .......... .......... .......... .......... .......... 91% 22.5M 3s
463150K .......... .......... .......... .......... .......... 91% 25.7M 3s
463200K .......... .......... .......... .......... .......... 91% 25.2M 3s
463250K .......... .......... .......... .......... .......... 91% 12.9M 3s
463300K .......... .......... .......... .......... .......... 91% 21.0M 3s
463350K .......... .......... .......... .......... .......... 91% 22.7M 3s
463400K .......... .......... .......... .......... .......... 91% 21.2M 3s
463450K .......... .......... .......... .......... .......... 91% 18.2M 3s
463500K .......... .......... .......... .......... .......... 91% 14.7M 3s
463550K .......... .......... .......... .......... .......... 91%  136M 3s
463600K .......... .......... .......... .......... .......... 91% 21.3M 3s
463650K .......... .......... .......... .......... .......... 91% 33.5M 3s
463700K .......... .......... .......... .......... .......... 91% 21.2M 3s
463750K .......... .......... .......... .......... .......... 91% 24.3M 3s
463800K .......... .......... .......... .......... .......... 91% 17.8M 3s
463850K .......... .......... .......... .......... .......... 91% 17.6M 3s
463900K .......... .......... .......... .......... .......... 91% 26.4M 3s
463950K .......... .......... .......... .......... .......... 91% 15.7M 3s
464000K .......... .......... .......... .......... .......... 91% 25.9M 3s
464050K .......... .......... .......... .......... .......... 91% 22.7M 3s
464100K .......... .......... .......... .......... .......... 91% 18.0M 3s
464150K .......... .......... .......... .......... .......... 91% 22.1M 3s
464200K .......... .......... .......... .......... .......... 91% 14.5M 3s
464250K .......... .......... .......... .......... .......... 91% 23.8M 3s
464300K .......... .......... .......... .......... .......... 91% 26.4M 3s
464350K .......... .......... .......... .......... .......... 91% 16.3M 3s
464400K .......... .......... .......... .......... .......... 91% 15.6M 3s
464450K .......... .......... .......... .......... .......... 91% 10.8M 3s
464500K .......... .......... .......... .......... .......... 91% 12.7M 3s
464550K .......... .......... .......... .......... .......... 91% 30.2M 3s
464600K .......... .......... .......... .......... .......... 91% 22.2M 3s
464650K .......... .......... .......... .......... .......... 91% 17.6M 3s
464700K .......... .......... .......... .......... .......... 91% 15.1M 3s
464750K .......... .......... .......... .......... .......... 91% 26.0M 3s
464800K .......... .......... .......... .......... .......... 91% 21.5M 3s
464850K .......... .......... .......... .......... .......... 91% 13.7M 3s
464900K .......... .......... .......... .......... .......... 91% 24.9M 3s
464950K .......... .......... .......... .......... .......... 91% 18.7M 3s
465000K .......... .......... .......... .......... .......... 91% 20.1M 3s
465050K .......... .......... .......... .......... .......... 91% 23.6M 3s
465100K .......... .......... .......... .......... .......... 91% 15.8M 3s
465150K .......... .......... .......... .......... .......... 91% 26.1M 3s
465200K .......... .......... .......... .......... .......... 91% 18.4M 3s
465250K .......... .......... .......... .......... .......... 91% 19.7M 3s
465300K .......... .......... .......... .......... .......... 91% 18.9M 3s
465350K .......... .......... .......... .......... .......... 91% 23.9M 3s
465400K .......... .......... .......... .......... .......... 91% 11.7M 3s
465450K .......... .......... .......... .......... .......... 91% 14.2M 3s
465500K .......... .......... .......... .......... .......... 91% 37.2M 3s
465550K .......... .......... .......... .......... .......... 91% 18.7M 3s
465600K .......... .......... .......... .......... .......... 91% 18.8M 3s
465650K .......... .......... .......... .......... .......... 91% 24.5M 3s
465700K .......... .......... .......... .......... .......... 91% 17.3M 3s
465750K .......... .......... .......... .......... .......... 91% 20.9M 3s
465800K .......... .......... .......... .......... .......... 91% 22.6M 3s
465850K .......... .......... .......... .......... .......... 91% 21.2M 3s
465900K .......... .......... .......... .......... .......... 91% 24.1M 3s
465950K .......... .......... .......... .......... .......... 91% 18.0M 3s
466000K .......... .......... .......... .......... .......... 91% 20.8M 3s
466050K .......... .......... .......... .......... .......... 91% 23.7M 3s
466100K .......... .......... .......... .......... .......... 91% 16.9M 3s
466150K .......... .......... .......... .......... .......... 91% 21.5M 3s
466200K .......... .......... .......... .......... .......... 91% 16.4M 3s
466250K .......... .......... .......... .......... .......... 91% 21.7M 3s
466300K .......... .......... .......... .......... .......... 91% 19.9M 3s
466350K .......... .......... .......... .......... .......... 91% 19.6M 3s
466400K .......... .......... .......... .......... .......... 91% 32.4M 3s
466450K .......... .......... .......... .......... .......... 91% 17.5M 3s
466500K .......... .......... .......... .......... .......... 91%  135M 3s
466550K .......... .......... .......... .......... .......... 91%  134M 3s
466600K .......... .......... .......... .......... .......... 91% 26.1M 3s
466650K .......... .......... .......... .......... .......... 91% 57.2M 3s
466700K .......... .......... .......... .......... .......... 91% 25.8M 3s
466750K .......... .......... .......... .......... .......... 91% 61.4M 3s
466800K .......... .......... .......... .......... .......... 91% 31.0M 3s
466850K .......... .......... .......... .......... .......... 91% 35.6M 3s
466900K .......... .......... .......... .......... .......... 91% 34.7M 3s
466950K .......... .......... .......... .......... .......... 91% 30.5M 3s
467000K .......... .......... .......... .......... .......... 91% 34.1M 3s
467050K .......... .......... .......... .......... .......... 91% 37.4M 3s
467100K .......... .......... .......... .......... .......... 91% 33.0M 3s
467150K .......... .......... .......... .......... .......... 91% 33.0M 3s
467200K .......... .......... .......... .......... .......... 91% 28.8M 3s
467250K .......... .......... .......... .......... .......... 91% 49.4M 3s
467300K .......... .......... .......... .......... .......... 91% 24.0M 3s
467350K .......... .......... .......... .......... .......... 91% 35.8M 3s
467400K .......... .......... .......... .......... .......... 91% 36.7M 3s
467450K .......... .......... .......... .......... .......... 91% 35.6M 3s
467500K .......... .......... .......... .......... .......... 91% 27.2M 3s
467550K .......... .......... .......... .......... .......... 91% 44.5M 3s
467600K .......... .......... .......... .......... .......... 91% 41.6M 3s
467650K .......... .......... .......... .......... .......... 91% 40.6M 3s
467700K .......... .......... .......... .......... .......... 91% 29.5M 3s
467750K .......... .......... .......... .......... .......... 92% 40.0M 3s
467800K .......... .......... .......... .......... .......... 92% 38.3M 3s
467850K .......... .......... .......... .......... .......... 92% 27.9M 3s
467900K .......... .......... .......... .......... .......... 92% 38.6M 3s
467950K .......... .......... .......... .......... .......... 92% 47.7M 3s
468000K .......... .......... .......... .......... .......... 92% 34.0M 3s
468050K .......... .......... .......... .......... .......... 92% 15.5M 3s
468100K .......... .......... .......... .......... .......... 92% 58.1M 3s
468150K .......... .......... .......... .......... .......... 92%  148M 3s
468200K .......... .......... .......... .......... .......... 92% 26.9M 3s
468250K .......... .......... .......... .......... .......... 92% 37.5M 3s
468300K .......... .......... .......... .......... .......... 92%  109M 3s
468350K .......... .......... .......... .......... .......... 92% 31.4M 3s
468400K .......... .......... .......... .......... .......... 92% 54.6M 3s
468450K .......... .......... .......... .......... .......... 92% 34.9M 3s
468500K .......... .......... .......... .......... .......... 92% 43.1M 3s
468550K .......... .......... .......... .......... .......... 92% 25.0M 3s
468600K .......... .......... .......... .......... .......... 92% 27.1M 3s
468650K .......... .......... .......... .......... .......... 92% 39.6M 3s
468700K .......... .......... .......... .......... .......... 92% 30.0M 3s
468750K .......... .......... .......... .......... .......... 92% 19.1M 3s
468800K .......... .......... .......... .......... .......... 92% 65.5M 3s
468850K .......... .......... .......... .......... .......... 92% 28.5M 3s
468900K .......... .......... .......... .......... .......... 92% 32.9M 3s
468950K .......... .......... .......... .......... .......... 92% 28.9M 3s
469000K .......... .......... .......... .......... .......... 92% 27.2M 3s
469050K .......... .......... .......... .......... .......... 92% 29.3M 3s
469100K .......... .......... .......... .......... .......... 92% 27.5M 3s
469150K .......... .......... .......... .......... .......... 92% 29.3M 3s
469200K .......... .......... .......... .......... .......... 92% 19.9M 3s
469250K .......... .......... .......... .......... .......... 92% 30.5M 3s
469300K .......... .......... .......... .......... .......... 92% 24.8M 3s
469350K .......... .......... .......... .......... .......... 92% 45.7M 3s
469400K .......... .......... .......... .......... .......... 92% 21.0M 3s
469450K .......... .......... .......... .......... .......... 92% 18.4M 3s
469500K .......... .......... .......... .......... .......... 92% 32.1M 3s
469550K .......... .......... .......... .......... .......... 92% 40.1M 3s
469600K .......... .......... .......... .......... .......... 92% 21.6M 3s
469650K .......... .......... .......... .......... .......... 92% 26.2M 3s
469700K .......... .......... .......... .......... .......... 92% 23.3M 3s
469750K .......... .......... .......... .......... .......... 92% 23.9M 3s
469800K .......... .......... .......... .......... .......... 92% 32.0M 3s
469850K .......... .......... .......... .......... .......... 92% 53.7M 3s
469900K .......... .......... .......... .......... .......... 92% 19.9M 3s
469950K .......... .......... .......... .......... .......... 92% 12.6M 3s
470000K .......... .......... .......... .......... .......... 92%  207M 3s
470050K .......... .......... .......... .......... .......... 92% 22.0M 3s
470100K .......... .......... .......... .......... .......... 92% 19.7M 3s
470150K .......... .......... .......... .......... .......... 92% 49.2M 3s
470200K .......... .......... .......... .......... .......... 92% 21.6M 3s
470250K .......... .......... .......... .......... .......... 92% 26.6M 3s
470300K .......... .......... .......... .......... .......... 92% 28.4M 3s
470350K .......... .......... .......... .......... .......... 92% 21.5M 3s
470400K .......... .......... .......... .......... .......... 92% 23.3M 3s
470450K .......... .......... .......... .......... .......... 92% 24.2M 3s
470500K .......... .......... .......... .......... .......... 92% 24.6M 3s
470550K .......... .......... .......... .......... .......... 92% 27.1M 3s
470600K .......... .......... .......... .......... .......... 92% 24.1M 3s
470650K .......... .......... .......... .......... .......... 92% 23.4M 3s
470700K .......... .......... .......... .......... .......... 92% 24.3M 3s
470750K .......... .......... .......... .......... .......... 92% 25.8M 3s
470800K .......... .......... .......... .......... .......... 92% 23.6M 3s
470850K .......... .......... .......... .......... .......... 92% 23.6M 3s
470900K .......... .......... .......... .......... .......... 92% 18.7M 3s
470950K .......... .......... .......... .......... .......... 92% 14.0M 3s
471000K .......... .......... .......... .......... .......... 92% 26.0M 3s
471050K .......... .......... .......... .......... .......... 92% 24.2M 3s
471100K .......... .......... .......... .......... .......... 92% 26.1M 3s
471150K .......... .......... .......... .......... .......... 92% 20.7M 3s
471200K .......... .......... .......... .......... .......... 92% 24.5M 3s
471250K .......... .......... .......... .......... .......... 92% 23.9M 3s
471300K .......... .......... .......... .......... .......... 92% 16.3M 3s
471350K .......... .......... .......... .......... .......... 92% 16.9M 3s
471400K .......... .......... .......... .......... .......... 92% 14.0M 3s
471450K .......... .......... .......... .......... .......... 92% 15.8M 3s
471500K .......... .......... .......... .......... .......... 92% 16.2M 3s
471550K .......... .......... .......... .......... .......... 92% 14.0M 3s
471600K .......... .......... .......... .......... .......... 92% 14.8M 3s
471650K .......... .......... .......... .......... .......... 92% 16.8M 3s
471700K .......... .......... .......... .......... .......... 92% 16.3M 3s
471750K .......... .......... .......... .......... .......... 92% 18.5M 3s
471800K .......... .......... .......... .......... .......... 92% 11.9M 3s
471850K .......... .......... .......... .......... .......... 92% 19.8M 3s
471900K .......... .......... .......... .......... .......... 92% 32.5M 3s
471950K .......... .......... .......... .......... .......... 92% 16.1M 3s
472000K .......... .......... .......... .......... .......... 92% 21.8M 3s
472050K .......... .......... .......... .......... .......... 92% 46.1M 3s
472100K .......... .......... .......... .......... .......... 92% 18.7M 3s
472150K .......... .......... .......... .......... .......... 92% 13.7M 3s
472200K .......... .......... .......... .......... .......... 92% 20.3M 3s
472250K .......... .......... .......... .......... .......... 92% 23.7M 3s
472300K .......... .......... .......... .......... .......... 92% 13.9M 3s
472350K .......... .......... .......... .......... .......... 92% 13.2M 3s
472400K .......... .......... .......... .......... .......... 92% 13.8M 3s
472450K .......... .......... .......... .......... .......... 92% 13.9M 3s
472500K .......... .......... .......... .......... .......... 92% 16.2M 3s
472550K .......... .......... .......... .......... .......... 92% 16.3M 3s
472600K .......... .......... .......... .......... .......... 92% 13.2M 3s
472650K .......... .......... .......... .......... .......... 92% 14.3M 3s
472700K .......... .......... .......... .......... .......... 92% 12.1M 3s
472750K .......... .......... .......... .......... .......... 92% 16.8M 3s
472800K .......... .......... .......... .......... .......... 93% 17.6M 3s
472850K .......... .......... .......... .......... .......... 93% 29.9M 3s
472900K .......... .......... .......... .......... .......... 93% 55.9M 3s
472950K .......... .......... .......... .......... .......... 93% 35.1M 3s
473000K .......... .......... .......... .......... .......... 93% 40.1M 3s
473050K .......... .......... .......... .......... .......... 93% 64.7M 3s
473100K .......... .......... .......... .......... .......... 93% 27.8M 3s
473150K .......... .......... .......... .......... .......... 93% 29.9M 3s
473200K .......... .......... .......... .......... .......... 93% 46.6M 3s
473250K .......... .......... .......... .......... .......... 93% 36.0M 3s
473300K .......... .......... .......... .......... .......... 93% 27.6M 3s
473350K .......... .......... .......... .......... .......... 93% 40.5M 3s
473400K .......... .......... .......... .......... .......... 93% 38.3M 3s
473450K .......... .......... .......... .......... .......... 93% 18.7M 3s
473500K .......... .......... .......... .......... .......... 93%  101M 3s
473550K .......... .......... .......... .......... .......... 93% 29.3M 3s
473600K .......... .......... .......... .......... .......... 93% 29.2M 3s
473650K .......... .......... .......... .......... .......... 93% 27.2M 3s
473700K .......... .......... .......... .......... .......... 93% 30.1M 3s
473750K .......... .......... .......... .......... .......... 93% 27.4M 3s
473800K .......... .......... .......... .......... .......... 93% 31.3M 3s
473850K .......... .......... .......... .......... .......... 93% 18.9M 3s
473900K .......... .......... .......... .......... .......... 93% 30.5M 3s
473950K .......... .......... .......... .......... .......... 93% 27.3M 3s
474000K .......... .......... .......... .......... .......... 93% 20.3M 3s
474050K .......... .......... .......... .......... .......... 93% 38.8M 3s
474100K .......... .......... .......... .......... .......... 93% 39.6M 3s
474150K .......... .......... .......... .......... .......... 93% 26.0M 3s
474200K .......... .......... .......... .......... .......... 93% 36.1M 3s
474250K .......... .......... .......... .......... .......... 93% 36.4M 3s
474300K .......... .......... .......... .......... .......... 93% 18.1M 2s
474350K .......... .......... .......... .......... .......... 93% 29.8M 2s
474400K .......... .......... .......... .......... .......... 93% 32.8M 2s
474450K .......... .......... .......... .......... .......... 93% 19.1M 2s
474500K .......... .......... .......... .......... .......... 93% 28.1M 2s
474550K .......... .......... .......... .......... .......... 93% 31.7M 2s
474600K .......... .......... .......... .......... .......... 93% 64.1M 2s
474650K .......... .......... .......... .......... .......... 93% 44.1M 2s
474700K .......... .......... .......... .......... .......... 93% 15.2M 2s
474750K .......... .......... .......... .......... .......... 93%  185M 2s
474800K .......... .......... .......... .......... .......... 93%  139M 2s
474850K .......... .......... .......... .......... .......... 93% 18.0M 2s
474900K .......... .......... .......... .......... .......... 93%  147M 2s
474950K .......... .......... .......... .......... .......... 93%  153M 2s
475000K .......... .......... .......... .......... .......... 93% 45.8M 2s
475050K .......... .......... .......... .......... .......... 93% 35.2M 2s
475100K .......... .......... .......... .......... .......... 93% 27.6M 2s
475150K .......... .......... .......... .......... .......... 93% 54.1M 2s
475200K .......... .......... .......... .......... .......... 93% 32.7M 2s
475250K .......... .......... .......... .......... .......... 93% 34.6M 2s
475300K .......... .......... .......... .......... .......... 93% 44.1M 2s
475350K .......... .......... .......... .......... .......... 93% 27.6M 2s
475400K .......... .......... .......... .......... .......... 93% 27.9M 2s
475450K .......... .......... .......... .......... .......... 93% 42.5M 2s
475500K .......... .......... .......... .......... .......... 93% 33.4M 2s
475550K .......... .......... .......... .......... .......... 93% 26.7M 2s
475600K .......... .......... .......... .......... .......... 93% 35.1M 2s
475650K .......... .......... .......... .......... .......... 93% 43.7M 2s
475700K .......... .......... .......... .......... .......... 93% 37.1M 2s
475750K .......... .......... .......... .......... .......... 93% 34.6M 2s
475800K .......... .......... .......... .......... .......... 93% 47.8M 2s
475850K .......... .......... .......... .......... .......... 93% 29.2M 2s
475900K .......... .......... .......... .......... .......... 93% 44.2M 2s
475950K .......... .......... .......... .......... .......... 93% 32.6M 2s
476000K .......... .......... .......... .......... .......... 93% 35.9M 2s
476050K .......... .......... .......... .......... .......... 93% 48.3M 2s
476100K .......... .......... .......... .......... .......... 93% 25.0M 2s
476150K .......... .......... .......... .......... .......... 93% 41.0M 2s
476200K .......... .......... .......... .......... .......... 93% 38.5M 2s
476250K .......... .......... .......... .......... .......... 93% 37.5M 2s
476300K .......... .......... .......... .......... .......... 93% 33.4M 2s
476350K .......... .......... .......... .......... .......... 93% 40.6M 2s
476400K .......... .......... .......... .......... .......... 93% 23.9M 2s
476450K .......... .......... .......... .......... .......... 93% 26.0M 2s
476500K .......... .......... .......... .......... .......... 93% 16.6M 2s
476550K .......... .......... .......... .......... .......... 93%  137M 2s
476600K .......... .......... .......... .......... .......... 93%  126M 2s
476650K .......... .......... .......... .......... .......... 93% 15.0M 2s
476700K .......... .......... .......... .......... .......... 93% 30.0M 2s
476750K .......... .......... .......... .......... .......... 93% 56.7M 2s
476800K .......... .......... .......... .......... .......... 93% 21.3M 2s
476850K .......... .......... .......... .......... .......... 93% 32.5M 2s
476900K .......... .......... .......... .......... .......... 93% 36.3M 2s
476950K .......... .......... .......... .......... .......... 93% 16.8M 2s
477000K .......... .......... .......... .......... .......... 93% 44.3M 2s
477050K .......... .......... .......... .......... .......... 93% 23.1M 2s
477100K .......... .......... .......... .......... .......... 93% 23.5M 2s
477150K .......... .......... .......... .......... .......... 93% 21.0M 2s
477200K .......... .......... .......... .......... .......... 93% 18.7M 2s
477250K .......... .......... .......... .......... .......... 93% 26.4M 2s
477300K .......... .......... .......... .......... .......... 93% 19.3M 2s
477350K .......... .......... .......... .......... .......... 93% 24.4M 2s
477400K .......... .......... .......... .......... .......... 93% 20.5M 2s
477450K .......... .......... .......... .......... .......... 93% 23.2M 2s
477500K .......... .......... .......... .......... .......... 93% 30.0M 2s
477550K .......... .......... .......... .......... .......... 93% 24.4M 2s
477600K .......... .......... .......... .......... .......... 93% 19.4M 2s
477650K .......... .......... .......... .......... .......... 93% 18.0M 2s
477700K .......... .......... .......... .......... .......... 93% 50.4M 2s
477750K .......... .......... .......... .......... .......... 93% 20.7M 2s
477800K .......... .......... .......... .......... .......... 93% 28.6M 2s
477850K .......... .......... .......... .......... .......... 93% 18.0M 2s
477900K .......... .......... .......... .......... .......... 94%  114M 2s
477950K .......... .......... .......... .......... .......... 94% 20.8M 2s
478000K .......... .......... .......... .......... .......... 94% 20.5M 2s
478050K .......... .......... .......... .......... .......... 94% 35.7M 2s
478100K .......... .......... .......... .......... .......... 94% 22.6M 2s
478150K .......... .......... .......... .......... .......... 94% 28.4M 2s
478200K .......... .......... .......... .......... .......... 94% 28.2M 2s
478250K .......... .......... .......... .......... .......... 94% 28.3M 2s
478300K .......... .......... .......... .......... .......... 94% 46.5M 2s
478350K .......... .......... .......... .......... .......... 94% 30.3M 2s
478400K .......... .......... .......... .......... .......... 94% 25.1M 2s
478450K .......... .......... .......... .......... .......... 94% 36.9M 2s
478500K .......... .......... .......... .......... .......... 94% 21.7M 2s
478550K .......... .......... .......... .......... .......... 94% 28.0M 2s
478600K .......... .......... .......... .......... .......... 94% 26.6M 2s
478650K .......... .......... .......... .......... .......... 94% 29.5M 2s
478700K .......... .......... .......... .......... .......... 94% 24.7M 2s
478750K .......... .......... .......... .......... .......... 94% 31.7M 2s
478800K .......... .......... .......... .......... .......... 94% 35.8M 2s
478850K .......... .......... .......... .......... .......... 94% 20.6M 2s
478900K .......... .......... .......... .......... .......... 94% 46.8M 2s
478950K .......... .......... .......... .......... .......... 94% 21.6M 2s
479000K .......... .......... .......... .......... .......... 94% 40.8M 2s
479050K .......... .......... .......... .......... .......... 94% 44.5M 2s
479100K .......... .......... .......... .......... .......... 94% 42.0M 2s
479150K .......... .......... .......... .......... .......... 94% 79.7M 2s
479200K .......... .......... .......... .......... .......... 94% 17.3M 2s
479250K .......... .......... .......... .......... .......... 94%  130M 2s
479300K .......... .......... .......... .......... .......... 94%  151M 2s
479350K .......... .......... .......... .......... .......... 94% 19.2M 2s
479400K .......... .......... .......... .......... .......... 94%  144M 2s
479450K .......... .......... .......... .......... .......... 94% 44.6M 2s
479500K .......... .......... .......... .......... .......... 94% 27.1M 2s
479550K .......... .......... .......... .......... .......... 94% 53.8M 2s
479600K .......... .......... .......... .......... .......... 94% 22.6M 2s
479650K .......... .......... .......... .......... .......... 94% 33.2M 2s
479700K .......... .......... .......... .......... .......... 94% 21.0M 2s
479750K .......... .......... .......... .......... .......... 94% 29.6M 2s
479800K .......... .......... .......... .......... .......... 94% 35.1M 2s
479850K .......... .......... .......... .......... .......... 94% 38.4M 2s
479900K .......... .......... .......... .......... .......... 94% 28.3M 2s
479950K .......... .......... .......... .......... .......... 94% 31.3M 2s
480000K .......... .......... .......... .......... .......... 94% 29.2M 2s
480050K .......... .......... .......... .......... .......... 94% 43.7M 2s
480100K .......... .......... .......... .......... .......... 94% 24.6M 2s
480150K .......... .......... .......... .......... .......... 94% 34.6M 2s
480200K .......... .......... .......... .......... .......... 94% 30.0M 2s
480250K .......... .......... .......... .......... .......... 94% 35.4M 2s
480300K .......... .......... .......... .......... .......... 94% 39.2M 2s
480350K .......... .......... .......... .......... .......... 94% 26.3M 2s
480400K .......... .......... .......... .......... .......... 94% 42.3M 2s
480450K .......... .......... .......... .......... .......... 94% 34.0M 2s
480500K .......... .......... .......... .......... .......... 94% 25.1M 2s
480550K .......... .......... .......... .......... .......... 94% 39.3M 2s
480600K .......... .......... .......... .......... .......... 94% 33.0M 2s
480650K .......... .......... .......... .......... .......... 94% 31.1M 2s
480700K .......... .......... .......... .......... .......... 94% 20.6M 2s
480750K .......... .......... .......... .......... .......... 94% 57.7M 2s
480800K .......... .......... .......... .......... .......... 94% 45.2M 2s
480850K .......... .......... .......... .......... .......... 94% 43.7M 2s
480900K .......... .......... .......... .......... .......... 94% 34.4M 2s
480950K .......... .......... .......... .......... .......... 94% 24.2M 2s
481000K .......... .......... .......... .......... .......... 94% 31.4M 2s
481050K .......... .......... .......... .......... .......... 94% 24.7M 2s
481100K .......... .......... .......... .......... .......... 94% 25.5M 2s
481150K .......... .......... .......... .......... .......... 94% 21.0M 2s
481200K .......... .......... .......... .......... .......... 94% 21.2M 2s
481250K .......... .......... .......... .......... .......... 94% 19.1M 2s
481300K .......... .......... .......... .......... .......... 94% 27.8M 2s
481350K .......... .......... .......... .......... .......... 94% 20.5M 2s
481400K .......... .......... .......... .......... .......... 94% 20.0M 2s
481450K .......... .......... .......... .......... .......... 94% 23.4M 2s
481500K .......... .......... .......... .......... .......... 94% 27.5M 2s
481550K .......... .......... .......... .......... .......... 94% 21.2M 2s
481600K .......... .......... .......... .......... .......... 94% 35.6M 2s
481650K .......... .......... .......... .......... .......... 94% 18.5M 2s
481700K .......... .......... .......... .......... .......... 94% 26.1M 2s
481750K .......... .......... .......... .......... .......... 94% 28.4M 2s
481800K .......... .......... .......... .......... .......... 94% 31.5M 2s
481850K .......... .......... .......... .......... .......... 94% 23.2M 2s
481900K .......... .......... .......... .......... .......... 94%  105M 2s
481950K .......... .......... .......... .......... .......... 94% 52.0M 2s
482000K .......... .......... .......... .......... .......... 94% 60.9M 2s
482050K .......... .......... .......... .......... .......... 94% 21.6M 2s
482100K .......... .......... .......... .......... .......... 94% 43.1M 2s
482150K .......... .......... .......... .......... .......... 94%  225M 2s
482200K .......... .......... .......... .......... .......... 94% 23.0M 2s
482250K .......... .......... .......... .......... .......... 94%  167M 2s
482300K .......... .......... .......... .......... .......... 94%  215M 2s
482350K .......... .......... .......... .......... .......... 94% 25.3M 2s
482400K .......... .......... .......... .......... .......... 94% 33.7M 2s
482450K .......... .......... .......... .......... .......... 94% 36.6M 2s
482500K .......... .......... .......... .......... .......... 94% 43.2M 2s
482550K .......... .......... .......... .......... .......... 94% 45.0M 2s
482600K .......... .......... .......... .......... .......... 94% 42.6M 2s
482650K .......... .......... .......... .......... .......... 94% 24.6M 2s
482700K .......... .......... .......... .......... .......... 94% 75.0M 2s
482750K .......... .......... .......... .......... .......... 94% 24.8M 2s
482800K .......... .......... .......... .......... .......... 94% 48.1M 2s
482850K .......... .......... .......... .......... .......... 94% 36.3M 2s
482900K .......... .......... .......... .......... .......... 94% 26.6M 2s
482950K .......... .......... .......... .......... .......... 94% 27.0M 2s
483000K .......... .......... .......... .......... .......... 95% 36.2M 2s
483050K .......... .......... .......... .......... .......... 95% 21.9M 2s
483100K .......... .......... .......... .......... .......... 95% 28.3M 2s
483150K .......... .......... .......... .......... .......... 95% 48.9M 2s
483200K .......... .......... .......... .......... .......... 95% 34.5M 2s
483250K .......... .......... .......... .......... .......... 95% 27.1M 2s
483300K .......... .......... .......... .......... .......... 95% 40.5M 2s
483350K .......... .......... .......... .......... .......... 95% 26.1M 2s
483400K .......... .......... .......... .......... .......... 95% 35.9M 2s
483450K .......... .......... .......... .......... .......... 95% 24.0M 2s
483500K .......... .......... .......... .......... .......... 95% 34.1M 2s
483550K .......... .......... .......... .......... .......... 95% 28.7M 2s
483600K .......... .......... .......... .......... .......... 95% 30.4M 2s
483650K .......... .......... .......... .......... .......... 95% 35.4M 2s
483700K .......... .......... .......... .......... .......... 95% 22.3M 2s
483750K .......... .......... .......... .......... .......... 95% 38.0M 2s
483800K .......... .......... .......... .......... .......... 95% 23.5M 2s
483850K .......... .......... .......... .......... .......... 95% 25.5M 2s
483900K .......... .......... .......... .......... .......... 95% 83.2M 2s
483950K .......... .......... .......... .......... .......... 95% 12.1M 2s
484000K .......... .......... .......... .......... .......... 95% 77.6M 2s
484050K .......... .......... .......... .......... .......... 95%  129M 2s
484100K .......... .......... .......... .......... .......... 95% 22.0M 2s
484150K .......... .......... .......... .......... .......... 95%  141M 2s
484200K .......... .......... .......... .......... .......... 95% 30.5M 2s
484250K .......... .......... .......... .......... .......... 95% 90.9M 2s
484300K .......... .......... .......... .......... .......... 95% 32.8M 2s
484350K .......... .......... .......... .......... .......... 95% 27.6M 2s
484400K .......... .......... .......... .......... .......... 95% 33.1M 2s
484450K .......... .......... .......... .......... .......... 95% 31.9M 2s
484500K .......... .......... .......... .......... .......... 95% 44.8M 2s
484550K .......... .......... .......... .......... .......... 95% 30.5M 2s
484600K .......... .......... .......... .......... .......... 95% 30.8M 2s
484650K .......... .......... .......... .......... .......... 95% 38.3M 2s
484700K .......... .......... .......... .......... .......... 95% 33.3M 2s
484750K .......... .......... .......... .......... .......... 95% 33.9M 2s
484800K .......... .......... .......... .......... .......... 95% 39.3M 2s
484850K .......... .......... .......... .......... .......... 95% 43.2M 2s
484900K .......... .......... .......... .......... .......... 95% 38.0M 2s
484950K .......... .......... .......... .......... .......... 95% 30.4M 2s
485000K .......... .......... .......... .......... .......... 95% 26.8M 2s
485050K .......... .......... .......... .......... .......... 95% 46.3M 2s
485100K .......... .......... .......... .......... .......... 95% 30.8M 2s
485150K .......... .......... .......... .......... .......... 95% 28.4M 2s
485200K .......... .......... .......... .......... .......... 95% 34.6M 2s
485250K .......... .......... .......... .......... .......... 95% 38.5M 2s
485300K .......... .......... .......... .......... .......... 95% 38.4M 2s
485350K .......... .......... .......... .......... .......... 95% 30.1M 2s
485400K .......... .......... .......... .......... .......... 95% 41.3M 2s
485450K .......... .......... .......... .......... .......... 95% 34.6M 2s
485500K .......... .......... .......... .......... .......... 95% 33.6M 2s
485550K .......... .......... .......... .......... .......... 95% 28.9M 2s
485600K .......... .......... .......... .......... .......... 95% 36.9M 2s
485650K .......... .......... .......... .......... .......... 95% 14.9M 2s
485700K .......... .......... .......... .......... .......... 95%  186M 2s
485750K .......... .......... .......... .......... .......... 95% 81.7M 2s
485800K .......... .......... .......... .......... .......... 95% 22.6M 2s
485850K .......... .......... .......... .......... .......... 95% 18.1M 2s
485900K .......... .......... .......... .......... .......... 95% 60.1M 2s
485950K .......... .......... .......... .......... .......... 95% 24.7M 2s
486000K .......... .......... .......... .......... .......... 95% 25.2M 2s
486050K .......... .......... .......... .......... .......... 95% 21.7M 2s
486100K .......... .......... .......... .......... .......... 95% 23.5M 2s
486150K .......... .......... .......... .......... .......... 95% 25.8M 2s
486200K .......... .......... .......... .......... .......... 95% 24.0M 2s
486250K .......... .......... .......... .......... .......... 95% 22.7M 2s
486300K .......... .......... .......... .......... .......... 95% 20.6M 2s
486350K .......... .......... .......... .......... .......... 95% 21.7M 2s
486400K .......... .......... .......... .......... .......... 95% 25.8M 2s
486450K .......... .......... .......... .......... .......... 95% 22.3M 2s
486500K .......... .......... .......... .......... .......... 95% 23.5M 2s
486550K .......... .......... .......... .......... .......... 95% 24.1M 2s
486600K .......... .......... .......... .......... .......... 95% 18.9M 2s
486650K .......... .......... .......... .......... .......... 95% 22.5M 2s
486700K .......... .......... .......... .......... .......... 95% 16.3M 2s
486750K .......... .......... .......... .......... .......... 95% 22.5M 2s
486800K .......... .......... .......... .......... .......... 95% 13.1M 2s
486850K .......... .......... .......... .......... .......... 95% 22.1M 2s
486900K .......... .......... .......... .......... .......... 95% 77.9M 2s
486950K .......... .......... .......... .......... .......... 95% 15.9M 2s
487000K .......... .......... .......... .......... .......... 95% 24.2M 2s
487050K .......... .......... .......... .......... .......... 95% 15.2M 2s
487100K .......... .......... .......... .......... .......... 95% 15.3M 2s
487150K .......... .......... .......... .......... .......... 95% 14.0M 2s
487200K .......... .......... .......... .......... .......... 95% 16.1M 2s
487250K .......... .......... .......... .......... .......... 95% 19.3M 2s
487300K .......... .......... .......... .......... .......... 95% 14.1M 2s
487350K .......... .......... .......... .......... .......... 95% 17.3M 2s
487400K .......... .......... .......... .......... .......... 95% 15.0M 2s
487450K .......... .......... .......... .......... .......... 95% 17.1M 2s
487500K .......... .......... .......... .......... .......... 95% 18.6M 2s
487550K .......... .......... .......... .......... .......... 95% 18.6M 2s
487600K .......... .......... .......... .......... .......... 95% 17.7M 1s
487650K .......... .......... .......... .......... .......... 95% 14.3M 1s
487700K .......... .......... .......... .......... .......... 95% 18.7M 1s
487750K .......... .......... .......... .......... .......... 95% 17.0M 1s
487800K .......... .......... .......... .......... .......... 95% 22.2M 1s
487850K .......... .......... .......... .......... .......... 95% 15.0M 1s
487900K .......... .......... .......... .......... .......... 95% 24.0M 1s
487950K .......... .......... .......... .......... .......... 95% 14.8M 1s
488000K .......... .......... .......... .......... .......... 95% 15.6M 1s
488050K .......... .......... .......... .......... .......... 96% 10.9M 1s
488100K .......... .......... .......... .......... .......... 96% 11.0M 1s
488150K .......... .......... .......... .......... .......... 96% 28.8M 1s
488200K .......... .......... .......... .......... .......... 96% 10.7M 1s
488250K .......... .......... .......... .......... .......... 96% 31.1M 1s
488300K .......... .......... .......... .......... .......... 96% 17.0M 1s
488350K .......... .......... .......... .......... .......... 96% 19.7M 1s
488400K .......... .......... .......... .......... .......... 96% 18.9M 1s
488450K .......... .......... .......... .......... .......... 96% 17.0M 1s
488500K .......... .......... .......... .......... .......... 96% 24.6M 1s
488550K .......... .......... .......... .......... .......... 96% 22.4M 1s
488600K .......... .......... .......... .......... .......... 96% 17.2M 1s
488650K .......... .......... .......... .......... .......... 96% 18.8M 1s
488700K .......... .......... .......... .......... .......... 96% 19.7M 1s
488750K .......... .......... .......... .......... .......... 96% 16.7M 1s
488800K .......... .......... .......... .......... .......... 96% 21.5M 1s
488850K .......... .......... .......... .......... .......... 96% 13.9M 1s
488900K .......... .......... .......... .......... .......... 96% 15.3M 1s
488950K .......... .......... .......... .......... .......... 96% 26.5M 1s
489000K .......... .......... .......... .......... .......... 96% 34.2M 1s
489050K .......... .......... .......... .......... .......... 96% 52.4M 1s
489100K .......... .......... .......... .......... .......... 96% 14.7M 1s
489150K .......... .......... .......... .......... .......... 96% 40.2M 1s
489200K .......... .......... .......... .......... .......... 96% 24.7M 1s
489250K .......... .......... .......... .......... .......... 96% 19.2M 1s
489300K .......... .......... .......... .......... .......... 96%  125M 1s
489350K .......... .......... .......... .......... .......... 96% 18.1M 1s
489400K .......... .......... .......... .......... .......... 96% 21.1M 1s
489450K .......... .......... .......... .......... .......... 96% 18.5M 1s
489500K .......... .......... .......... .......... .......... 96% 20.4M 1s
489550K .......... .......... .......... .......... .......... 96% 23.0M 1s
489600K .......... .......... .......... .......... .......... 96% 20.8M 1s
489650K .......... .......... .......... .......... .......... 96% 18.5M 1s
489700K .......... .......... .......... .......... .......... 96% 18.9M 1s
489750K .......... .......... .......... .......... .......... 96% 19.4M 1s
489800K .......... .......... .......... .......... .......... 96% 23.5M 1s
489850K .......... .......... .......... .......... .......... 96% 17.6M 1s
489900K .......... .......... .......... .......... .......... 96% 19.4M 1s
489950K .......... .......... .......... .......... .......... 96% 17.5M 1s
490000K .......... .......... .......... .......... .......... 96% 27.6M 1s
490050K .......... .......... .......... .......... .......... 96% 21.8M 1s
490100K .......... .......... .......... .......... .......... 96% 48.1M 1s
490150K .......... .......... .......... .......... .......... 96% 47.7M 1s
490200K .......... .......... .......... .......... .......... 96% 48.2M 1s
490250K .......... .......... .......... .......... .......... 96% 33.4M 1s
490300K .......... .......... .......... .......... .......... 96% 18.1M 1s
490350K .......... .......... .......... .......... .......... 96% 38.9M 1s
490400K .......... .......... .......... .......... .......... 96% 41.6M 1s
490450K .......... .......... .......... .......... .......... 96% 46.5M 1s
490500K .......... .......... .......... .......... .......... 96% 52.3M 1s
490550K .......... .......... .......... .......... .......... 96% 20.9M 1s
490600K .......... .......... .......... .......... .......... 96% 20.2M 1s
490650K .......... .......... .......... .......... .......... 96% 41.7M 1s
490700K .......... .......... .......... .......... .......... 96% 22.7M 1s
490750K .......... .......... .......... .......... .......... 96% 30.8M 1s
490800K .......... .......... .......... .......... .......... 96% 31.9M 1s
490850K .......... .......... .......... .......... .......... 96% 18.2M 1s
490900K .......... .......... .......... .......... .......... 96% 26.4M 1s
490950K .......... .......... .......... .......... .......... 96% 32.6M 1s
491000K .......... .......... .......... .......... .......... 96% 17.7M 1s
491050K .......... .......... .......... .......... .......... 96% 42.8M 1s
491100K .......... .......... .......... .......... .......... 96% 21.8M 1s
491150K .......... .......... .......... .......... .......... 96% 22.3M 1s
491200K .......... .......... .......... .......... .......... 96% 16.7M 1s
491250K .......... .......... .......... .......... .......... 96% 30.7M 1s
491300K .......... .......... .......... .......... .......... 96% 19.2M 1s
491350K .......... .......... .......... .......... .......... 96% 14.6M 1s
491400K .......... .......... .......... .......... .......... 96% 22.8M 1s
491450K .......... .......... .......... .......... .......... 96% 17.7M 1s
491500K .......... .......... .......... .......... .......... 96% 22.4M 1s
491550K .......... .......... .......... .......... .......... 96% 15.0M 1s
491600K .......... .......... .......... .......... .......... 96% 23.5M 1s
491650K .......... .......... .......... .......... .......... 96% 20.1M 1s
491700K .......... .......... .......... .......... .......... 96% 20.0M 1s
491750K .......... .......... .......... .......... .......... 96% 22.6M 1s
491800K .......... .......... .......... .......... .......... 96% 18.7M 1s
491850K .......... .......... .......... .......... .......... 96% 14.8M 1s
491900K .......... .......... .......... .......... .......... 96% 25.6M 1s
491950K .......... .......... .......... .......... .......... 96% 12.5M 1s
492000K .......... .......... .......... .......... .......... 96%  160M 1s
492050K .......... .......... .......... .......... .......... 96% 18.1M 1s
492100K .......... .......... .......... .......... .......... 96% 38.1M 1s
492150K .......... .......... .......... .......... .......... 96% 30.6M 1s
492200K .......... .......... .......... .......... .......... 96% 23.0M 1s
492250K .......... .......... .......... .......... .......... 96% 22.9M 1s
492300K .......... .......... .......... .......... .......... 96% 29.7M 1s
492350K .......... .......... .......... .......... .......... 96% 23.9M 1s
492400K .......... .......... .......... .......... .......... 96% 35.2M 1s
492450K .......... .......... .......... .......... .......... 96% 19.7M 1s
492500K .......... .......... .......... .......... .......... 96% 19.9M 1s
492550K .......... .......... .......... .......... .......... 96% 20.0M 1s
492600K .......... .......... .......... .......... .......... 96% 20.4M 1s
492650K .......... .......... .......... .......... .......... 96% 37.8M 1s
492700K .......... .......... .......... .......... .......... 96% 23.2M 1s
492750K .......... .......... .......... .......... .......... 96% 24.9M 1s
492800K .......... .......... .......... .......... .......... 96% 21.8M 1s
492850K .......... .......... .......... .......... .......... 96% 23.1M 1s
492900K .......... .......... .......... .......... .......... 96% 34.9M 1s
492950K .......... .......... .......... .......... .......... 96% 22.1M 1s
493000K .......... .......... .......... .......... .......... 96% 38.9M 1s
493050K .......... .......... .......... .......... .......... 96% 27.4M 1s
493100K .......... .......... .......... .......... .......... 96% 25.8M 1s
493150K .......... .......... .......... .......... .......... 97% 23.2M 1s
493200K .......... .......... .......... .......... .......... 97%  127M 1s
493250K .......... .......... .......... .......... .......... 97% 27.7M 1s
493300K .......... .......... .......... .......... .......... 97% 95.2M 1s
493350K .......... .......... .......... .......... .......... 97% 30.8M 1s
493400K .......... .......... .......... .......... .......... 97% 34.4M 1s
493450K .......... .......... .......... .......... .......... 97% 31.5M 1s
493500K .......... .......... .......... .......... .......... 97% 41.1M 1s
493550K .......... .......... .......... .......... .......... 97% 35.0M 1s
493600K .......... .......... .......... .......... .......... 97% 27.7M 1s
493650K .......... .......... .......... .......... .......... 97% 32.0M 1s
493700K .......... .......... .......... .......... .......... 97% 33.0M 1s
493750K .......... .......... .......... .......... .......... 97% 38.2M 1s
493800K .......... .......... .......... .......... .......... 97% 30.1M 1s
493850K .......... .......... .......... .......... .......... 97% 33.1M 1s
493900K .......... .......... .......... .......... .......... 97% 42.5M 1s
493950K .......... .......... .......... .......... .......... 97% 17.0M 1s
494000K .......... .......... .......... .......... .......... 97% 48.5M 1s
494050K .......... .......... .......... .......... .......... 97% 36.2M 1s
494100K .......... .......... .......... .......... .......... 97% 20.4M 1s
494150K .......... .......... .......... .......... .......... 97% 36.2M 1s
494200K .......... .......... .......... .......... .......... 97% 27.0M 1s
494250K .......... .......... .......... .......... .......... 97% 45.4M 1s
494300K .......... .......... .......... .......... .......... 97% 45.9M 1s
494350K .......... .......... .......... .......... .......... 97% 24.7M 1s
494400K .......... .......... .......... .......... .......... 97% 39.1M 1s
494450K .......... .......... .......... .......... .......... 97% 24.1M 1s
494500K .......... .......... .......... .......... .......... 97% 28.1M 1s
494550K .......... .......... .......... .......... .......... 97%  114M 1s
494600K .......... .......... .......... .......... .......... 97% 25.2M 1s
494650K .......... .......... .......... .......... .......... 97% 35.4M 1s
494700K .......... .......... .......... .......... .......... 97% 26.2M 1s
494750K .......... .......... .......... .......... .......... 97% 22.4M 1s
494800K .......... .......... .......... .......... .......... 97% 50.3M 1s
494850K .......... .......... .......... .......... .......... 97% 36.5M 1s
494900K .......... .......... .......... .......... .......... 97% 47.3M 1s
494950K .......... .......... .......... .......... .......... 97% 28.9M 1s
495000K .......... .......... .......... .......... .......... 97% 97.1M 1s
495050K .......... .......... .......... .......... .......... 97% 30.1M 1s
495100K .......... .......... .......... .......... .......... 97% 25.2M 1s
495150K .......... .......... .......... .......... .......... 97% 41.9M 1s
495200K .......... .......... .......... .......... .......... 97% 26.6M 1s
495250K .......... .......... .......... .......... .......... 97% 31.9M 1s
495300K .......... .......... .......... .......... .......... 97% 29.8M 1s
495350K .......... .......... .......... .......... .......... 97% 28.1M 1s
495400K .......... .......... .......... .......... .......... 97% 29.3M 1s
495450K .......... .......... .......... .......... .......... 97% 29.3M 1s
495500K .......... .......... .......... .......... .......... 97% 29.4M 1s
495550K .......... .......... .......... .......... .......... 97% 32.9M 1s
495600K .......... .......... .......... .......... .......... 97% 31.8M 1s
495650K .......... .......... .......... .......... .......... 97% 23.3M 1s
495700K .......... .......... .......... .......... .......... 97% 34.7M 1s
495750K .......... .......... .......... .......... .......... 97% 28.1M 1s
495800K .......... .......... .......... .......... .......... 97% 32.4M 1s
495850K .......... .......... .......... .......... .......... 97% 28.5M 1s
495900K .......... .......... .......... .......... .......... 97% 27.9M 1s
495950K .......... .......... .......... .......... .......... 97% 28.8M 1s
496000K .......... .......... .......... .......... .......... 97% 33.9M 1s
496050K .......... .......... .......... .......... .......... 97% 33.2M 1s
496100K .......... .......... .......... .......... .......... 97% 29.8M 1s
496150K .......... .......... .......... .......... .......... 97% 27.4M 1s
496200K .......... .......... .......... .......... .......... 97% 11.5M 1s
496250K .......... .......... .......... .......... .......... 97%  147M 1s
496300K .......... .......... .......... .......... .......... 97%  209M 1s
496350K .......... .......... .......... .......... .......... 97% 17.1M 1s
496400K .......... .......... .......... .......... .......... 97% 14.5M 1s
496450K .......... .......... .......... .......... .......... 97% 81.5M 1s
496500K .......... .......... .......... .......... .......... 97% 24.1M 1s
496550K .......... .......... .......... .......... .......... 97% 23.9M 1s
496600K .......... .......... .......... .......... .......... 97% 12.6M 1s
496650K .......... .......... .......... .......... .......... 97% 14.8M 1s
496700K .......... .......... .......... .......... .......... 97% 22.2M 1s
496750K .......... .......... .......... .......... .......... 97% 15.6M 1s
496800K .......... .......... .......... .......... .......... 97% 23.1M 1s
496850K .......... .......... .......... .......... .......... 97% 16.3M 1s
496900K .......... .......... .......... .......... .......... 97% 19.2M 1s
496950K .......... .......... .......... .......... .......... 97% 14.8M 1s
497000K .......... .......... .......... .......... .......... 97% 20.5M 1s
497050K .......... .......... .......... .......... .......... 97% 22.7M 1s
497100K .......... .......... .......... .......... .......... 97% 14.3M 1s
497150K .......... .......... .......... .......... .......... 97% 13.4M 1s
497200K .......... .......... .......... .......... .......... 97% 7.90M 1s
497250K .......... .......... .......... .......... .......... 97% 26.3M 1s
497300K .......... .......... .......... .......... .......... 97% 16.0M 1s
497350K .......... .......... .......... .......... .......... 97% 30.7M 1s
497400K .......... .......... .......... .......... .......... 97% 28.5M 1s
497450K .......... .......... .......... .......... .......... 97% 17.3M 1s
497500K .......... .......... .......... .......... .......... 97% 19.4M 1s
497550K .......... .......... .......... .......... .......... 97% 29.7M 1s
497600K .......... .......... .......... .......... .......... 97% 22.9M 1s
497650K .......... .......... .......... .......... .......... 97% 24.3M 1s
497700K .......... .......... .......... .......... .......... 97% 18.6M 1s
497750K .......... .......... .......... .......... .......... 97% 27.0M 1s
497800K .......... .......... .......... .......... .......... 97% 21.4M 1s
497850K .......... .......... .......... .......... .......... 97% 17.6M 1s
497900K .......... .......... .......... .......... .......... 97% 20.4M 1s
497950K .......... .......... .......... .......... .......... 97% 18.8M 1s
498000K .......... .......... .......... .......... .......... 97% 23.2M 1s
498050K .......... .......... .......... .......... .......... 97% 18.5M 1s
498100K .......... .......... .......... .......... .......... 97% 12.4M 1s
498150K .......... .......... .......... .......... .......... 97% 15.7M 1s
498200K .......... .......... .......... .......... .......... 97% 15.0M 1s
498250K .......... .......... .......... .......... .......... 98% 15.1M 1s
498300K .......... .......... .......... .......... .......... 98% 16.9M 1s
498350K .......... .......... .......... .......... .......... 98% 12.1M 1s
498400K .......... .......... .......... .......... .......... 98% 17.2M 1s
498450K .......... .......... .......... .......... .......... 98% 13.1M 1s
498500K .......... .......... .......... .......... .......... 98% 33.4M 1s
498550K .......... .......... .......... .......... .......... 98% 33.6M 1s
498600K .......... .......... .......... .......... .......... 98% 28.1M 1s
498650K .......... .......... .......... .......... .......... 98% 17.5M 1s
498700K .......... .......... .......... .......... .......... 98% 66.6M 1s
498750K .......... .......... .......... .......... .......... 98% 26.3M 1s
498800K .......... .......... .......... .......... .......... 98%  170M 1s
498850K .......... .......... .......... .......... .......... 98% 29.7M 1s
498900K .......... .......... .......... .......... .......... 98% 25.1M 1s
498950K .......... .......... .......... .......... .......... 98% 14.6M 1s
499000K .......... .......... .......... .......... .......... 98%  142M 1s
499050K .......... .......... .......... .......... .......... 98% 19.9M 1s
499100K .......... .......... .......... .......... .......... 98% 19.4M 1s
499150K .......... .......... .......... .......... .......... 98% 34.1M 1s
499200K .......... .......... .......... .......... .......... 98% 17.4M 1s
499250K .......... .......... .......... .......... .......... 98% 19.9M 1s
499300K .......... .......... .......... .......... .......... 98% 23.5M 1s
499350K .......... .......... .......... .......... .......... 98% 22.7M 1s
499400K .......... .......... .......... .......... .......... 98% 20.6M 1s
499450K .......... .......... .......... .......... .......... 98% 18.9M 1s
499500K .......... .......... .......... .......... .......... 98% 25.2M 1s
499550K .......... .......... .......... .......... .......... 98% 18.5M 1s
499600K .......... .......... .......... .......... .......... 98% 18.3M 1s
499650K .......... .......... .......... .......... .......... 98% 18.3M 1s
499700K .......... .......... .......... .......... .......... 98% 20.3M 1s
499750K .......... .......... .......... .......... .......... 98% 14.6M 1s
499800K .......... .......... .......... .......... .......... 98% 11.3M 1s
499850K .......... .......... .......... .......... .......... 98% 70.1M 1s
499900K .......... .......... .......... .......... .......... 98% 20.3M 1s
499950K .......... .......... .......... .......... .......... 98% 17.6M 1s
500000K .......... .......... .......... .......... .......... 98% 23.2M 1s
500050K .......... .......... .......... .......... .......... 98% 28.1M 1s
500100K .......... .......... .......... .......... .......... 98% 13.5M 1s
500150K .......... .......... .......... .......... .......... 98% 42.0M 1s
500200K .......... .......... .......... .......... .......... 98% 20.1M 1s
500250K .......... .......... .......... .......... .......... 98% 27.7M 1s
500300K .......... .......... .......... .......... .......... 98% 34.3M 1s
500350K .......... .......... .......... .......... .......... 98% 17.1M 1s
500400K .......... .......... .......... .......... .......... 98% 34.4M 1s
500450K .......... .......... .......... .......... .......... 98% 22.1M 1s
500500K .......... .......... .......... .......... .......... 98% 34.7M 1s
500550K .......... .......... .......... .......... .......... 98% 24.4M 1s
500600K .......... .......... .......... .......... .......... 98% 23.4M 1s
500650K .......... .......... .......... .......... .......... 98% 25.9M 1s
500700K .......... .......... .......... .......... .......... 98% 19.9M 1s
500750K .......... .......... .......... .......... .......... 98% 32.0M 1s
500800K .......... .......... .......... .......... .......... 98% 27.1M 1s
500850K .......... .......... .......... .......... .......... 98% 22.9M 1s
500900K .......... .......... .......... .......... .......... 98% 47.3M 1s
500950K .......... .......... .......... .......... .......... 98% 48.3M 1s
501000K .......... .......... .......... .......... .......... 98% 37.0M 1s
501050K .......... .......... .......... .......... .......... 98% 23.8M 1s
501100K .......... .......... .......... .......... .......... 98% 26.4M 1s
501150K .......... .......... .......... .......... .......... 98% 21.7M 1s
501200K .......... .......... .......... .......... .......... 98%  115M 1s
501250K .......... .......... .......... .......... .......... 98%  154M 1s
501300K .......... .......... .......... .......... .......... 98% 70.5M 1s
501350K .......... .......... .......... .......... .......... 98% 37.2M 1s
501400K .......... .......... .......... .......... .......... 98% 30.4M 0s
501450K .......... .......... .......... .......... .......... 98% 42.6M 0s
501500K .......... .......... .......... .......... .......... 98% 20.6M 0s
501550K .......... .......... .......... .......... .......... 98% 45.3M 0s
501600K .......... .......... .......... .......... .......... 98% 33.6M 0s
501650K .......... .......... .......... .......... .......... 98% 41.2M 0s
501700K .......... .......... .......... .......... .......... 98% 21.0M 0s
501750K .......... .......... .......... .......... .......... 98% 46.3M 0s
501800K .......... .......... .......... .......... .......... 98% 35.3M 0s
501850K .......... .......... .......... .......... .......... 98% 30.0M 0s
501900K .......... .......... .......... .......... .......... 98% 34.8M 0s
501950K .......... .......... .......... .......... .......... 98% 29.3M 0s
502000K .......... .......... .......... .......... .......... 98% 38.5M 0s
502050K .......... .......... .......... .......... .......... 98% 44.9M 0s
502100K .......... .......... .......... .......... .......... 98% 26.4M 0s
502150K .......... .......... .......... .......... .......... 98% 39.6M 0s
502200K .......... .......... .......... .......... .......... 98% 29.3M 0s
502250K .......... .......... .......... .......... .......... 98% 43.9M 0s
502300K .......... .......... .......... .......... .......... 98% 33.0M 0s
502350K .......... .......... .......... .......... .......... 98% 37.9M 0s
502400K .......... .......... .......... .......... .......... 98% 38.0M 0s
502450K .......... .......... .......... .......... .......... 98% 34.9M 0s
502500K .......... .......... .......... .......... .......... 98% 22.2M 0s
502550K .......... .......... .......... .......... .......... 98% 24.8M 0s
502600K .......... .......... .......... .......... .......... 98% 24.5M 0s
502650K .......... .......... .......... .......... .......... 98% 19.1M 0s
502700K .......... .......... .......... .......... .......... 98%  111M 0s
502750K .......... .......... .......... .......... .......... 98%  138M 0s
502800K .......... .......... .......... .......... .......... 98% 40.9M 0s
502850K .......... .......... .......... .......... .......... 98% 30.9M 0s
502900K .......... .......... .......... .......... .......... 98% 24.3M 0s
502950K .......... .......... .......... .......... .......... 98% 36.0M 0s
503000K .......... .......... .......... .......... .......... 98% 25.3M 0s
503050K .......... .......... .......... .......... .......... 98% 33.7M 0s
503100K .......... .......... .......... .......... .......... 98% 21.2M 0s
503150K .......... .......... .......... .......... .......... 98% 37.0M 0s
503200K .......... .......... .......... .......... .......... 98% 20.0M 0s
503250K .......... .......... .......... .......... .......... 98% 30.8M 0s
503300K .......... .......... .......... .......... .......... 99% 34.2M 0s
503350K .......... .......... .......... .......... .......... 99% 32.3M 0s
503400K .......... .......... .......... .......... .......... 99% 30.1M 0s
503450K .......... .......... .......... .......... .......... 99% 32.0M 0s
503500K .......... .......... .......... .......... .......... 99% 31.8M 0s
503550K .......... .......... .......... .......... .......... 99% 29.9M 0s
503600K .......... .......... .......... .......... .......... 99% 25.7M 0s
503650K .......... .......... .......... .......... .......... 99% 21.9M 0s
503700K .......... .......... .......... .......... .......... 99% 33.1M 0s
503750K .......... .......... .......... .......... .......... 99% 28.9M 0s
503800K .......... .......... .......... .......... .......... 99% 40.4M 0s
503850K .......... .......... .......... .......... .......... 99% 19.1M 0s
503900K .......... .......... .......... .......... .......... 99% 41.9M 0s
503950K .......... .......... .......... .......... .......... 99% 25.0M 0s
504000K .......... .......... .......... .......... .......... 99% 43.8M 0s
504050K .......... .......... .......... .......... .......... 99% 31.3M 0s
504100K .......... .......... .......... .......... .......... 99% 66.7M 0s
504150K .......... .......... .......... .......... .......... 99% 57.2M 0s
504200K .......... .......... .......... .......... .......... 99% 15.3M 0s
504250K .......... .......... .......... .......... .......... 99% 73.4M 0s
504300K .......... .......... .......... .......... .......... 99% 86.6M 0s
504350K .......... .......... .......... .......... .......... 99% 54.6M 0s
504400K .......... .......... .......... .......... .......... 99% 36.1M 0s
504450K .......... .......... .......... .......... .......... 99% 43.7M 0s
504500K .......... .......... .......... .......... .......... 99%  105M 0s
504550K .......... .......... .......... .......... .......... 99% 45.4M 0s
504600K .......... .......... .......... .......... .......... 99% 36.7M 0s
504650K .......... .......... .......... .......... .......... 99% 37.5M 0s
504700K .......... .......... .......... .......... .......... 99% 38.4M 0s
504750K .......... .......... .......... .......... .......... 99% 66.4M 0s
504800K .......... .......... .......... .......... .......... 99% 50.8M 0s
504850K .......... .......... .......... .......... .......... 99% 38.3M 0s
504900K .......... .......... .......... .......... .......... 99% 52.1M 0s
504950K .......... .......... .......... .......... .......... 99% 25.0M 0s
505000K .......... .......... .......... .......... .......... 99%  189M 0s
505050K .......... .......... .......... .......... .......... 99% 49.8M 0s
505100K .......... .......... .......... .......... .......... 99% 38.0M 0s
505150K .......... .......... .......... .......... .......... 99% 30.4M 0s
505200K .......... .......... .......... .......... .......... 99% 28.2M 0s
505250K .......... .......... .......... .......... .......... 99% 42.8M 0s
505300K .......... .......... .......... .......... .......... 99% 37.6M 0s
505350K .......... .......... .......... .......... .......... 99% 31.6M 0s
505400K .......... .......... .......... .......... .......... 99% 35.2M 0s
505450K .......... .......... .......... .......... .......... 99% 33.4M 0s
505500K .......... .......... .......... .......... .......... 99% 40.5M 0s
505550K .......... .......... .......... .......... .......... 99% 38.0M 0s
505600K .......... .......... .......... .......... .......... 99% 33.0M 0s
505650K .......... .......... .......... .......... .......... 99% 45.0M 0s
505700K .......... .......... .......... .......... .......... 99% 20.8M 0s
505750K .......... .......... .......... .......... .......... 99% 31.7M 0s
505800K .......... .......... .......... .......... .......... 99% 32.1M 0s
505850K .......... .......... .......... .......... .......... 99% 35.7M 0s
505900K .......... .......... .......... .......... .......... 99% 46.1M 0s
505950K .......... .......... .......... .......... .......... 99% 23.9M 0s
506000K .......... .......... .......... .......... .......... 99% 27.5M 0s
506050K .......... .......... .......... .......... .......... 99% 38.4M 0s
506100K .......... .......... .......... .......... .......... 99% 31.7M 0s
506150K .......... .......... .......... .......... .......... 99% 26.3M 0s
506200K .......... .......... .......... .......... .......... 99% 41.3M 0s
506250K .......... .......... .......... .......... .......... 99% 15.9M 0s
506300K .......... .......... .......... .......... .......... 99%  122M 0s
506350K .......... .......... .......... .......... .......... 99% 69.6M 0s
506400K .......... .......... .......... .......... .......... 99% 40.2M 0s
506450K .......... .......... .......... .......... .......... 99% 32.5M 0s
506500K .......... .......... .......... .......... .......... 99% 12.4M 0s
506550K .......... .......... .......... .......... .......... 99% 18.0M 0s
506600K .......... .......... .......... .......... .......... 99% 11.1M 0s
506650K .......... .......... .......... .......... .......... 99% 15.4M 0s
506700K .......... .......... .......... .......... .......... 99% 17.3M 0s
506750K .......... .......... .......... .......... .......... 99% 15.8M 0s
506800K .......... .......... .......... .......... .......... 99% 16.8M 0s
506850K .......... .......... .......... .......... .......... 99% 12.3M 0s
506900K .......... .......... .......... .......... .......... 99% 17.6M 0s
506950K .......... .......... .......... .......... .......... 99% 14.2M 0s
507000K .......... .......... .......... .......... .......... 99% 13.6M 0s
507050K .......... .......... .......... .......... .......... 99% 10.2M 0s
507100K .......... .......... .......... .......... .......... 99%  134M 0s
507150K .......... .......... .......... .......... .......... 99% 15.3M 0s
507200K .......... .......... .......... .......... .......... 99% 24.3M 0s
507250K .......... .......... .......... .......... .......... 99% 23.7M 0s
507300K .......... .......... .......... .......... .......... 99% 20.4M 0s
507350K .......... .......... .......... .......... .......... 99% 23.0M 0s
507400K .......... .......... .......... .......... .......... 99% 22.0M 0s
507450K .......... .......... .......... .......... .......... 99% 14.9M 0s
507500K .......... .......... .......... .......... .......... 99% 23.7M 0s
507550K .......... .......... .......... .......... .......... 99% 25.6M 0s
507600K .......... .......... .......... .......... .......... 99% 19.1M 0s
507650K .......... .......... .......... .......... .......... 99% 19.4M 0s
507700K .......... .......... .......... .......... .......... 99% 22.8M 0s
507750K .......... .......... .......... .......... .......... 99% 24.4M 0s
507800K .......... .......... .......... .......... .......... 99% 22.2M 0s
507850K .......... .......... .......... .......... .......... 99% 18.7M 0s
507900K .......... .......... .......... .......... .......... 99% 24.3M 0s
507950K .......... .......... .......... .......... .......... 99% 22.3M 0s
508000K .......... .......... .......... .......... .......... 99% 62.0M 0s
508050K .......... .......... .......... .......... .......... 99% 65.2M 0s
508100K .......... .......... .......... .......... .......... 99% 37.1M 0s
508150K .......... .......... .......... .......... .......... 99% 21.7M 0s
508200K .......... .......... .......... .......... .......... 99% 66.1M 0s
508250K .......... .......... .......... .......... .......... 99% 99.4M 0s
508300K .......... .......... .......... .......... .......... 99% 39.1M 0s
508350K .......... .......... .......... .......... .......... 99% 56.5M 0s
508400K .......... .......... ..........                      100% 24.6M=36s

2024-05-31 15:00:45 (13.8 MB/s) - ‘ESP125-macos-x86_64.tgz’ saved [520633019/520633019]

+ tar -xf ESP125-macos-x86_64.tgz
+ cd ESP125
+ rm -rf /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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/ESP125/EngSketchPad/ESP/esp_logo.png'.
Custom icon assigned to '/Users/jenkins/Desktop/runESP125.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/ESP/esp_logo.png'.
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/idle3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/pyftsubset'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/test_op4'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/ttx'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/wingproj'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/test_op2'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/pip3'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/test_bdf'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/undill'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/bdf'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/run_om_test'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/f90nml'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/webview'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/fonttools'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/openmdao'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/pyNastranGUI'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/f2py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/pydoc3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/2to3-3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/pip3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/test_pynastrangui'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/numba'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/normalizer'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/virtualenv'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/reset_notebook'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/abaqus_to_nastran'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/get_gprof'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/format_converter'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/pyftmerge'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/python3.11-config'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/f06'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/get_objgraph'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/lib/python3.11/config-3.11-darwin/Makefile'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/lib/python3.11/config-3.11-darwin/python-config.py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/lib/pkgconfig/python-3.11-embed.pc'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/lib/pkgconfig/python-3.11.pc'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/lib/python3.11/_sysconfigdata__darwin_darwin.py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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/ESP125.command /Users/jenkins/Desktop/runESP125.command
+ source /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=DARWIN64
++ ESP_ARCH=DARWIN64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad
++ ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad
++ export CASROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/OpenCASCADE-7.8.0
++ CASROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/OpenCASCADE-7.8.0
++ export CARARCH=.
++ CARARCH=.
++ export CASREV=7.8
++ CASREV=7.8
++ export PATH=.:/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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/ESP125/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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/ESP125/Python-3.11.9/include/python3.11
++ PYTHONINC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/include/python3.11
++ export 'PYTHONLIB=-L/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/lib -lpython3.11'
++ PYTHONLIB='-L/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/lib -lpython3.11'
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/lib:/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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/ESP125/EngSketchPad/lib:/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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/ESP125/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ export CAPS_GLYPH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ export 'SLUGS_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/SLUGS/Slugs.html'
++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/SLUGS/Slugs.html'
++ export 'ESP_START=open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/ESP/ESP-localhost7681.html'
++ ESP_START='open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/ESP/ESP-localhost7681.html'
++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/wvClient/wv.html'
++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/wvClient/wv.html'
+ which python
/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/Python-3.11.9/bin/python
+ python --version
Python 3.11.9
+ export CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data
+ CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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/ESP125/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/verify_7.8.0/expressions.vfy", so verification is being skipped
ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set)
ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set)
ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set)
==&gt; serveESP completed successfully with no verification data

real	0m4.788s
user	0m0.283s
sys	0m0.020s
+ set +x

=============================================
ESP verification case 01 passed (as expected)
=============================================

+ expectSuccess 02 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/verify_7.8.0/demo2.vfy", so verification is being skipped
==&gt; 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/ESP125/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/legacy/verify_7.8.0/tutorial1_whole.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m1.900s
user	0m3.051s
sys	0m0.758s
+ set +x

=============================================
ESP verification case 03 passed (as expected)
=============================================

+ expectSuccess 04 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/design2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/verify_7.8.0/design2.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.581s
user	0m0.640s
sys	0m0.054s
+ set +x

=============================================
ESP verification case 04 passed (as expected)
=============================================

+ expectSuccess 05 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/design3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/verify_7.8.0/design3.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.558s
user	0m0.726s
sys	0m0.078s
+ set +x

=============================================
ESP verification case 05 passed (as expected)
=============================================

+ expectSuccess 06 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/legacy/verify_7.8.0/tutorial2.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.588s
user	0m0.747s
sys	0m0.040s
+ set +x

=============================================
ESP verification case 06 passed (as expected)
=============================================

+ expectSuccess 07 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/legacy/verify_7.8.0/tutorial3.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m3.022s
user	0m4.951s
sys	0m0.649s
+ set +x

=============================================
ESP verification case 07 passed (as expected)
=============================================

+ expectSuccess 08 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/CAPS/verify_7.8.0/myPlane.vfy", so verification is being skipped
==&gt; serveESP completed successfully with 12 warnings and no verification data

real	0m18.185s
user	0m32.682s
sys	0m2.192s
+ set +x

=============================================
ESP verification case 08 passed (as expected)
=============================================

+ expectSuccess 09 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/bottle
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/verify_7.8.0/bottle.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.578s
user	0m0.688s
sys	0m0.030s
+ set +x

=============================================
ESP verification case 09 passed (as expected)
=============================================

+ expectSuccess 10 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/verify_7.8.0/wingMultiModel.vfy", so verification is being skipped
==&gt; serveESP completed successfully with 4 warnings and no verification data

real	0m22.018s
user	1m20.746s
sys	0m22.429s
+ set +x

=============================================
ESP verification case 10 passed (as expected)
=============================================

+ expectSuccess 11 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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
==&gt; serveESP completed successfully with 1 warnings and no verification data

real	0m0.719s
user	0m0.472s
sys	0m0.046s
+ set +x

=============================================
ESP verification case 11 passed (as expected)
=============================================

+ expectSuccess 12 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/verify_7.8.0/connect5.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.591s
user	0m0.785s
sys	0m0.018s
+ set +x

=============================================
ESP verification case 12 passed (as expected)
=============================================

+ expectSuccess 13 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/group2
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/verify_7.8.0/group2.vfy", so verification is being skipped
==&gt; serveESP completed successfully with no verification data

real	0m0.364s
user	0m0.399s
sys	0m0.017s
+ set +x

=============================================
ESP verification case 13 passed (as expected)
=============================================

+ expectSuccess 14 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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
==&gt; serveESP completed successfully with no verification data

real	0m0.726s
user	0m0.603s
sys	0m0.023s
+ set +x

=============================================
ESP verification case 14 passed (as expected)
=============================================

+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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 1.538s

OK
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/pyESP/testOCSM
+ source /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp

real	0m5.263s
user	0m7.391s
sys	0m0.185s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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
..........--&gt; 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 -&gt; __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _body (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _nface (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _body (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _nface (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _body (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _nface (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _body (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _nface (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __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 -&gt; __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _body (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _nface (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _body (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _nface (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _body (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _nface (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _body (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; _nface (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -&gt; __numRemaining__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.--&gt; 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 19.643s

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/ESP125/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          =     0.022   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          =     0.054   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          =     0.022   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4122      6020
AFLR2 GG : Nodes, Faces      =      5812      9400
AFLR2 GG : Nodes, Faces      =      7299     12374
AFLR2 GG : Nodes, Faces      =      8574     14924
AFLR2 GG : Nodes, Faces      =      9729     17234
AFLR2 GG : Nodes, Faces      =     10787     19350
AFLR2 GG : Nodes, Faces      =     11767     21310
AFLR2 GG : Nodes, Faces      =     12683     23142
AFLR2 GG : Nodes, Faces      =     13516     24808
AFLR2 GG : Nodes, Faces      =     14278     26332
AFLR2 GG : Nodes, Faces      =     14999     27774
AFLR2 GG : Nodes, Faces      =     15682     29140
AFLR2 GG : Nodes, Faces      =     16312     30400
AFLR2 GG : Nodes, Faces      =     16899     31574
AFLR2 GG : Nodes, Faces      =     17451     32678
AFLR2 GG : Nodes, Faces      =     17959     33694
AFLR2 GG : Nodes, Faces      =     18443     34662
AFLR2 GG : Nodes, Faces      =     18877     35530
AFLR2 GG : Nodes, Faces      =     19283     36342
AFLR2 GG : Nodes, Faces      =     19650     37076
AFLR2 GG : Nodes, Faces      =     19994     37764
AFLR2 GG : Nodes, Faces      =     20325     38426
AFLR2 GG : Nodes, Faces      =     20638     39052
AFLR2 GG : Nodes, Faces      =     20940     39656
AFLR2 GG : Nodes, Faces      =     21240     40256
AFLR2 GG : Nodes, Faces      =     21523     40822
AFLR2 GG : Nodes, Faces      =     21792     41360
AFLR2 GG : Nodes, Faces      =     22053     41882
AFLR2 GG : Nodes, Faces      =     22305     42386
AFLR2 GG : Nodes, Faces      =     22521     42818
AFLR2 GG : Nodes, Faces      =     22696     43168
AFLR2 GG : Nodes, Faces      =     22829     43434
AFLR2 GG : Nodes, Faces      =     22953     43682
AFLR2 GG : Nodes, Faces      =     23050     43876
AFLR2 GG : Nodes, Faces      =     23110     43996
AFLR2 GG : Nodes, Faces      =     23139     44054
AFLR2 GG : Nodes, Faces      =     23157     44090
AFLR2 GG : Nodes, Faces      =     23175     44126
AFLR2 GG : Nodes, Faces      =     23183     44142
AFLR2 GG : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.054   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.005   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
 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          =     0.021   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          =     0.049   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          =     0.048   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.004   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          =     0.052   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.004   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          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =       344       344
AFLR2 GG : Nodes, Faces      =       679      1014
AFLR2 GG : Nodes, Faces      =      1006      1668
AFLR2 GG : Nodes, Faces      =      1321      2298
AFLR2 GG : Nodes, Faces      =      1604      2864
AFLR2 GG : Nodes, Faces      =      1886      3428
AFLR2 GG : Nodes, Faces      =      2155      3966
AFLR2 GG : Nodes, Faces      =      2409      4474
AFLR2 GG : Nodes, Faces      =      2649      4954
AFLR2 GG : Nodes, Faces      =      2867      5390
AFLR2 GG : Nodes, Faces      =      3063      5782
AFLR2 GG : Nodes, Faces      =      3243      6142
AFLR2 GG : Nodes, Faces      =      3400      6456
AFLR2 GG : Nodes, Faces      =      3540      6736
AFLR2 GG : Nodes, Faces      =      3665      6986
AFLR2 GG : Nodes, Faces      =      3786      7228
AFLR2 GG : Nodes, Faces      =      3900      7456
AFLR2 GG : Nodes, Faces      =      4010      7676
AFLR2 GG : Nodes, Faces      =      4114      7884
AFLR2 GG : Nodes, Faces      =      4209      8074
AFLR2 GG : Nodes, Faces      =      4292      8240
AFLR2 GG : Nodes, Faces      =      4368      8392
AFLR2 GG : Nodes, Faces      =      4439      8534
AFLR2 GG : Nodes, Faces      =      4503      8662
AFLR2 GG : Nodes, Faces      =      4560      8776
AFLR2 GG : Nodes, Faces      =      4611      8878
AFLR2 GG : Nodes, Faces      =      4650      8956
AFLR2 GG : Nodes, Faces      =      4677      9010
AFLR2 GG : Nodes, Faces      =      4695      9046
AFLR2 GG : Nodes, Faces      =      4705      9066
 
AFLR2    : CPU Time          =     0.007   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          =     0.010   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4058      7772
AFLR2 QI : Nodes, Faces      =      4057       364
AFLR2 QI : Nodes, Faces      =      4057      3703
AFLR2 QI : Nodes, Faces      =      4057      7770
AFLR2 QI : Nodes, Faces      =      4056       344
AFLR2 QI : Nodes, Faces      =      4056      3712
AFLR2 QI : Nodes, Faces      =      4056      7768
AFLR2 QI : Nodes, Faces      =      4055       348
AFLR2 QI : Nodes, Faces      =      4055      3709
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       392
AFLR2 QI : Nodes, Faces      =      4055      3687
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
 
AFLR2    : CPU Time          =     0.004   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          =     0.010   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4058      7772
AFLR2 QI : Nodes, Faces      =      4057       364
AFLR2 QI : Nodes, Faces      =      4057      3703
AFLR2 QI : Nodes, Faces      =      4057      7770
AFLR2 QI : Nodes, Faces      =      4056       344
AFLR2 QI : Nodes, Faces      =      4056      3712
AFLR2 QI : Nodes, Faces      =      4056      7768
AFLR2 QI : Nodes, Faces      =      4055       348
AFLR2 QI : Nodes, Faces      =      4055      3709
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       392
AFLR2 QI : Nodes, Faces      =      4055      3687
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
 
AFLR2    : CPU Time          =     0.005   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:62030)
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:62030)
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:62030)
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:62030)
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:62030)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
 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:62030)
 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:62030)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
 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:62030)
 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:62030)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
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 &gt; autoInputs.out
 Executing: ./aero.csh &gt; 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  &gt; autoInputs.out
 Executing: ./aero.csh &gt; aero.out
 Executing: ./aero.csh &gt; 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  &gt; autoInputs.out
 Executing: ./aero.csh &gt; 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  &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:05:46) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:05:47) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:05:48) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:05:50) 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
   (15:05:51) Linearizing cut-cells
   (15:05:51) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:05:51) Computing gradients
   (15:05:59) ... 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
   (15:06:00) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:06:01) 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
   (15:06:02) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:06:03) 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
   (15:06:04) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:06:07) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (15:06:07) Linearizing cut-cells
   (15:06:07) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:06:07) Computing gradients
   (15:06:15) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:06:18) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:06:20) 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
   (15:06:21) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:06:23) 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
   (15:06:24) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:06:26) 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
   (15:06:27) Linearizing cut-cells
   (15:06:27) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:06:27) Computing gradients
   (15:06:31) ... 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
   (15:06:33) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:06:34) 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
   (15:06:36) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:06:37) 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
   (15:06:38) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:06:40) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (15:06:40) Linearizing cut-cells
   (15:06:40) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:06:40) Computing gradients
   (15:06:44) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:06:45) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:06:47) 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
   (15:06:48) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:06:49) 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
   (15:06:51) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:06:52) 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
   (15:06:52) Linearizing cut-cells
   (15:06:52) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:06:52) Computing gradients
   (15:06:57) ... 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
   (15:06:58) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:07:00) 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
   (15:07:01) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:07:02) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:07:03) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:07:05) 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
   (15:07:05) Linearizing cut-cells
   (15:07:05) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:07:05) Computing gradients
   (15:07:09) ... 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
   (15:07:10) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:07:12) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_M_y
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:07:13) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:07:14) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:07:15) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:07:16) 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
   (15:07:17) Linearizing cut-cells
   (15:07:17) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:07:17) Computing gradients
   (15:07:21) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:07:22) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:07:24) 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
   (15:07:25) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:07:26) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:07:27) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:07:28) 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
   (15:07:29) Linearizing cut-cells
   (15:07:29) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:07:29) Computing gradients
   (15:07:33) ... 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
   (15:07:34) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:07:35) 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  &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:07:38) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:07:39) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:07:40) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:07:43) 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
   (15:07:43) Linearizing cut-cells
   (15:07:45) ... done
   o Number of simultaneous xsensit jobs:  2
   (15:07:45) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (15:07:53) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:07:54) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (15:07:55) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
ok
test_Output_v5 (test_cbaero.TestCBAERO.test_Output_v5) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = Wing1, index = 1
	Name = trailingEdge, index = 2

Writing FAST file ....
Finished writing FAST file

Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_Output_v6 (test_cbaero.TestCBAERO.test_Output_v6) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
ok
test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
ok
test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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 -&gt; Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7FF8487D9780 EGADS Info: Face #3 -&gt; Edge #9 (9) Internally in Loop 7 4, sen = 1!
 70000AF51000 EGADS Info: Face #5 -&gt; Edge #17 (9) Internally in Loop 7 4, sen = -1!
 70000AF51000 EGADS Info: Face #5 -&gt; 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 -&gt; Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7FF8487D9780 EGADS Info: Face #3 -&gt; Edge #9 (9) Internally in Loop 7 4, sen = 1!
 70000AF51000 EGADS Info: Face #5 -&gt; Edge #17 (9) Internally in Loop 7 4, sen = -1!
 70000AF51000 EGADS Info: Face #5 -&gt; 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 -&gt; Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7FF8487D9780 EGADS Info: Face #3 -&gt; Edge #9 (9) Internally in Loop 7 4, sen = 1!
 70000AF51000 EGADS Info: Face #5 -&gt; Edge #17 (9) Internally in Loop 7 4, sen = -1!
 70000AF51000 EGADS Info: Face #5 -&gt; 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 -&gt; Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7FF8487D9780 EGADS Info: Face #3 -&gt; Edge #9 (9) Internally in Loop 7 4, sen = 1!
 70000AF51000 EGADS Info: Face #5 -&gt; Edge #17 (9) Internally in Loop 7 4, sen = -1!
 70000AF51000 EGADS Info: Face #5 -&gt; 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:62030)
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:62030)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
 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:62030)
 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:62030)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
 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:62030)
 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:62030)
 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:62030)
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:62030)
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:62030)
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:  0.11004
Creating surface mesh ...
Surface mesh seconds:  0.018616
Recovering boundaries...
Boundary recovery seconds:  0.089427
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.040137
Recovering Delaunayness...
Delaunay recovery seconds:  0.054033
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:  1.8604
Smoothing vertices...
Mesh smoothing seconds:  1.86786
Improving mesh...
Mesh improvement seconds:  0.046751

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.010934
Total running seconds:  4.09862

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:  0.134414
Creating surface mesh ...
Surface mesh seconds:  0.020061
Recovering boundaries...
Boundary recovery seconds:  0.092947
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.034114
Recovering Delaunayness...
Delaunay recovery seconds:  0.044856
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:  1.59161
Smoothing vertices...
Mesh smoothing seconds:  1.66349
Improving mesh...
Mesh improvement seconds:  0.038835

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.008837
Total running seconds:  3.62964

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/ESP125/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/ESP125/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/ESP125/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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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
===&gt; 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          =     0.016   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          =     0.164   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          =     5.223   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          =     1.755   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          =     0.096   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&gt;160.0   =        58
UG3      : No. Angle&gt;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&lt;TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 &lt;= Q &lt;= 1

UG3      : No. Tet Elems     =    414414
UG3      : Min, Max Q        =    0.0775         1
UG3      : Average Q         =     0.891
UG3      : No. Q&lt;       0.1  =        29
UG3      : No. Q&lt;      0.01  =         0

OVERALL  : CPU Time          =     7.508   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&gt;160.0   =        58
UG3      : No. Angle&gt;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&lt;TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 &lt;= Q &lt;= 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&lt;       0.1  =         0
UG3      : No. Q&lt;      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:62030)
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 -&gt; Edge #9 (9) Internally in Loop 4 7, sen = -1!
 70000AF51000 EGADS Info: Face #5 -&gt; Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7FF8487D9780 EGADS Info: Face #3 -&gt; Edge #9 (9) Internally in Loop 7 4, sen = 1!
 70000AF51000 EGADS Info: Face #5 -&gt; 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 -&gt; [0.345898, 1.652951, -0.041403]
	- weight -&gt; 476456.149985
	- weightMomentOfInertia -&gt; [304902.643270, 98963.803820, 69822.813290, 6179.981375, 19723.152207, 370546.335523]
ok

----------------------------------------------------------------------
Ran 144 tests in 660.323s

OK (skipped=10)
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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/ESP125/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./avlTest test;
+ ./avlTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m0.896s
user	0m0.527s
sys	0m0.157s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./avlTest passed (as expected)
=============================================


=================================================
+ echo './msesTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./msesTest test;
+ ./msesTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt


Attention: msesTest is hard coded to look for ../csmData/airfoilSection.csm

Value of CL = 0.276892 

real	0m1.659s
user	0m1.447s
sys	0m0.109s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./msesTest passed (as expected)
=============================================


=================================================
+ echo './frictionTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./frictionTest test;
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
+ ./frictionTest 0


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 , &gt;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	0m0.755s
user	0m0.363s
sys	0m0.056s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./frictionTest passed (as expected)
=============================================

Running.... MESH c-Tests
Running.... CFD c-Tests

=================================================
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
+ echo './fun3dAFLR2Test test;'
./fun3dAFLR2Test test;
+ ./fun3dAFLR2Test 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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          =     0.052   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          =     0.026   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	0m1.667s
user	0m1.245s
sys	0m0.420s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./fun3dAFLR2Test passed (as expected)
=============================================


=================================================
+ echo './fun3dTetgenTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./fun3dTetgenTest test;
+ ./fun3dTetgenTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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:  0.147327
Creating surface mesh ...
Surface mesh seconds:  0.023533
Recovering boundaries...
Boundary recovery seconds:  0.100815
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.036763
Recovering Delaunayness...
Delaunay recovery seconds:  0.055502
Refining mesh...
  21350 insertions, added 16804 points, 756241 tetrahedra in queue.
  7109 insertions, added 2842 points, 312650 tetrahedra in queue.
Refinement seconds:  1.34814
Smoothing vertices...
Mesh smoothing seconds:  1.90728
Improving mesh...
Mesh improvement seconds:  0.041233

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.010279
Total running seconds:  3.67137

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	0m6.606s
user	0m7.063s
sys	0m0.318s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./interferenceTest test;
+ ./interferenceTest
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m3.251s
user	0m5.502s
sys	0m0.121s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./interferenceTest passed (as expected)
=============================================


=================================================
+ echo './hsmCantileverPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmCantileverPlateTest test;
+ ./hsmCantileverPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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
-&gt;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	0m0.789s
user	0m0.559s
sys	0m0.069s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./hsmCantileverPlateTest passed (as expected)
=============================================


=================================================
+ echo './hsmSimplePlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmSimplePlateTest test;
+ ./hsmSimplePlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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
-&gt;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	0m1.100s
user	0m0.939s
sys	0m0.070s
+ status=0
+ set +x

=============================================
CAPS verification (using c-executables) case ./hsmSimplePlateTest passed (as expected)
=============================================


=================================================
+ echo './hsmJoinedPlateTest test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/cCAPSlog.txt
./hsmJoinedPlateTest test;
+ ./hsmJoinedPlateTest 0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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
-&gt;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	0m0.820s
user	0m0.508s
sys	0m0.073s
+ 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/ESP125/Python-3.11.9/bin/python
=================================================

No options provided...defaulting to ALL
Running.... LINEARAERO PyTests

avl: /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/bin/avl

=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m1.116s
user	0m0.735s
sys	0m0.499s
+ 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/ESP125/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/ESP125/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	0m11.373s
user	0m14.062s
sys	0m6.932s
+ 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/ESP125/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/ESP125/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	0m38.304s
user	0m16.158s
sys	0m20.872s
+ 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/ESP125/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/ESP125/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	0m1.291s
user	0m0.845s
sys	0m0.528s
+ 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/ESP125/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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing mass properties file: caps.mass
Parsing MassProp
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
EigenValues  {'case 1': [[0.48252996, 1.0092579], [0.48252996, -1.0092579], [-6.42569, 0.0], [-1.2733929, 0.0], [-0.0011487329, 0.0], [-1.2380479, 0.49321593], [-1.2380479, -0.49321593], [0.77888703, 0.0]]}

real	0m1.058s
user	0m0.695s
sys	0m0.459s
+ 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/ESP125/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/ESP125/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_&lt;=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-5.50424967] [2.89504288]

real	1m34.215s
user	0m4.616s
sys	0m1.669s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_OpenMDAO_3_PyTest.py passed (as expected)
=================================================

friction: /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/bin/friction

=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting Mach &amp; 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	0m0.685s
user	0m0.580s
sys	0m0.200s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m0.913s
user	0m0.617s
sys	0m0.191s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================

mses: /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/bin/mses

=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  0.3783793240300122
Cd =  0.007775858044231098
Cm =  0.005262576090314894

real	0m3.046s
user	0m2.563s
sys	0m0.317s
+ 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/ESP125/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/ESP125/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_&lt;=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-0.0002103]

real	0m17.342s
user	0m16.110s
sys	0m0.961s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case mses_OpenMDAO_3_PyTest.py passed (as expected)
=================================================

xfoil: /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/bin/xfoil

=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m3.027s
user	0m2.904s
sys	0m0.206s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m5.509s
user	0m17.440s
sys	0m6.631s
+ 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/ESP125/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/ESP125/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	0m3.771s
user	0m3.976s
sys	0m0.182s
+ 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/ESP125/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/ESP125/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	0m7.179s
user	0m9.967s
sys	0m0.301s
+ 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/ESP125/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/ESP125/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	0m2.651s
user	0m2.937s
sys	0m0.213s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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          =     0.012   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	0m0.854s
user	0m0.959s
sys	0m0.517s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_PyTest.py test;
+ python -u aflr4_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m1.092s
sys	0m0.269s
+ 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/ESP125/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/ESP125/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	0m2.357s
user	0m2.202s
sys	0m0.560s
+ 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/ESP125/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/ESP125/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	0m5.220s
user	0m9.255s
sys	0m0.679s
+ 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/ESP125/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/ESP125/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	0m6.977s
user	0m6.445s
sys	0m0.449s
+ 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/ESP125/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/ESP125/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	0m10.783s
user	0m10.113s
sys	0m0.539s
+ 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/ESP125/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/ESP125/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	0m26.762s
user	0m25.583s
sys	0m1.219s
+ 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/ESP125/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/ESP125/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	0m7.466s
user	0m18.124s
sys	0m4.717s
+ 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/ESP125/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/ESP125/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	0m12.988s
user	0m11.316s
sys	0m0.805s
+ 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/ESP125/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/ESP125/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          =     0.092   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:  0.011675
Creating surface mesh ...
Surface mesh seconds:  0.002951
Recovering boundaries...
Boundary recovery seconds:  0.006496
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000975
Recovering Delaunayness...
Delaunay recovery seconds:  0.001993
Refining mesh...
Refinement seconds:  0.013098
Smoothing vertices...
Mesh smoothing seconds:  0.02404
Improving mesh...
Mesh improvement seconds:  0.001582

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.000632
Total running seconds:  0.063643

Statistics:

  Input points: 1246
  Input facets: 2534
  Input segments: 3777
  Input holes: 0
  Input regions: 2

  Mesh points: 1455
  Mesh tetrahedra: 5105
  Mesh faces: 11319
  Mesh faces on exterior boundary: 2218
  Mesh faces on input facets: 2534
  Mesh edges on input segments: 3777
  Steiner points inside domain: 209

Done meshing using TetGen!

Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing Tecplot file ....
Finished writing Tecplot file


real	0m1.104s
user	0m0.871s
sys	0m0.309s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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:  0.022608
Creating surface mesh ...
Surface mesh seconds:  0.00786
Recovering boundaries...
Boundary recovery seconds:  0.058461
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.007899
Suppressing Steiner points ...
Steiner suppression seconds:  1.4e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.009641
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:  0.701865
Smoothing vertices...
Mesh smoothing seconds:  0.442973
Improving mesh...
Mesh improvement seconds:  0.010686
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.002868
Total running seconds:  1.26507

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	0m3.527s
user	0m2.818s
sys	0m0.423s
+ 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/ESP125/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/ESP125/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:  0.180995
Creating surface mesh ...
Surface mesh seconds:  0.013346
Recovering boundaries...
Boundary recovery seconds:  0.086657
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.010798
Recovering Delaunayness...
Delaunay recovery seconds:  0.045767
Refining mesh...
Refinement seconds:  0.211408
Smoothing vertices...
Mesh smoothing seconds:  0.297762
Improving mesh...
Mesh improvement seconds:  0.011459
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.004713
Total running seconds:  0.863649

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	0m2.286s
user	0m2.121s
sys	0m0.317s
+ 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/ESP125/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/ESP125/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:  0.179901
Creating surface mesh ...
Surface mesh seconds:  0.013491
Recovering boundaries...
Boundary recovery seconds:  0.089334
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.010443
Recovering Delaunayness...
Delaunay recovery seconds:  0.089447
Refining mesh...
Refinement seconds:  0.479675
Smoothing vertices...
Mesh smoothing seconds:  0.635811
Improving mesh...
Mesh improvement seconds:  0.016545

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.006221
Total running seconds:  1.52193

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	0m2.948s
user	0m2.766s
sys	0m0.313s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6

Getting mesh sizing parameters
	Mesh sizing name - Airfoil
	Mesh sizing name - AirfoilTE
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting edge discretization for body 1
	Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
	Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
	Writing out *.pts file
Reading delaundo mesh file - delaundo_CAPS.mesh
	Swapping y and z coordinates!

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


real	0m1.120s
user	0m1.012s
sys	0m0.488s
+ 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/ESP125/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/ESP125/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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  3.4617e-02|   -0.385358|    2.453598|    1.625650|    5.369499|    0.360138|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  3.3050e-02|   -0.512634|    2.087781|    1.374671|    4.973554|    1.183036|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  3.2569e-02|   -0.792582|    1.733529|    1.142729|    4.657622|    3.896320|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  3.3592e-02|   -0.880738|    1.486539|    1.023158|    4.334759|   14.592265|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  3.3722e-02|   -0.987528|    1.351478|    0.932491|    4.191092|  111.166022|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  3.4588e-02|   -1.104038|    1.188715|    0.874764|    3.951825| -483.924340|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  3.4607e-02|   -1.178622|    1.124587|    0.844310|    3.820426|  127.331200|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  3.5091e-02|   -1.243517|    1.097463|    0.824869|    3.768858|   40.162273|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  3.5064e-02|   -1.287932|    1.075843|    0.810639|    3.733440|   25.154653|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  3.4714e-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|         &lt; -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	0m2.498s
user	0m1.508s
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/ESP125/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/ESP125/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          =     0.035   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     11156     21767
AFLR2 QI : Nodes, Faces      =     11155       819
AFLR2 QI : Nodes, Faces      =     11155     10473
AFLR2 QI : Nodes, Faces      =     11155     21765
AFLR2 QI : Nodes, Faces      =     11154       811
AFLR2 QI : Nodes, Faces      =     11154     10476
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11154       805
AFLR2 QI : Nodes, Faces      =     11154     10479
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11154       911
AFLR2 QI : Nodes, Faces      =     11154     10426
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11153       915
AFLR2 QI : Nodes, Faces      =     11153     10423
AFLR2 QI : Nodes, Faces      =     11153       917
AFLR2 QI : Nodes, Faces      =     11153     10423
 
AFLR2    : CPU Time          =     0.014   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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  7.8919e-02|    0.071067|    2.739763|    1.616077|    5.599701|    0.055267|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  8.4505e-02|   -0.447576|    2.193837|    1.571349|    5.070382|    0.046028|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  8.3059e-02|   -0.561159|    2.074597|    1.490746|    4.953698|    0.033910|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  8.2745e-02|   -0.723326|    1.921155|    1.390756|    4.790278|    0.049695|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  8.3512e-02|   -0.876572|    1.825653|    1.275093|    4.637161|    0.133976|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  8.3888e-02|   -1.029177|    1.759196|    1.156078|    4.482282|    0.368542|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  8.3400e-02|   -1.215334|    1.704909|    1.114966|    4.286060|    0.974759|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  8.3103e-02|   -1.329970|    1.644937|    1.145030|    4.116982|    2.716332|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  8.4139e-02|   -1.270672|    1.570739|    1.155400|    4.139480|   16.569216|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  8.3528e-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|         &lt; -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_su2_aflr2.dat  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|CSV file                           |surface_flow_pyCAPS_su2_aflr2.csv  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary                     |flow_pyCAPS_su2_aflr2.szplt        |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary surface             |surface_flow_pyCAPS_su2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 994 more values.0: Error finishing Tecplot file output.

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

Total Force - Pressure + Viscous
Cl =  0.072253 Cd =  -0.01151
Cmz =  0.070975
Cx =  -0.01151 Cy =  0.072253
Pressure Contribution
Cl_p =  0.072253 Cd_p =  -0.01151
Cmz_p =  0.070975
Cx_p =  -0.01151 Cy_p =  0.072253
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0

real	0m4.172s
user	0m2.380s
sys	0m0.928s
+ 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/ESP125/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/ESP125/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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  1.2168e+00|   -0.064586|    2.297676|    2.033300|    5.426310|    1.967108|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.1657e+00|   -0.028142|    2.443813|    2.177084|    5.469820|    2.669025|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.1475e+00|    0.006388|    2.521945|    2.416533|    5.497519|    4.072698|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.1518e+00|   -0.032771|    2.543134|    2.541766|    5.444377|    5.959388|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.1435e+00|   -0.059484|    2.561671|    2.593774|    5.414288|    7.593451|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.1409e+00|   -0.076814|    2.565225|    2.615896|    5.407625|    8.782803|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.1274e+00|   -0.111978|    2.544207|    2.636258|    5.381265|    9.653546|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.1210e+00|   -0.156369|    2.495539|    2.651467|    5.333878|   10.185394|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.1210e+00|   -0.203072|    2.428150|    2.650114|    5.275471|   10.322264|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.1208e+00|   -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|          &lt; -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	0m45.095s
user	0m36.930s
sys	0m1.321s
+ 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/ESP125/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/ESP125/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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  1.6365e+00|   -0.457870|    1.873279|    1.656710|    5.033025|    0.755651|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.6121e+00|   -0.472284|    2.010746|    1.748231|    5.024932|    1.425370|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.6004e+00|   -0.414217|    2.107665|    1.963200|    5.074925|    3.245288|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.5701e+00|   -0.400337|    2.167522|    2.099318|    5.078948|    7.034217|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.5672e+00|   -0.401529|    2.203755|    2.175567|    5.071313|   12.883621|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.5756e+00|   -0.407291|    2.221380|    2.217144|    5.067540|   20.159074|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.5532e+00|   -0.411436|    2.211548|    2.246056|    5.067163|   27.796880|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.5596e+00|   -0.418757|    2.160924|    2.267618|    5.055632|   32.034412|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.5585e+00|   -0.438528|    2.092229|    2.272883|    5.027335|   30.335774|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.5590e+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|          &lt; -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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- 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 12.568842 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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  1.8752e+00|   -0.397349|    1.978876|    1.645486|    5.093547|    1.917484|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.8101e+00|   -0.252045|    2.234760|    1.970250|    5.252026|    2.558863|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.7520e+00|   -0.196042|    2.339633|    2.224120|    5.301659|    3.948869|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.7320e+00|   -0.220076|    2.386540|    2.365409|    5.264943|    5.948479|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.7796e+00|   -0.253573|    2.408600|    2.430554|    5.223815|    7.864579|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.7864e+00|   -0.270783|    2.418936|    2.458803|    5.218653|    9.389224|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.7864e+00|   -0.286712|    2.403031|    2.476999|    5.213229|   10.603736|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.7854e+00|   -0.315381|    2.351751|    2.489815|    5.182543|   11.481006|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.7991e+00|   -0.352500|    2.274582|    2.487389|    5.133384|   11.951691|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.8101e+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|          &lt; -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	1m16.583s
user	1m10.179s
sys	0m4.430s
+ 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/ESP125/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/ESP125/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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  8.1926e-02|   -1.163171|    1.073770|    1.341444|    4.312165|    0.062120|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  8.2066e-02|   -1.561828|    0.808636|    0.967487|    3.922716|    0.139775|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  7.8252e-02|   -1.601698|    0.943793|    1.009036|    3.876382|    0.373708|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  7.7756e-02|   -1.659374|    1.008221|    1.015635|    3.799753|    0.952935|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  7.9144e-02|   -1.663585|    1.011627|    0.956487|    3.788246|    2.344781|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  7.8247e-02|   -1.633451|    0.991734|    0.872954|    3.829708|    6.259549|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  7.8580e-02|   -1.626398|    0.990123|    0.847075|    3.843511|   26.349556|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  7.9680e-02|   -1.643439|    1.009125|    0.895796|    3.825758|  -56.104876|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  8.0816e-02|   -1.659565|    1.020774|    0.939260|    3.804303|  -24.431167|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  8.1162e-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|         &lt; -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	0m3.050s
user	0m2.180s
sys	0m0.805s
+ 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/ESP125/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/ESP125/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:  0.025261
Creating surface mesh ...
Surface mesh seconds:  0.008814
Recovering boundaries...
Boundary recovery seconds:  0.092077
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.011099
Suppressing Steiner points ...
Steiner suppression seconds:  1.9e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.013132
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:  0.949618
Smoothing vertices...
Mesh smoothing seconds:  0.612198
Improving mesh...
Mesh improvement seconds:  0.01612
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.00368
Total running seconds:  1.73251

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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  2.1725e-01|    0.617984|    3.049944|    2.093190|    6.108879|    1.810742|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.2647e-01|    0.748911|    3.251769|    2.987153|    6.248586|    2.155825|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.4261e-01|    0.688623|    3.311837|    3.249508|    6.186781|    3.173369|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  2.5015e-01|    0.587426|    3.265724|    3.310895|    6.060983|    4.532123|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  2.5517e-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|         &lt; -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	0m16.832s
user	0m16.037s
sys	0m0.827s
+ 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/ESP125/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/ESP125/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:  0.067454
Creating surface mesh ...
Surface mesh seconds:  0.02473
Recovering boundaries...
Warning:  6 segments are not recovered.
Boundary recovery seconds:  0.230102
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.020963
Suppressing Steiner points ...
Steiner suppression seconds:  2e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.027842
Refining mesh...
  12618 insertions, added 5274 points, 8959 tetrahedra in queue.
Refinement seconds:  0.723668
Smoothing vertices...
Mesh smoothing seconds:  0.614155
Improving mesh...
Mesh improvement seconds:  0.018773
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.007439
Total running seconds:  1.74059

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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  3.9785e-01|    2.730957|    5.664998|    4.728682|    8.730433|   -0.398804|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  4.1104e-01|    3.137446|    6.177776|    5.665282|    9.126833|   -0.137986|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  4.1082e-01|    3.221739|    6.293564|    5.717532|    9.173826|   -0.037061|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  4.0420e-01|    3.189146|    6.230574|    5.640455|    9.149183|   -0.012053|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  3.9917e-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|         &lt; -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	0m10.956s
user	0m12.903s
sys	0m1.462s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ python -u cart3d_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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  &gt; autoInputs.out
 Executing: ./aero.csh &gt; 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	0m20.885s
user	0m37.409s
sys	0m0.958s
+ 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/ESP125/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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
----------------------------------------
&gt;&gt;&gt; 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 &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:21:50) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (15:21:53) aero.csh done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [0.01631562]  CL 0.12773309
----------------------------------------
----------------------------------------
&gt;&gt;&gt; alpha [2.]
&gt;&gt;&gt; CL2 [0.01631562]  CL 0.12773309
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:21:54) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (15:21:58) 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
   (15:21:58) Linearizing cut-cells
   (15:21:58) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:21:58) Computing gradients
   (15:22:02) ... done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; 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
----------------------------------------
&gt;&gt;&gt; alpha [1.98427373]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:22:04) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1
   (15:22:06) aero.csh done
 o case M0.5901A1.98427B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [0.01606724]  CL 0.12675617
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:22:08) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1
   (15:22:11) 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
   (15:22:11) Linearizing cut-cells
   (15:22:11) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:22:11) Computing gradients
   (15:22:16) ... done
 o case M0.5901A1.98427B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_alpha [[0.01560329]]
========================================

At iterate    1    f=  1.60672D-02    |proj g|=  1.56033D-02
----------------------------------------
&gt;&gt;&gt; alpha [-0.01099175]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:22:17) Running aero.csh on 2 core(s) in M0.5901A-0.0109918B0_DP1
   (15:22:20) aero.csh done
 o case M0.5901A-0.0109918B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [6.05653687e-06]  CL 0.00246101
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:22:21) Running aero.csh on 2 core(s) in M0.5901A-0.0109918B0_DP1
   (15:22:25) 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
   (15:22:25) Linearizing cut-cells
   (15:22:25) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:22:25) Computing gradients
   (15:22:29) ... done
 o case M0.5901A-0.0109918B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_alpha [[0.00031042]]
========================================

At iterate    2    f=  6.05654D-06    |proj g|=  3.10424D-04
----------------------------------------
&gt;&gt;&gt; alpha [-0.05149286]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:22:31) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1
   (15:22:33) aero.csh done
 o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [2.59817201e-10]  CL 1.612e-05
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:22:35) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1
   (15:22:38) 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
   (15:22:39) Linearizing cut-cells
   (15:22:39) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:22:39) Computing gradients
   (15:22:43) ... done
 o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_alpha [[2.03612486e-06]]
========================================

At iterate    3    f=  2.59817D-10    |proj g|=  2.03612D-06
----------------------------------------
&gt;&gt;&gt; alpha [-0.05176027]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:22:44) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1
   (15:22:47) aero.csh done
 o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [9.26120217e-15]  CL 1e-07
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:22:48) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1
   (15:22:53) 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
   (15:22:53) Linearizing cut-cells
   (15:22:53) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:22:53) Computing gradients
   (15:22:57) ... done
 o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; 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_&lt;=_PGTOL            
Optimization Complete
-----------------------------------
Optimized value: [-0.05176027]

real	1m13.933s
user	0m55.252s
sys	0m11.497s
+ 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/ESP125/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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
----------------------------------------
&gt;&gt;&gt; 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 &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:23:02) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (15:23:20) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [0.00411365]  CL 0.0641354
----------------------------------------
----------------------------------------
&gt;&gt;&gt; twist [4.]
&gt;&gt;&gt; CL2 [0.00411365]  CL 0.0641354
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:23:22) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (15:23:48) 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
   (15:23:48) Linearizing cut-cells
   (15:23:50) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:23:50) Computing gradients
   (15:23:54) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; 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
----------------------------------------
&gt;&gt;&gt; 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 &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:23:57) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (15:24:15) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [0.0041123]  CL 0.0641197
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:24:17) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (15:24:42) 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
   (15:24:43) Linearizing cut-cells
   (15:24:45) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:24:45) Computing gradients
   (15:24:49) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_twist [[0.00210014]]
========================================

At iterate    1    f=  4.11230D-03    |proj g|=  2.10014D-03
----------------------------------------
&gt;&gt;&gt; twist [-6.47168778]
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 &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:24:51) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (15:25:09) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [0.00980712]  CL -0.0990178
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:25:11) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (15:25:38) 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
   (15:25:39) Linearizing cut-cells
   (15:25:41) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:25:41) Computing gradients
   (15:25:45) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_twist [[-0.00318447]]
========================================
----------------------------------------
&gt;&gt;&gt; twist [-0.15773815]
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 &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:25:48) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (15:26:06) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [2.57282943e-07]  CL -0.00057627
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:26:08) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (15:26:34) 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
   (15:26:35) Linearizing cut-cells
   (15:26:37) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:26:37) Computing gradients
   (15:26:41) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_twist [[-1.67854775e-05]]
========================================

At iterate    2    f=  2.57283D-07    |proj g|=  1.67855D-05
----------------------------------------
&gt;&gt;&gt; twist [-0.12478737]
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 &gt; autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:26:43) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (15:27:01) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2 [1.79305026e-08]  CL 0.00016606
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (15:27:03) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (15:27:29) 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
   (15:27:30) Linearizing cut-cells
   (15:27:32) ... done
   o Number of simultaneous xsensit jobs:  1
   (15:27:32) Computing gradients
   (15:27:36) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
&gt;&gt;&gt; CL2_twist [[4.43472912e-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 =   1.7930502629000000E-008

CONVERGENCE: REL_REDUCTION_OF_F_&lt;=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-0.12478737]

real	4m38.980s
user	7m15.990s
sys	0m13.615s
+ 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/ESP125/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/ESP125/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	0m11.933s
user	0m10.265s
sys	0m0.967s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m5.965s
user	0m11.125s
sys	0m7.280s
+ 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/ESP125/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/ESP125/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	0m0.705s
user	0m0.579s
sys	0m0.226s
+ 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/ESP125/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/ESP125/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
-&gt;HSMSOL
 Matrix Non-zero Entries = 5741

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.130E-01  0.165E+00  0.153E-04    1.000  ddy @ (   0.25   0.06   0.00)
   1*   0.260E-03  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.12   0.00)
   1*   0.240E-05  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.09   0.00)
   2    0.379E-02  0.505E-01  0.750E-04    1.000  ddy @ (   0.25   0.19   0.00)
   2*   0.420E-04  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.12   0.00)
   3    0.168E-02  0.225E-01  0.208E-04    1.000  ddy @ (   0.25   0.06   0.00)
   4    0.325E-03  0.427E-02  0.250E-05    1.000  ddy @ (   0.25   0.19   0.00)
   5    0.794E-05  0.112E-03  0.170E-06    1.000  ddy @ (   0.25   0.19   0.00)
   6    0.387E-08  0.598E-07  0.197E-09    1.000  ddy @ (   0.25   0.06   0.00)
   7    0.848E-15  0.147E-13  0.924E-15    1.000  ddy @ (   0.25   0.19   0.00)

 Converging n vectors ...
 it =  1    dn =  0.788E-01   rlx = 1.000  (  59 )
 it =  2    dn =  0.566E-16   rlx = 1.000  (  35 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.691E-03   rlx = 1.000  (  45 )
 it =  2    de =  0.404E-04   rlx = 1.000  (   9 )
 it =  3    de =  0.142E-07   rlx = 1.000  (  46 )
 it =  4    de =  0.521E-11   rlx = 1.000  (  62 )

 Calculating  strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat

real	0m1.072s
user	0m0.960s
sys	0m0.170s
+ 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/ESP125/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/ESP125/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
-&gt;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	0m0.892s
user	0m0.835s
sys	0m0.170s
+ 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/ESP125/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/ESP125/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	0m10.984s
user	0m20.118s
sys	0m5.613s
+ 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/ESP125/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/ESP125/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	0m0.939s
user	0m0.708s
sys	0m0.295s
+ 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/ESP125/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/ESP125/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	0m1.170s
user	0m0.812s
sys	0m0.326s
+ 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/ESP125/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/ESP125/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	0m37.106s
user	0m36.143s
sys	0m0.961s
+ 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/ESP125/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/ESP125/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	0m1.584s
user	0m1.065s
sys	0m0.479s
+ 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/ESP125/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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 16
	Number of elements = 9
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 9
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 5
	Load name - load_0
	Load name - load_1
	Load name - load_2
	Load name - load_3
	Load name - load_4
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 5
	Analysis name - load_0
	Analysis name - load_1
	Analysis name - load_2
	Analysis name - load_3
	Analysis name - load_4
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_2, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_3, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_4, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL

real	0m1.208s
user	0m0.921s
sys	0m0.383s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_PyTest.py test;
+ python -u astros_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m15.886s
user	0m21.039s
sys	0m8.216s
+ 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/ESP125/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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 6
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 6
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL

real	0m1.512s
user	0m0.884s
sys	0m0.405s
+ 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/ESP125/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/ESP125/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	0m1.197s
user	0m0.883s
sys	0m0.382s
+ 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/ESP125/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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedForce
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control

Getting FEA design variables.......
	Number of design variables          - 3
	Design_Variable name - Bar1A
	Design_Variable name - Bar2A
	Design_Variable name - Bar3A
	Design_Variable_Relation name - Bar1A
	Design_Variable_Relation name - Bar2A
	Design_Variable_Relation name - Bar3A
	Number of design variable relations - 3
	Done getting FEA design variables

Getting FEA design constraints.......
	Number of design constraints - 3
	Design_Constraint name - stress1
	Design_Constraint name - stress2
	Design_Constraint name - stress3
Done getting FEA design constraints

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - SingleLoadCase
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing design constraint cards
	Writing load cards
	Writing material cards
	Writing property cards
	Writing design variable cards


Running Astros......
Done running Astros!

real	0m1.326s
user	0m0.952s
sys	0m0.390s
+ 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/ESP125/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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 2
	Constraint name - conOne
	No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement"
	Constraint name - conTwo
	No "constraintType" specified for Constraint tuple conTwo, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 2
	Load name - loadOne
	Load name - loadTwo
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 2
	Analysis name - analysisOne
	Analysis name - analysisTwo
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards

real	0m1.124s
user	0m0.864s
sys	0m0.370s
+ 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/ESP125/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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedForce
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - SingleLoadCase
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards

real	0m1.107s
user	0m0.856s
sys	0m0.376s
+ 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/ESP125/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/ESP125/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	0m1.535s
user	0m1.123s
sys	0m0.470s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Trim_15degree.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_AGARD445_PyTest.py test;
+ python -u nastran_AGARD445_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = yatesPlate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 49
Number of elements = 36
Number of triangle elements      = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes    = 49
Total number of elements = 36
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = constEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 49
	Number of elements = 36
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 36
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Mahogany
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - yatesPlate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Warning: No loads specified for case EigenAnalysis!!!!
	Writing mass increment cards
	Writing analysis cards, 0
	Writing combined constraint cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

Getting results natural frequencies.....
Reading Nastran FO6 file - extracting Eigen-Values!
	Number of Eigen-Values = 132
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
	Loading Eigen-Value = 4
	Loading Eigen-Value = 5
	Loading Eigen-Value = 6
	Loading Eigen-Value = 7
	Loading Eigen-Value = 8
	Loading Eigen-Value = 9
	Loading Eigen-Value = 10
	Loading Eigen-Value = 11
	Loading Eigen-Value = 12
	Loading Eigen-Value = 13
	Loading Eigen-Value = 14
	Loading Eigen-Value = 15
	Loading Eigen-Value = 16
	Loading Eigen-Value = 17
	Loading Eigen-Value = 18
	Loading Eigen-Value = 19
	Loading Eigen-Value = 20
	Loading Eigen-Value = 21
	Loading Eigen-Value = 22
	Loading Eigen-Value = 23
	Loading Eigen-Value = 24
	Loading Eigen-Value = 25
	Loading Eigen-Value = 26
	Loading Eigen-Value = 27
	Loading Eigen-Value = 28
	Loading Eigen-Value = 29
	Loading Eigen-Value = 30
	Loading Eigen-Value = 31
	Loading Eigen-Value = 32
	Loading Eigen-Value = 33
	Loading Eigen-Value = 34
	Loading Eigen-Value = 35
	Loading Eigen-Value = 36
	Loading Eigen-Value = 37
	Loading Eigen-Value = 38
	Loading Eigen-Value = 39
	Loading Eigen-Value = 40
	Loading Eigen-Value = 41
	Loading Eigen-Value = 42
	Loading Eigen-Value = 43
	Loading Eigen-Value = 44
	Loading Eigen-Value = 45
	Loading Eigen-Value = 46
	Loading Eigen-Value = 47
	Loading Eigen-Value = 48
	Loading Eigen-Value = 49
	Loading Eigen-Value = 50
	Loading Eigen-Value = 51
	Loading Eigen-Value = 52
	Loading Eigen-Value = 53
	Loading Eigen-Value = 54
	Loading Eigen-Value = 55
	Loading Eigen-Value = 56
	Loading Eigen-Value = 57
	Loading Eigen-Value = 58
	Loading Eigen-Value = 59
	Loading Eigen-Value = 60
	Loading Eigen-Value = 61
	Loading Eigen-Value = 62
	Loading Eigen-Value = 63
	Loading Eigen-Value = 64
	Loading Eigen-Value = 65
	Loading Eigen-Value = 66
	Loading Eigen-Value = 67
	Loading Eigen-Value = 68
	Loading Eigen-Value = 69
	Loading Eigen-Value = 70
	Loading Eigen-Value = 71
	Loading Eigen-Value = 72
	Loading Eigen-Value = 73
	Loading Eigen-Value = 74
	Loading Eigen-Value = 75
	Loading Eigen-Value = 76
	Loading Eigen-Value = 77
	Loading Eigen-Value = 78
	Loading Eigen-Value = 79
	Loading Eigen-Value = 80
	Loading Eigen-Value = 81
	Loading Eigen-Value = 82
	Loading Eigen-Value = 83
	Loading Eigen-Value = 84
	Loading Eigen-Value = 85
	Loading Eigen-Value = 86
	Loading Eigen-Value = 87
	Loading Eigen-Value = 88
	Loading Eigen-Value = 89
	Loading Eigen-Value = 90
	Loading Eigen-Value = 91
	Loading Eigen-Value = 92
	Loading Eigen-Value = 93
	Loading Eigen-Value = 94
	Loading Eigen-Value = 95
	Loading Eigen-Value = 96
	Loading Eigen-Value = 97
	Loading Eigen-Value = 98
	Loading Eigen-Value = 99
	Loading Eigen-Value = 100
	Loading Eigen-Value = 101
	Loading Eigen-Value = 102
	Loading Eigen-Value = 103
	Loading Eigen-Value = 104
	Loading Eigen-Value = 105
	Loading Eigen-Value = 106
	Loading Eigen-Value = 107
	Loading Eigen-Value = 108
	Loading Eigen-Value = 109
	Loading Eigen-Value = 110
	Loading Eigen-Value = 111
	Loading Eigen-Value = 112
	Loading Eigen-Value = 113
	Loading Eigen-Value = 114
	Loading Eigen-Value = 115
	Loading Eigen-Value = 116
	Loading Eigen-Value = 117
	Loading Eigen-Value = 118
	Loading Eigen-Value = 119
	Loading Eigen-Value = 120
	Loading Eigen-Value = 121
	Loading Eigen-Value = 122
	Loading Eigen-Value = 123
	Loading Eigen-Value = 124
	Loading Eigen-Value = 125
	Loading Eigen-Value = 126
	Loading Eigen-Value = 127
	Loading Eigen-Value = 128
	Loading Eigen-Value = 129
	Loading Eigen-Value = 130
	Loading Eigen-Value = 131
	Loading Eigen-Value = 132
Natural freq (Mode 0) = 9.44 (Hz)
Natural freq (Mode 1) = 35.99 (Hz)
Natural freq (Mode 2) = 50.58 (Hz)
Natural freq (Mode 3) = 93.48 (Hz)
Natural freq (Mode 4) = 122.58 (Hz)
Natural freq (Mode 5) = 142.96 (Hz)
Natural freq (Mode 6) = 153.81 (Hz)
Natural freq (Mode 7) = 201.18 (Hz)
Natural freq (Mode 8) = 203.69 (Hz)
Natural freq (Mode 9) = 218.54 (Hz)
Natural freq (Mode 10) = 244.49 (Hz)
Natural freq (Mode 11) = 267.52 (Hz)
Natural freq (Mode 12) = 282.33 (Hz)
Natural freq (Mode 13) = 284.46 (Hz)
Natural freq (Mode 14) = 311.84 (Hz)
Natural freq (Mode 15) = 328.87 (Hz)
Natural freq (Mode 16) = 334.68 (Hz)
Natural freq (Mode 17) = 346.25 (Hz)
Natural freq (Mode 18) = 362.24 (Hz)
Natural freq (Mode 19) = 368.68 (Hz)
Natural freq (Mode 20) = 377.76 (Hz)
Natural freq (Mode 21) = 393.48 (Hz)
Natural freq (Mode 22) = 403.01 (Hz)
Natural freq (Mode 23) = 415.98 (Hz)
Natural freq (Mode 24) = 430.66 (Hz)
Natural freq (Mode 25) = 456.25 (Hz)
Natural freq (Mode 26) = 460.70 (Hz)
Natural freq (Mode 27) = 478.12 (Hz)
Natural freq (Mode 28) = 500.39 (Hz)
Natural freq (Mode 29) = 510.45 (Hz)
Natural freq (Mode 30) = 514.48 (Hz)
Natural freq (Mode 31) = 519.72 (Hz)
Natural freq (Mode 32) = 531.28 (Hz)
Natural freq (Mode 33) = 553.76 (Hz)
Natural freq (Mode 34) = 566.65 (Hz)
Natural freq (Mode 35) = 591.27 (Hz)
Natural freq (Mode 36) = 611.71 (Hz)
Natural freq (Mode 37) = 612.08 (Hz)
Natural freq (Mode 38) = 624.35 (Hz)
Natural freq (Mode 39) = 650.56 (Hz)
Natural freq (Mode 40) = 670.08 (Hz)
Natural freq (Mode 41) = 721.11 (Hz)
Natural freq (Mode 42) = 732.49 (Hz)
Natural freq (Mode 43) = 751.28 (Hz)
Natural freq (Mode 44) = 814.54 (Hz)
Natural freq (Mode 45) = 883.96 (Hz)
Natural freq (Mode 46) = 951.75 (Hz)
Natural freq (Mode 47) = 975.90 (Hz)
Natural freq (Mode 48) = 1290.98 (Hz)
Natural freq (Mode 49) = 1356.05 (Hz)
Natural freq (Mode 50) = 1506.01 (Hz)
Natural freq (Mode 51) = 1619.60 (Hz)
Natural freq (Mode 52) = 1631.13 (Hz)
Natural freq (Mode 53) = 1745.44 (Hz)
Natural freq (Mode 54) = 1904.47 (Hz)
Natural freq (Mode 55) = 2010.78 (Hz)
Natural freq (Mode 56) = 2031.59 (Hz)
Natural freq (Mode 57) = 2108.70 (Hz)
Natural freq (Mode 58) = 2215.97 (Hz)
Natural freq (Mode 59) = 2306.66 (Hz)
Natural freq (Mode 60) = 2320.15 (Hz)
Natural freq (Mode 61) = 2390.78 (Hz)
Natural freq (Mode 62) = 2494.64 (Hz)
Natural freq (Mode 63) = 2560.50 (Hz)
Natural freq (Mode 64) = 2584.60 (Hz)
Natural freq (Mode 65) = 2587.28 (Hz)
Natural freq (Mode 66) = 2659.52 (Hz)
Natural freq (Mode 67) = 2737.71 (Hz)
Natural freq (Mode 68) = 2789.18 (Hz)
Natural freq (Mode 69) = 2840.95 (Hz)
Natural freq (Mode 70) = 2888.34 (Hz)
Natural freq (Mode 71) = 2967.46 (Hz)
Natural freq (Mode 72) = 3051.49 (Hz)
Natural freq (Mode 73) = 3112.98 (Hz)
Natural freq (Mode 74) = 3139.85 (Hz)
Natural freq (Mode 75) = 3247.88 (Hz)
Natural freq (Mode 76) = 3303.45 (Hz)
Natural freq (Mode 77) = 3344.57 (Hz)
Natural freq (Mode 78) = 3466.41 (Hz)
Natural freq (Mode 79) = 3489.29 (Hz)
Natural freq (Mode 80) = 3562.75 (Hz)
Natural freq (Mode 81) = 3651.56 (Hz)
Natural freq (Mode 82) = 3712.84 (Hz)
Natural freq (Mode 83) = 3761.27 (Hz)
Natural freq (Mode 84) = 3806.30 (Hz)
Natural freq (Mode 85) = 3902.83 (Hz)
Natural freq (Mode 86) = 3961.00 (Hz)
Natural freq (Mode 87) = 4028.45 (Hz)
Natural freq (Mode 88) = 4110.02 (Hz)
Natural freq (Mode 89) = 4191.05 (Hz)
Natural freq (Mode 90) = 4202.44 (Hz)
Natural freq (Mode 91) = 4299.35 (Hz)
Natural freq (Mode 92) = 4376.59 (Hz)
Natural freq (Mode 93) = 4425.85 (Hz)
Natural freq (Mode 94) = 4501.49 (Hz)
Natural freq (Mode 95) = 4518.77 (Hz)
Natural freq (Mode 96) = 4586.52 (Hz)
Natural freq (Mode 97) = 4621.28 (Hz)
Natural freq (Mode 98) = 4678.52 (Hz)
Natural freq (Mode 99) = 4733.41 (Hz)
Natural freq (Mode 100) = 4788.76 (Hz)
Natural freq (Mode 101) = 4816.52 (Hz)
Natural freq (Mode 102) = 4942.47 (Hz)
Natural freq (Mode 103) = 4997.55 (Hz)
Natural freq (Mode 104) = 5045.56 (Hz)
Natural freq (Mode 105) = 5120.59 (Hz)
Natural freq (Mode 106) = 5155.17 (Hz)
Natural freq (Mode 107) = 5325.08 (Hz)
Natural freq (Mode 108) = 5474.54 (Hz)
Natural freq (Mode 109) = 5512.48 (Hz)
Natural freq (Mode 110) = 5525.67 (Hz)
Natural freq (Mode 111) = 5576.25 (Hz)
Natural freq (Mode 112) = 5647.01 (Hz)
Natural freq (Mode 113) = 5841.96 (Hz)
Natural freq (Mode 114) = 6096.57 (Hz)
Natural freq (Mode 115) = 6188.63 (Hz)
Natural freq (Mode 116) = 6328.76 (Hz)
Natural freq (Mode 117) = 6428.94 (Hz)
Natural freq (Mode 118) = 6468.91 (Hz)
Natural freq (Mode 119) = 6958.88 (Hz)
Natural freq (Mode 120) = 7050.41 (Hz)
Natural freq (Mode 121) = 7389.46 (Hz)
Natural freq (Mode 122) = 7464.28 (Hz)
Natural freq (Mode 123) = 7559.48 (Hz)
Natural freq (Mode 124) = 8076.62 (Hz)
Natural freq (Mode 125) = 8344.67 (Hz)
Natural freq (Mode 126) = 8685.13 (Hz)
Natural freq (Mode 127) = 9093.83 (Hz)
Natural freq (Mode 128) = 9351.46 (Hz)
Natural freq (Mode 129) = 10123.65 (Hz)
Natural freq (Mode 130) = 10828.55 (Hz)
Natural freq (Mode 131) = 11674.11 (Hz)

real	0m1.088s
user	0m0.661s
sys	0m0.400s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_AGARD445_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_Aeroelastic_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_Aeroelastic_PyTest.py test;
+ python -u nastran_Aeroelastic_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
	Name = Wing, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes    = 1377
Number of elements = 1514
Number of triangle elements      = 0
Number of quadrilateral elements = 1514
Body 2 (of 4)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes    = 17
Number of elements = 10
Number of triangle elements      = 0
Number of quadrilateral elements = 10
Body 4 (of 4)
Number of nodes    = 17
Number of elements = 10
Number of triangle elements      = 0
Number of quadrilateral elements = 10
----------------------------
Total number of nodes    = 1412
Total number of elements = 1534
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
	Name = Wing, index = 7
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1377
	Number of elements = 1514
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 1514
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 17
	Number of elements = 10
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 10
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 3
	Number of nodal coordinates = 17
	Number of elements = 10
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 10
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 1412
	Combined Number of elements = 1535
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 1534
Getting vortex lattice surface data
	VLM surface name - Skin_Top
	Done getting vortex lattice surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 300
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 5
	Property name - Rib_Root
	No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
	Property name - Ribs
	No "material" specified for Property tuple Ribs, defaulting to an index of 1
	Property name - Skin
	No "material" specified for Property tuple Skin, defaulting to an index of 1
	Property name - Spar1
	No "material" specified for Property tuple Spar1, defaulting to an index of 1
	Property name - Spar2
	No "material" specified for Property tuple Spar2, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - ribConstraint
	No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA supports.......
	Number of supports - 1
	Support name - ribSupport
	Done getting FEA supports

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Rib_Root
	No "groupName" specified for Connection tuple Rib_Root!
	Looking for automatic connections from the use of capsConnectLink for Rib_Root
	93 automatic connections were made for capsConnect Rib_Root (node id 1378)
	Done getting FEA connections
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Trim1
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No loads specified for case Trim1!!!!
	Writing mass increment cards
	Writing aeros card
	Writing aestat cards
	Writing analysis cards, 0
	Writing constraint ADD cards
	Writing constraint cards
	Writing support cards
	Writing material cards
	Writing property cards
	Writing aeroelastic cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m6.696s
user	0m17.329s
sys	0m5.229s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_Aeroelastic_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_CompositeWingDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_CompositeWingDesign_PyTest.py test;
+ python -u nastran_CompositeWingDesign_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 282
Number of elements = 221
Number of triangle elements      = 0
Number of quadrilateral elements = 221
----------------------------
Total number of nodes    = 282
Total number of elements = 221
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 = 282
	Number of elements = 221
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 221
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Aluminum
	No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
	Material name - Graphite_epoxy
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - wing
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 8
	Design_Variable name - L1
	Design_Variable name - L2
	Design_Variable name - L3
	Design_Variable name - L4
	Design_Variable name - L5
	Design_Variable name - L6
	Design_Variable name - L7
	Design_Variable name - L8
	Design_Variable_Relation name - L1R
	Design_Variable_Relation name - L2R
	Design_Variable_Relation name - L3R
	Design_Variable_Relation name - L4R
	Design_Variable_Relation name - L5R
	Design_Variable_Relation name - L6R
	Design_Variable_Relation name - L7R
	Design_Variable_Relation name - L8R
	Number of design variable relations - 8
	Done getting FEA design variables

Getting FEA design constraints.......
	Number of design constraints - 8
	Design_Constraint name - stress1
	Design_Constraint name - stress2
	Design_Constraint name - stress3
	Design_Constraint name - stress4
	Design_Constraint name - stress5
	Design_Constraint name - stress6
	Design_Constraint name - stress7
	Design_Constraint name - stress8
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - StaticAnalysis
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing constraint ADD cards
	Writing design constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing coordinate system cards
	Writing design variable cards
	Writing design variable relation cards
	Writing design constraints and responses cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m1.521s
user	0m1.211s
sys	0m0.372s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_CompositeWingDesign_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_CompositeWingFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_CompositeWingFreq_PyTest.py test;
+ python -u nastran_CompositeWingFreq_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 282
Number of elements = 221
Number of triangle elements      = 0
Number of quadrilateral elements = 221
----------------------------
Total number of nodes    = 282
Total number of elements = 221
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 = 282
	Number of elements = 221
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 221
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Aluminum
	No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
	Material name - Graphite_epoxy
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - wing
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - root
	No "constraintType" specified for Constraint tuple root, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Warning: No loads specified for case EigenAnalysis!!!!
	Writing mass increment cards
	Writing analysis cards, 0
	Writing combined constraint cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing coordinate system cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

Getting results for natural frequencies.....
Reading Nastran FO6 file - extracting Eigen-Values!
	Number of Eigen-Values = 1779
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
	Loading Eigen-Value = 4
	Loading Eigen-Value = 5
	Loading Eigen-Value = 6
	Loading Eigen-Value = 7
	Loading Eigen-Value = 8
	Loading Eigen-Value = 9
	Loading Eigen-Value = 10
	Loading Eigen-Value = 11
	Loading Eigen-Value = 12
	Loading Eigen-Value = 13
	Loading Eigen-Value = 14
	Loading Eigen-Value = 15
	Loading Eigen-Value = 16
	Loading Eigen-Value = 17
	Loading Eigen-Value = 18
	Loading Eigen-Value = 19
	Loading Eigen-Value = 20
	Loading Eigen-Value = 21
	Loading Eigen-Value = 22
	Loading Eigen-Value = 23
	Loading Eigen-Value = 24
	Loading Eigen-Value = 25
	Loading Eigen-Value = 26
	Loading Eigen-Value = 27
	Loading Eigen-Value = 28
	Loading Eigen-Value = 29
	Loading Eigen-Value = 30
	Loading Eigen-Value = 31
	Loading Eigen-Value = 32
	Loading Eigen-Value = 33
	Loading Eigen-Value = 34
	Loading Eigen-Value = 35
	Loading Eigen-Value = 36
	Loading Eigen-Value = 37
	Loading Eigen-Value = 38
	Loading Eigen-Value = 39
	Loading Eigen-Value = 40
	Loading Eigen-Value = 41
	Loading Eigen-Value = 42
	Loading Eigen-Value = 43
	Loading Eigen-Value = 44
	Loading Eigen-Value = 45
	Loading Eigen-Value = 46
	Loading Eigen-Value = 47
	Loading Eigen-Value = 48
	Loading Eigen-Value = 49
	Loading Eigen-Value = 50
	Loading Eigen-Value = 51
	Loading Eigen-Value = 52
	Loading Eigen-Value = 53
	Loading Eigen-Value = 54
	Loading Eigen-Value = 55
	Loading Eigen-Value = 56
	Loading Eigen-Value = 57
	Loading Eigen-Value = 58
	Loading Eigen-Value = 59
	Loading Eigen-Value = 60
	Loading Eigen-Value = 61
	Loading Eigen-Value = 62
	Loading Eigen-Value = 63
	Loading Eigen-Value = 64
	Loading Eigen-Value = 65
	Loading Eigen-Value = 66
	Loading Eigen-Value = 67
	Loading Eigen-Value = 68
	Loading Eigen-Value = 69
	Loading Eigen-Value = 70
	Loading Eigen-Value = 71
	Loading Eigen-Value = 72
	Loading Eigen-Value = 73
	Loading Eigen-Value = 74
	Loading Eigen-Value = 75
	Loading Eigen-Value = 76
	Loading Eigen-Value = 77
	Loading Eigen-Value = 78
	Loading Eigen-Value = 79
	Loading Eigen-Value = 80
	Loading Eigen-Value = 81
	Loading Eigen-Value = 82
	Loading Eigen-Value = 83
	Loading Eigen-Value = 84
	Loading Eigen-Value = 85
	Loading Eigen-Value = 86
	Loading Eigen-Value = 87
	Loading Eigen-Value = 88
	Loading Eigen-Value = 89
	Loading Eigen-Value = 90
	Loading Eigen-Value = 91
	Loading Eigen-Value = 92
	Loading Eigen-Value = 93
	Loading Eigen-Value = 94
	Loading Eigen-Value = 95
	Loading Eigen-Value = 96
	Loading Eigen-Value = 97
	Loading Eigen-Value = 98
	Loading Eigen-Value = 99
	Loading Eigen-Value = 100
	Loading Eigen-Value = 101
	Loading Eigen-Value = 102
	Loading Eigen-Value = 103
	Loading Eigen-Value = 104
	Loading Eigen-Value = 105
	Loading Eigen-Value = 106
	Loading Eigen-Value = 107
	Loading Eigen-Value = 108
	Loading Eigen-Value = 109
	Loading Eigen-Value = 110
	Loading Eigen-Value = 111
	Loading Eigen-Value = 112
	Loading Eigen-Value = 113
	Loading Eigen-Value = 114
	Loading Eigen-Value = 115
	Loading Eigen-Value = 116
	Loading Eigen-Value = 117
	Loading Eigen-Value = 118
	Loading Eigen-Value = 119
	Loading Eigen-Value = 120
	Loading Eigen-Value = 121
	Loading Eigen-Value = 122
	Loading Eigen-Value = 123
	Loading Eigen-Value = 124
	Loading Eigen-Value = 125
	Loading Eigen-Value = 126
	Loading Eigen-Value = 127
	Loading Eigen-Value = 128
	Loading Eigen-Value = 129
	Loading Eigen-Value = 130
	Loading Eigen-Value = 131
	Loading Eigen-Value = 132
	Loading Eigen-Value = 133
	Loading Eigen-Value = 134
	Loading Eigen-Value = 135
	Loading Eigen-Value = 136
	Loading Eigen-Value = 137
	Loading Eigen-Value = 138
	Loading Eigen-Value = 139
	Loading Eigen-Value = 140
	Loading Eigen-Value = 141
	Loading Eigen-Value = 142
	Loading Eigen-Value = 143
	Loading Eigen-Value = 144
	Loading Eigen-Value = 145
	Loading Eigen-Value = 146
	Loading Eigen-Value = 147
	Loading Eigen-Value = 148
	Loading Eigen-Value = 149
	Loading Eigen-Value = 150
	Loading Eigen-Value = 151
	Loading Eigen-Value = 152
	Loading Eigen-Value = 153
	Loading Eigen-Value = 154
	Loading Eigen-Value = 155
	Loading Eigen-Value = 156
	Loading Eigen-Value = 157
	Loading Eigen-Value = 158
	Loading Eigen-Value = 159
	Loading Eigen-Value = 160
	Loading Eigen-Value = 161
	Loading Eigen-Value = 162
	Loading Eigen-Value = 163
	Loading Eigen-Value = 164
	Loading Eigen-Value = 165
	Loading Eigen-Value = 166
	Loading Eigen-Value = 167
	Loading Eigen-Value = 168
	Loading Eigen-Value = 169
	Loading Eigen-Value = 170
	Loading Eigen-Value = 171
	Loading Eigen-Value = 172
	Loading Eigen-Value = 173
	Loading Eigen-Value = 174
	Loading Eigen-Value = 175
	Loading Eigen-Value = 176
	Loading Eigen-Value = 177
	Loading Eigen-Value = 178
	Loading Eigen-Value = 179
	Loading Eigen-Value = 180
	Loading Eigen-Value = 181
	Loading Eigen-Value = 182
	Loading Eigen-Value = 183
	Loading Eigen-Value = 184
	Loading Eigen-Value = 185
	Loading Eigen-Value = 186
	Loading Eigen-Value = 187
	Loading Eigen-Value = 188
	Loading Eigen-Value = 189
	Loading Eigen-Value = 190
	Loading Eigen-Value = 191
	Loading Eigen-Value = 192
	Loading Eigen-Value = 193
	Loading Eigen-Value = 194
	Loading Eigen-Value = 195
	Loading Eigen-Value = 196
	Loading Eigen-Value = 197
	Loading Eigen-Value = 198
	Loading Eigen-Value = 199
	Loading Eigen-Value = 200
	Loading Eigen-Value = 201
	Loading Eigen-Value = 202
	Loading Eigen-Value = 203
	Loading Eigen-Value = 204
	Loading Eigen-Value = 205
	Loading Eigen-Value = 206
	Loading Eigen-Value = 207
	Loading Eigen-Value = 208
	Loading Eigen-Value = 209
	Loading Eigen-Value = 210
	Loading Eigen-Value = 211
	Loading Eigen-Value = 212
	Loading Eigen-Value = 213
	Loading Eigen-Value = 214
	Loading Eigen-Value = 215
	Loading Eigen-Value = 216
	Loading Eigen-Value = 217
	Loading Eigen-Value = 218
	Loading Eigen-Value = 219
	Loading Eigen-Value = 220
	Loading Eigen-Value = 221
	Loading Eigen-Value = 222
	Loading Eigen-Value = 223
	Loading Eigen-Value = 224
	Loading Eigen-Value = 225
	Loading Eigen-Value = 226
	Loading Eigen-Value = 227
	Loading Eigen-Value = 228
	Loading Eigen-Value = 229
	Loading Eigen-Value = 230
	Loading Eigen-Value = 231
	Loading Eigen-Value = 232
	Loading Eigen-Value = 233
	Loading Eigen-Value = 234
	Loading Eigen-Value = 235
	Loading Eigen-Value = 236
	Loading Eigen-Value = 237
	Loading Eigen-Value = 238
	Loading Eigen-Value = 239
	Loading Eigen-Value = 240
	Loading Eigen-Value = 241
	Loading Eigen-Value = 242
	Loading Eigen-Value = 243
	Loading Eigen-Value = 244
	Loading Eigen-Value = 245
	Loading Eigen-Value = 246
	Loading Eigen-Value = 247
	Loading Eigen-Value = 248
	Loading Eigen-Value = 249
	Loading Eigen-Value = 250
	Loading Eigen-Value = 251
	Loading Eigen-Value = 252
	Loading Eigen-Value = 253
	Loading Eigen-Value = 254
	Loading Eigen-Value = 255
	Loading Eigen-Value = 256
	Loading Eigen-Value = 257
	Loading Eigen-Value = 258
	Loading Eigen-Value = 259
	Loading Eigen-Value = 260
	Loading Eigen-Value = 261
	Loading Eigen-Value = 262
	Loading Eigen-Value = 263
	Loading Eigen-Value = 264
	Loading Eigen-Value = 265
	Loading Eigen-Value = 266
	Loading Eigen-Value = 267
	Loading Eigen-Value = 268
	Loading Eigen-Value = 269
	Loading Eigen-Value = 270
	Loading Eigen-Value = 271
	Loading Eigen-Value = 272
	Loading Eigen-Value = 273
	Loading Eigen-Value = 274
	Loading Eigen-Value = 275
	Loading Eigen-Value = 276
	Loading Eigen-Value = 277
	Loading Eigen-Value = 278
	Loading Eigen-Value = 279
	Loading Eigen-Value = 280
	Loading Eigen-Value = 281
	Loading Eigen-Value = 282
	Loading Eigen-Value = 283
	Loading Eigen-Value = 284
	Loading Eigen-Value = 285
	Loading Eigen-Value = 286
	Loading Eigen-Value = 287
	Loading Eigen-Value = 288
	Loading Eigen-Value = 289
	Loading Eigen-Value = 290
	Loading Eigen-Value = 291
	Loading Eigen-Value = 292
	Loading Eigen-Value = 293
	Loading Eigen-Value = 294
	Loading Eigen-Value = 295
	Loading Eigen-Value = 296
	Loading Eigen-Value = 297
	Loading Eigen-Value = 298
	Loading Eigen-Value = 299
	Loading Eigen-Value = 300
	Loading Eigen-Value = 301
	Loading Eigen-Value = 302
	Loading Eigen-Value = 303
	Loading Eigen-Value = 304
	Loading Eigen-Value = 305
	Loading Eigen-Value = 306
	Loading Eigen-Value = 307
	Loading Eigen-Value = 308
	Loading Eigen-Value = 309
	Loading Eigen-Value = 310
	Loading Eigen-Value = 311
	Loading Eigen-Value = 312
	Loading Eigen-Value = 313
	Loading Eigen-Value = 314
	Loading Eigen-Value = 315
	Loading Eigen-Value = 316
	Loading Eigen-Value = 317
	Loading Eigen-Value = 318
	Loading Eigen-Value = 319
	Loading Eigen-Value = 320
	Loading Eigen-Value = 321
	Loading Eigen-Value = 322
	Loading Eigen-Value = 323
	Loading Eigen-Value = 324
	Loading Eigen-Value = 325
	Loading Eigen-Value = 326
	Loading Eigen-Value = 327
	Loading Eigen-Value = 328
	Loading Eigen-Value = 329
	Loading Eigen-Value = 330
	Loading Eigen-Value = 331
	Loading Eigen-Value = 332
	Loading Eigen-Value = 333
	Loading Eigen-Value = 334
	Loading Eigen-Value = 335
	Loading Eigen-Value = 336
	Loading Eigen-Value = 337
	Loading Eigen-Value = 338
	Loading Eigen-Value = 339
	Loading Eigen-Value = 340
	Loading Eigen-Value = 341
	Loading Eigen-Value = 342
	Loading Eigen-Value = 343
	Loading Eigen-Value = 344
	Loading Eigen-Value = 345
	Loading Eigen-Value = 346
	Loading Eigen-Value = 347
	Loading Eigen-Value = 348
	Loading Eigen-Value = 349
	Loading Eigen-Value = 350
	Loading Eigen-Value = 351
	Loading Eigen-Value = 352
	Loading Eigen-Value = 353
	Loading Eigen-Value = 354
	Loading Eigen-Value = 355
	Loading Eigen-Value = 356
	Loading Eigen-Value = 357
	Loading Eigen-Value = 358
	Loading Eigen-Value = 359
	Loading Eigen-Value = 360
	Loading Eigen-Value = 361
	Loading Eigen-Value = 362
	Loading Eigen-Value = 363
	Loading Eigen-Value = 364
	Loading Eigen-Value = 365
	Loading Eigen-Value = 366
	Loading Eigen-Value = 367
	Loading Eigen-Value = 368
	Loading Eigen-Value = 369
	Loading Eigen-Value = 370
	Loading Eigen-Value = 371
	Loading Eigen-Value = 372
	Loading Eigen-Value = 373
	Loading Eigen-Value = 374
	Loading Eigen-Value = 375
	Loading Eigen-Value = 376
	Loading Eigen-Value = 377
	Loading Eigen-Value = 378
	Loading Eigen-Value = 379
	Loading Eigen-Value = 380
	Loading Eigen-Value = 381
	Loading Eigen-Value = 382
	Loading Eigen-Value = 383
	Loading Eigen-Value = 384
	Loading Eigen-Value = 385
	Loading Eigen-Value = 386
	Loading Eigen-Value = 387
	Loading Eigen-Value = 388
	Loading Eigen-Value = 389
	Loading Eigen-Value = 390
	Loading Eigen-Value = 391
	Loading Eigen-Value = 392
	Loading Eigen-Value = 393
	Loading Eigen-Value = 394
	Loading Eigen-Value = 395
	Loading Eigen-Value = 396
	Loading Eigen-Value = 397
	Loading Eigen-Value = 398
	Loading Eigen-Value = 399
	Loading Eigen-Value = 400
	Loading Eigen-Value = 401
	Loading Eigen-Value = 402
	Loading Eigen-Value = 403
	Loading Eigen-Value = 404
	Loading Eigen-Value = 405
	Loading Eigen-Value = 406
	Loading Eigen-Value = 407
	Loading Eigen-Value = 408
	Loading Eigen-Value = 409
	Loading Eigen-Value = 410
	Loading Eigen-Value = 411
	Loading Eigen-Value = 412
	Loading Eigen-Value = 413
	Loading Eigen-Value = 414
	Loading Eigen-Value = 415
	Loading Eigen-Value = 416
	Loading Eigen-Value = 417
	Loading Eigen-Value = 418
	Loading Eigen-Value = 419
	Loading Eigen-Value = 420
	Loading Eigen-Value = 421
	Loading Eigen-Value = 422
	Loading Eigen-Value = 423
	Loading Eigen-Value = 424
	Loading Eigen-Value = 425
	Loading Eigen-Value = 426
	Loading Eigen-Value = 427
	Loading Eigen-Value = 428
	Loading Eigen-Value = 429
	Loading Eigen-Value = 430
	Loading Eigen-Value = 431
	Loading Eigen-Value = 432
	Loading Eigen-Value = 433
	Loading Eigen-Value = 434
	Loading Eigen-Value = 435
	Loading Eigen-Value = 436
	Loading Eigen-Value = 437
	Loading Eigen-Value = 438
	Loading Eigen-Value = 439
	Loading Eigen-Value = 440
	Loading Eigen-Value = 441
	Loading Eigen-Value = 442
	Loading Eigen-Value = 443
	Loading Eigen-Value = 444
	Loading Eigen-Value = 445
	Loading Eigen-Value = 446
	Loading Eigen-Value = 447
	Loading Eigen-Value = 448
	Loading Eigen-Value = 449
	Loading Eigen-Value = 450
	Loading Eigen-Value = 451
	Loading Eigen-Value = 452
	Loading Eigen-Value = 453
	Loading Eigen-Value = 454
	Loading Eigen-Value = 455
	Loading Eigen-Value = 456
	Loading Eigen-Value = 457
	Loading Eigen-Value = 458
	Loading Eigen-Value = 459
	Loading Eigen-Value = 460
	Loading Eigen-Value = 461
	Loading Eigen-Value = 462
	Loading Eigen-Value = 463
	Loading Eigen-Value = 464
	Loading Eigen-Value = 465
	Loading Eigen-Value = 466
	Loading Eigen-Value = 467
	Loading Eigen-Value = 468
	Loading Eigen-Value = 469
	Loading Eigen-Value = 470
	Loading Eigen-Value = 471
	Loading Eigen-Value = 472
	Loading Eigen-Value = 473
	Loading Eigen-Value = 474
	Loading Eigen-Value = 475
	Loading Eigen-Value = 476
	Loading Eigen-Value = 477
	Loading Eigen-Value = 478
	Loading Eigen-Value = 479
	Loading Eigen-Value = 480
	Loading Eigen-Value = 481
	Loading Eigen-Value = 482
	Loading Eigen-Value = 483
	Loading Eigen-Value = 484
	Loading Eigen-Value = 485
	Loading Eigen-Value = 486
	Loading Eigen-Value = 487
	Loading Eigen-Value = 488
	Loading Eigen-Value = 489
	Loading Eigen-Value = 490
	Loading Eigen-Value = 491
	Loading Eigen-Value = 492
	Loading Eigen-Value = 493
	Loading Eigen-Value = 494
	Loading Eigen-Value = 495
	Loading Eigen-Value = 496
	Loading Eigen-Value = 497
	Loading Eigen-Value = 498
	Loading Eigen-Value = 499
	Loading Eigen-Value = 500
	Loading Eigen-Value = 501
	Loading Eigen-Value = 502
	Loading Eigen-Value = 503
	Loading Eigen-Value = 504
	Loading Eigen-Value = 505
	Loading Eigen-Value = 506
	Loading Eigen-Value = 507
	Loading Eigen-Value = 508
	Loading Eigen-Value = 509
	Loading Eigen-Value = 510
	Loading Eigen-Value = 511
	Loading Eigen-Value = 512
	Loading Eigen-Value = 513
	Loading Eigen-Value = 514
	Loading Eigen-Value = 515
	Loading Eigen-Value = 516
	Loading Eigen-Value = 517
	Loading Eigen-Value = 518
	Loading Eigen-Value = 519
	Loading Eigen-Value = 520
	Loading Eigen-Value = 521
	Loading Eigen-Value = 522
	Loading Eigen-Value = 523
	Loading Eigen-Value = 524
	Loading Eigen-Value = 525
	Loading Eigen-Value = 526
	Loading Eigen-Value = 527
	Loading Eigen-Value = 528
	Loading Eigen-Value = 529
	Loading Eigen-Value = 530
	Loading Eigen-Value = 531
	Loading Eigen-Value = 532
	Loading Eigen-Value = 533
	Loading Eigen-Value = 534
	Loading Eigen-Value = 535
	Loading Eigen-Value = 536
	Loading Eigen-Value = 537
	Loading Eigen-Value = 538
	Loading Eigen-Value = 539
	Loading Eigen-Value = 540
	Loading Eigen-Value = 541
	Loading Eigen-Value = 542
	Loading Eigen-Value = 543
	Loading Eigen-Value = 544
	Loading Eigen-Value = 545
	Loading Eigen-Value = 546
	Loading Eigen-Value = 547
	Loading Eigen-Value = 548
	Loading Eigen-Value = 549
	Loading Eigen-Value = 550
	Loading Eigen-Value = 551
	Loading Eigen-Value = 552
	Loading Eigen-Value = 553
	Loading Eigen-Value = 554
	Loading Eigen-Value = 555
	Loading Eigen-Value = 556
	Loading Eigen-Value = 557
	Loading Eigen-Value = 558
	Loading Eigen-Value = 559
	Loading Eigen-Value = 560
	Loading Eigen-Value = 561
	Loading Eigen-Value = 562
	Loading Eigen-Value = 563
	Loading Eigen-Value = 564
	Loading Eigen-Value = 565
	Loading Eigen-Value = 566
	Loading Eigen-Value = 567
	Loading Eigen-Value = 568
	Loading Eigen-Value = 569
	Loading Eigen-Value = 570
	Loading Eigen-Value = 571
	Loading Eigen-Value = 572
	Loading Eigen-Value = 573
	Loading Eigen-Value = 574
	Loading Eigen-Value = 575
	Loading Eigen-Value = 576
	Loading Eigen-Value = 577
	Loading Eigen-Value = 578
	Loading Eigen-Value = 579
	Loading Eigen-Value = 580
	Loading Eigen-Value = 581
	Loading Eigen-Value = 582
	Loading Eigen-Value = 583
	Loading Eigen-Value = 584
	Loading Eigen-Value = 585
	Loading Eigen-Value = 586
	Loading Eigen-Value = 587
	Loading Eigen-Value = 588
	Loading Eigen-Value = 589
	Loading Eigen-Value = 590
	Loading Eigen-Value = 591
	Loading Eigen-Value = 592
	Loading Eigen-Value = 593
	Loading Eigen-Value = 594
	Loading Eigen-Value = 595
	Loading Eigen-Value = 596
	Loading Eigen-Value = 597
	Loading Eigen-Value = 598
	Loading Eigen-Value = 599
	Loading Eigen-Value = 600
	Loading Eigen-Value = 601
	Loading Eigen-Value = 602
	Loading Eigen-Value = 603
	Loading Eigen-Value = 604
	Loading Eigen-Value = 605
	Loading Eigen-Value = 606
	Loading Eigen-Value = 607
	Loading Eigen-Value = 608
	Loading Eigen-Value = 609
	Loading Eigen-Value = 610
	Loading Eigen-Value = 611
	Loading Eigen-Value = 612
	Loading Eigen-Value = 613
	Loading Eigen-Value = 614
	Loading Eigen-Value = 615
	Loading Eigen-Value = 616
	Loading Eigen-Value = 617
	Loading Eigen-Value = 618
	Loading Eigen-Value = 619
	Loading Eigen-Value = 620
	Loading Eigen-Value = 621
	Loading Eigen-Value = 622
	Loading Eigen-Value = 623
	Loading Eigen-Value = 624
	Loading Eigen-Value = 625
	Loading Eigen-Value = 626
	Loading Eigen-Value = 627
	Loading Eigen-Value = 628
	Loading Eigen-Value = 629
	Loading Eigen-Value = 630
	Loading Eigen-Value = 631
	Loading Eigen-Value = 632
	Loading Eigen-Value = 633
	Loading Eigen-Value = 634
	Loading Eigen-Value = 635
	Loading Eigen-Value = 636
	Loading Eigen-Value = 637
	Loading Eigen-Value = 638
	Loading Eigen-Value = 639
	Loading Eigen-Value = 640
	Loading Eigen-Value = 641
	Loading Eigen-Value = 642
	Loading Eigen-Value = 643
	Loading Eigen-Value = 644
	Loading Eigen-Value = 645
	Loading Eigen-Value = 646
	Loading Eigen-Value = 647
	Loading Eigen-Value = 648
	Loading Eigen-Value = 649
	Loading Eigen-Value = 650
	Loading Eigen-Value = 651
	Loading Eigen-Value = 652
	Loading Eigen-Value = 653
	Loading Eigen-Value = 654
	Loading Eigen-Value = 655
	Loading Eigen-Value = 656
	Loading Eigen-Value = 657
	Loading Eigen-Value = 658
	Loading Eigen-Value = 659
	Loading Eigen-Value = 660
	Loading Eigen-Value = 661
	Loading Eigen-Value = 662
	Loading Eigen-Value = 663
	Loading Eigen-Value = 664
	Loading Eigen-Value = 665
	Loading Eigen-Value = 666
	Loading Eigen-Value = 667
	Loading Eigen-Value = 668
	Loading Eigen-Value = 669
	Loading Eigen-Value = 670
	Loading Eigen-Value = 671
	Loading Eigen-Value = 672
	Loading Eigen-Value = 673
	Loading Eigen-Value = 674
	Loading Eigen-Value = 675
	Loading Eigen-Value = 676
	Loading Eigen-Value = 677
	Loading Eigen-Value = 678
	Loading Eigen-Value = 679
	Loading Eigen-Value = 680
	Loading Eigen-Value = 681
	Loading Eigen-Value = 682
	Loading Eigen-Value = 683
	Loading Eigen-Value = 684
	Loading Eigen-Value = 685
	Loading Eigen-Value = 686
	Loading Eigen-Value = 687
	Loading Eigen-Value = 688
	Loading Eigen-Value = 689
	Loading Eigen-Value = 690
	Loading Eigen-Value = 691
	Loading Eigen-Value = 692
	Loading Eigen-Value = 693
	Loading Eigen-Value = 694
	Loading Eigen-Value = 695
	Loading Eigen-Value = 696
	Loading Eigen-Value = 697
	Loading Eigen-Value = 698
	Loading Eigen-Value = 699
	Loading Eigen-Value = 700
	Loading Eigen-Value = 701
	Loading Eigen-Value = 702
	Loading Eigen-Value = 703
	Loading Eigen-Value = 704
	Loading Eigen-Value = 705
	Loading Eigen-Value = 706
	Loading Eigen-Value = 707
	Loading Eigen-Value = 708
	Loading Eigen-Value = 709
	Loading Eigen-Value = 710
	Loading Eigen-Value = 711
	Loading Eigen-Value = 712
	Loading Eigen-Value = 713
	Loading Eigen-Value = 714
	Loading Eigen-Value = 715
	Loading Eigen-Value = 716
	Loading Eigen-Value = 717
	Loading Eigen-Value = 718
	Loading Eigen-Value = 719
	Loading Eigen-Value = 720
	Loading Eigen-Value = 721
	Loading Eigen-Value = 722
	Loading Eigen-Value = 723
	Loading Eigen-Value = 724
	Loading Eigen-Value = 725
	Loading Eigen-Value = 726
	Loading Eigen-Value = 727
	Loading Eigen-Value = 728
	Loading Eigen-Value = 729
	Loading Eigen-Value = 730
	Loading Eigen-Value = 731
	Loading Eigen-Value = 732
	Loading Eigen-Value = 733
	Loading Eigen-Value = 734
	Loading Eigen-Value = 735
	Loading Eigen-Value = 736
	Loading Eigen-Value = 737
	Loading Eigen-Value = 738
	Loading Eigen-Value = 739
	Loading Eigen-Value = 740
	Loading Eigen-Value = 741
	Loading Eigen-Value = 742
	Loading Eigen-Value = 743
	Loading Eigen-Value = 744
	Loading Eigen-Value = 745
	Loading Eigen-Value = 746
	Loading Eigen-Value = 747
	Loading Eigen-Value = 748
	Loading Eigen-Value = 749
	Loading Eigen-Value = 750
	Loading Eigen-Value = 751
	Loading Eigen-Value = 752
	Loading Eigen-Value = 753
	Loading Eigen-Value = 754
	Loading Eigen-Value = 755
	Loading Eigen-Value = 756
	Loading Eigen-Value = 757
	Loading Eigen-Value = 758
	Loading Eigen-Value = 759
	Loading Eigen-Value = 760
	Loading Eigen-Value = 761
	Loading Eigen-Value = 762
	Loading Eigen-Value = 763
	Loading Eigen-Value = 764
	Loading Eigen-Value = 765
	Loading Eigen-Value = 766
	Loading Eigen-Value = 767
	Loading Eigen-Value = 768
	Loading Eigen-Value = 769
	Loading Eigen-Value = 770
	Loading Eigen-Value = 771
	Loading Eigen-Value = 772
	Loading Eigen-Value = 773
	Loading Eigen-Value = 774
	Loading Eigen-Value = 775
	Loading Eigen-Value = 776
	Loading Eigen-Value = 777
	Loading Eigen-Value = 778
	Loading Eigen-Value = 779
	Loading Eigen-Value = 780
	Loading Eigen-Value = 781
	Loading Eigen-Value = 782
	Loading Eigen-Value = 783
	Loading Eigen-Value = 784
	Loading Eigen-Value = 785
	Loading Eigen-Value = 786
	Loading Eigen-Value = 787
	Loading Eigen-Value = 788
	Loading Eigen-Value = 789
	Loading Eigen-Value = 790
	Loading Eigen-Value = 791
	Loading Eigen-Value = 792
	Loading Eigen-Value = 793
	Loading Eigen-Value = 794
	Loading Eigen-Value = 795
	Loading Eigen-Value = 796
	Loading Eigen-Value = 797
	Loading Eigen-Value = 798
	Loading Eigen-Value = 799
	Loading Eigen-Value = 800
	Loading Eigen-Value = 801
	Loading Eigen-Value = 802
	Loading Eigen-Value = 803
	Loading Eigen-Value = 804
	Loading Eigen-Value = 805
	Loading Eigen-Value = 806
	Loading Eigen-Value = 807
	Loading Eigen-Value = 808
	Loading Eigen-Value = 809
	Loading Eigen-Value = 810
	Loading Eigen-Value = 811
	Loading Eigen-Value = 812
	Loading Eigen-Value = 813
	Loading Eigen-Value = 814
	Loading Eigen-Value = 815
	Loading Eigen-Value = 816
	Loading Eigen-Value = 817
	Loading Eigen-Value = 818
	Loading Eigen-Value = 819
	Loading Eigen-Value = 820
	Loading Eigen-Value = 821
	Loading Eigen-Value = 822
	Loading Eigen-Value = 823
	Loading Eigen-Value = 824
	Loading Eigen-Value = 825
	Loading Eigen-Value = 826
	Loading Eigen-Value = 827
	Loading Eigen-Value = 828
	Loading Eigen-Value = 829
	Loading Eigen-Value = 830
	Loading Eigen-Value = 831
	Loading Eigen-Value = 832
	Loading Eigen-Value = 833
	Loading Eigen-Value = 834
	Loading Eigen-Value = 835
	Loading Eigen-Value = 836
	Loading Eigen-Value = 837
	Loading Eigen-Value = 838
	Loading Eigen-Value = 839
	Loading Eigen-Value = 840
	Loading Eigen-Value = 841
	Loading Eigen-Value = 842
	Loading Eigen-Value = 843
	Loading Eigen-Value = 844
	Loading Eigen-Value = 845
	Loading Eigen-Value = 846
	Loading Eigen-Value = 847
	Loading Eigen-Value = 848
	Loading Eigen-Value = 849
	Loading Eigen-Value = 850
	Loading Eigen-Value = 851
	Loading Eigen-Value = 852
	Loading Eigen-Value = 853
	Loading Eigen-Value = 854
	Loading Eigen-Value = 855
	Loading Eigen-Value = 856
	Loading Eigen-Value = 857
	Loading Eigen-Value = 858
	Loading Eigen-Value = 859
	Loading Eigen-Value = 860
	Loading Eigen-Value = 861
	Loading Eigen-Value = 862
	Loading Eigen-Value = 863
	Loading Eigen-Value = 864
	Loading Eigen-Value = 865
	Loading Eigen-Value = 866
	Loading Eigen-Value = 867
	Loading Eigen-Value = 868
	Loading Eigen-Value = 869
	Loading Eigen-Value = 870
	Loading Eigen-Value = 871
	Loading Eigen-Value = 872
	Loading Eigen-Value = 873
	Loading Eigen-Value = 874
	Loading Eigen-Value = 875
	Loading Eigen-Value = 876
	Loading Eigen-Value = 877
	Loading Eigen-Value = 878
	Loading Eigen-Value = 879
	Loading Eigen-Value = 880
	Loading Eigen-Value = 881
	Loading Eigen-Value = 882
	Loading Eigen-Value = 883
	Loading Eigen-Value = 884
	Loading Eigen-Value = 885
	Loading Eigen-Value = 886
	Loading Eigen-Value = 887
	Loading Eigen-Value = 888
	Loading Eigen-Value = 889
	Loading Eigen-Value = 890
	Loading Eigen-Value = 891
	Loading Eigen-Value = 892
	Loading Eigen-Value = 893
	Loading Eigen-Value = 894
	Loading Eigen-Value = 895
	Loading Eigen-Value = 896
	Loading Eigen-Value = 897
	Loading Eigen-Value = 898
	Loading Eigen-Value = 899
	Loading Eigen-Value = 900
	Loading Eigen-Value = 901
	Loading Eigen-Value = 902
	Loading Eigen-Value = 903
	Loading Eigen-Value = 904
	Loading Eigen-Value = 905
	Loading Eigen-Value = 906
	Loading Eigen-Value = 907
	Loading Eigen-Value = 908
	Loading Eigen-Value = 909
	Loading Eigen-Value = 910
	Loading Eigen-Value = 911
	Loading Eigen-Value = 912
	Loading Eigen-Value = 913
	Loading Eigen-Value = 914
	Loading Eigen-Value = 915
	Loading Eigen-Value = 916
	Loading Eigen-Value = 917
	Loading Eigen-Value = 918
	Loading Eigen-Value = 919
	Loading Eigen-Value = 920
	Loading Eigen-Value = 921
	Loading Eigen-Value = 922
	Loading Eigen-Value = 923
	Loading Eigen-Value = 924
	Loading Eigen-Value = 925
	Loading Eigen-Value = 926
	Loading Eigen-Value = 927
	Loading Eigen-Value = 928
	Loading Eigen-Value = 929
	Loading Eigen-Value = 930
	Loading Eigen-Value = 931
	Loading Eigen-Value = 932
	Loading Eigen-Value = 933
	Loading Eigen-Value = 934
	Loading Eigen-Value = 935
	Loading Eigen-Value = 936
	Loading Eigen-Value = 937
	Loading Eigen-Value = 938
	Loading Eigen-Value = 939
	Loading Eigen-Value = 940
	Loading Eigen-Value = 941
	Loading Eigen-Value = 942
	Loading Eigen-Value = 943
	Loading Eigen-Value = 944
	Loading Eigen-Value = 945
	Loading Eigen-Value = 946
	Loading Eigen-Value = 947
	Loading Eigen-Value = 948
	Loading Eigen-Value = 949
	Loading Eigen-Value = 950
	Loading Eigen-Value = 951
	Loading Eigen-Value = 952
	Loading Eigen-Value = 953
	Loading Eigen-Value = 954
	Loading Eigen-Value = 955
	Loading Eigen-Value = 956
	Loading Eigen-Value = 957
	Loading Eigen-Value = 958
	Loading Eigen-Value = 959
	Loading Eigen-Value = 960
	Loading Eigen-Value = 961
	Loading Eigen-Value = 962
	Loading Eigen-Value = 963
	Loading Eigen-Value = 964
	Loading Eigen-Value = 965
	Loading Eigen-Value = 966
	Loading Eigen-Value = 967
	Loading Eigen-Value = 968
	Loading Eigen-Value = 969
	Loading Eigen-Value = 970
	Loading Eigen-Value = 971
	Loading Eigen-Value = 972
	Loading Eigen-Value = 973
	Loading Eigen-Value = 974
	Loading Eigen-Value = 975
	Loading Eigen-Value = 976
	Loading Eigen-Value = 977
	Loading Eigen-Value = 978
	Loading Eigen-Value = 979
	Loading Eigen-Value = 980
	Loading Eigen-Value = 981
	Loading Eigen-Value = 982
	Loading Eigen-Value = 983
	Loading Eigen-Value = 984
	Loading Eigen-Value = 985
	Loading Eigen-Value = 986
	Loading Eigen-Value = 987
	Loading Eigen-Value = 988
	Loading Eigen-Value = 989
	Loading Eigen-Value = 990
	Loading Eigen-Value = 991
	Loading Eigen-Value = 992
	Loading Eigen-Value = 993
	Loading Eigen-Value = 994
	Loading Eigen-Value = 995
	Loading Eigen-Value = 996
	Loading Eigen-Value = 997
	Loading Eigen-Value = 998
	Loading Eigen-Value = 999
	Loading Eigen-Value = 1000
	Loading Eigen-Value = 1001
	Loading Eigen-Value = 1002
	Loading Eigen-Value = 1003
	Loading Eigen-Value = 1004
	Loading Eigen-Value = 1005
	Loading Eigen-Value = 1006
	Loading Eigen-Value = 1007
	Loading Eigen-Value = 1008
	Loading Eigen-Value = 1009
	Loading Eigen-Value = 1010
	Loading Eigen-Value = 1011
	Loading Eigen-Value = 1012
	Loading Eigen-Value = 1013
	Loading Eigen-Value = 1014
	Loading Eigen-Value = 1015
	Loading Eigen-Value = 1016
	Loading Eigen-Value = 1017
	Loading Eigen-Value = 1018
	Loading Eigen-Value = 1019
	Loading Eigen-Value = 1020
	Loading Eigen-Value = 1021
	Loading Eigen-Value = 1022
	Loading Eigen-Value = 1023
	Loading Eigen-Value = 1024
	Loading Eigen-Value = 1025
	Loading Eigen-Value = 1026
	Loading Eigen-Value = 1027
	Loading Eigen-Value = 1028
	Loading Eigen-Value = 1029
	Loading Eigen-Value = 1030
	Loading Eigen-Value = 1031
	Loading Eigen-Value = 1032
	Loading Eigen-Value = 1033
	Loading Eigen-Value = 1034
	Loading Eigen-Value = 1035
	Loading Eigen-Value = 1036
	Loading Eigen-Value = 1037
	Loading Eigen-Value = 1038
	Loading Eigen-Value = 1039
	Loading Eigen-Value = 1040
	Loading Eigen-Value = 1041
	Loading Eigen-Value = 1042
	Loading Eigen-Value = 1043
	Loading Eigen-Value = 1044
	Loading Eigen-Value = 1045
	Loading Eigen-Value = 1046
	Loading Eigen-Value = 1047
	Loading Eigen-Value = 1048
	Loading Eigen-Value = 1049
	Loading Eigen-Value = 1050
	Loading Eigen-Value = 1051
	Loading Eigen-Value = 1052
	Loading Eigen-Value = 1053
	Loading Eigen-Value = 1054
	Loading Eigen-Value = 1055
	Loading Eigen-Value = 1056
	Loading Eigen-Value = 1057
	Loading Eigen-Value = 1058
	Loading Eigen-Value = 1059
	Loading Eigen-Value = 1060
	Loading Eigen-Value = 1061
	Loading Eigen-Value = 1062
	Loading Eigen-Value = 1063
	Loading Eigen-Value = 1064
	Loading Eigen-Value = 1065
	Loading Eigen-Value = 1066
	Loading Eigen-Value = 1067
	Loading Eigen-Value = 1068
	Loading Eigen-Value = 1069
	Loading Eigen-Value = 1070
	Loading Eigen-Value = 1071
	Loading Eigen-Value = 1072
	Loading Eigen-Value = 1073
	Loading Eigen-Value = 1074
	Loading Eigen-Value = 1075
	Loading Eigen-Value = 1076
	Loading Eigen-Value = 1077
	Loading Eigen-Value = 1078
	Loading Eigen-Value = 1079
	Loading Eigen-Value = 1080
	Loading Eigen-Value = 1081
	Loading Eigen-Value = 1082
	Loading Eigen-Value = 1083
	Loading Eigen-Value = 1084
	Loading Eigen-Value = 1085
	Loading Eigen-Value = 1086
	Loading Eigen-Value = 1087
	Loading Eigen-Value = 1088
	Loading Eigen-Value = 1089
	Loading Eigen-Value = 1090
	Loading Eigen-Value = 1091
	Loading Eigen-Value = 1092
	Loading Eigen-Value = 1093
	Loading Eigen-Value = 1094
	Loading Eigen-Value = 1095
	Loading Eigen-Value = 1096
	Loading Eigen-Value = 1097
	Loading Eigen-Value = 1098
	Loading Eigen-Value = 1099
	Loading Eigen-Value = 1100
	Loading Eigen-Value = 1101
	Loading Eigen-Value = 1102
	Loading Eigen-Value = 1103
	Loading Eigen-Value = 1104
	Loading Eigen-Value = 1105
	Loading Eigen-Value = 1106
	Loading Eigen-Value = 1107
	Loading Eigen-Value = 1108
	Loading Eigen-Value = 1109
	Loading Eigen-Value = 1110
	Loading Eigen-Value = 1111
	Loading Eigen-Value = 1112
	Loading Eigen-Value = 1113
	Loading Eigen-Value = 1114
	Loading Eigen-Value = 1115
	Loading Eigen-Value = 1116
	Loading Eigen-Value = 1117
	Loading Eigen-Value = 1118
	Loading Eigen-Value = 1119
	Loading Eigen-Value = 1120
	Loading Eigen-Value = 1121
	Loading Eigen-Value = 1122
	Loading Eigen-Value = 1123
	Loading Eigen-Value = 1124
	Loading Eigen-Value = 1125
	Loading Eigen-Value = 1126
	Loading Eigen-Value = 1127
	Loading Eigen-Value = 1128
	Loading Eigen-Value = 1129
	Loading Eigen-Value = 1130
	Loading Eigen-Value = 1131
	Loading Eigen-Value = 1132
	Loading Eigen-Value = 1133
	Loading Eigen-Value = 1134
	Loading Eigen-Value = 1135
	Loading Eigen-Value = 1136
	Loading Eigen-Value = 1137
	Loading Eigen-Value = 1138
	Loading Eigen-Value = 1139
	Loading Eigen-Value = 1140
	Loading Eigen-Value = 1141
	Loading Eigen-Value = 1142
	Loading Eigen-Value = 1143
	Loading Eigen-Value = 1144
	Loading Eigen-Value = 1145
	Loading Eigen-Value = 1146
	Loading Eigen-Value = 1147
	Loading Eigen-Value = 1148
	Loading Eigen-Value = 1149
	Loading Eigen-Value = 1150
	Loading Eigen-Value = 1151
	Loading Eigen-Value = 1152
	Loading Eigen-Value = 1153
	Loading Eigen-Value = 1154
	Loading Eigen-Value = 1155
	Loading Eigen-Value = 1156
	Loading Eigen-Value = 1157
	Loading Eigen-Value = 1158
	Loading Eigen-Value = 1159
	Loading Eigen-Value = 1160
	Loading Eigen-Value = 1161
	Loading Eigen-Value = 1162
	Loading Eigen-Value = 1163
	Loading Eigen-Value = 1164
	Loading Eigen-Value = 1165
	Loading Eigen-Value = 1166
	Loading Eigen-Value = 1167
	Loading Eigen-Value = 1168
	Loading Eigen-Value = 1169
	Loading Eigen-Value = 1170
	Loading Eigen-Value = 1171
	Loading Eigen-Value = 1172
	Loading Eigen-Value = 1173
	Loading Eigen-Value = 1174
	Loading Eigen-Value = 1175
	Loading Eigen-Value = 1176
	Loading Eigen-Value = 1177
	Loading Eigen-Value = 1178
	Loading Eigen-Value = 1179
	Loading Eigen-Value = 1180
	Loading Eigen-Value = 1181
	Loading Eigen-Value = 1182
	Loading Eigen-Value = 1183
	Loading Eigen-Value = 1184
	Loading Eigen-Value = 1185
	Loading Eigen-Value = 1186
	Loading Eigen-Value = 1187
	Loading Eigen-Value = 1188
	Loading Eigen-Value = 1189
	Loading Eigen-Value = 1190
	Loading Eigen-Value = 1191
	Loading Eigen-Value = 1192
	Loading Eigen-Value = 1193
	Loading Eigen-Value = 1194
	Loading Eigen-Value = 1195
	Loading Eigen-Value = 1196
	Loading Eigen-Value = 1197
	Loading Eigen-Value = 1198
	Loading Eigen-Value = 1199
	Loading Eigen-Value = 1200
	Loading Eigen-Value = 1201
	Loading Eigen-Value = 1202
	Loading Eigen-Value = 1203
	Loading Eigen-Value = 1204
	Loading Eigen-Value = 1205
	Loading Eigen-Value = 1206
	Loading Eigen-Value = 1207
	Loading Eigen-Value = 1208
	Loading Eigen-Value = 1209
	Loading Eigen-Value = 1210
	Loading Eigen-Value = 1211
	Loading Eigen-Value = 1212
	Loading Eigen-Value = 1213
	Loading Eigen-Value = 1214
	Loading Eigen-Value = 1215
	Loading Eigen-Value = 1216
	Loading Eigen-Value = 1217
	Loading Eigen-Value = 1218
	Loading Eigen-Value = 1219
	Loading Eigen-Value = 1220
	Loading Eigen-Value = 1221
	Loading Eigen-Value = 1222
	Loading Eigen-Value = 1223
	Loading Eigen-Value = 1224
	Loading Eigen-Value = 1225
	Loading Eigen-Value = 1226
	Loading Eigen-Value = 1227
	Loading Eigen-Value = 1228
	Loading Eigen-Value = 1229
	Loading Eigen-Value = 1230
	Loading Eigen-Value = 1231
	Loading Eigen-Value = 1232
	Loading Eigen-Value = 1233
	Loading Eigen-Value = 1234
	Loading Eigen-Value = 1235
	Loading Eigen-Value = 1236
	Loading Eigen-Value = 1237
	Loading Eigen-Value = 1238
	Loading Eigen-Value = 1239
	Loading Eigen-Value = 1240
	Loading Eigen-Value = 1241
	Loading Eigen-Value = 1242
	Loading Eigen-Value = 1243
	Loading Eigen-Value = 1244
	Loading Eigen-Value = 1245
	Loading Eigen-Value = 1246
	Loading Eigen-Value = 1247
	Loading Eigen-Value = 1248
	Loading Eigen-Value = 1249
	Loading Eigen-Value = 1250
	Loading Eigen-Value = 1251
	Loading Eigen-Value = 1252
	Loading Eigen-Value = 1253
	Loading Eigen-Value = 1254
	Loading Eigen-Value = 1255
	Loading Eigen-Value = 1256
	Loading Eigen-Value = 1257
	Loading Eigen-Value = 1258
	Loading Eigen-Value = 1259
	Loading Eigen-Value = 1260
	Loading Eigen-Value = 1261
	Loading Eigen-Value = 1262
	Loading Eigen-Value = 1263
	Loading Eigen-Value = 1264
	Loading Eigen-Value = 1265
	Loading Eigen-Value = 1266
	Loading Eigen-Value = 1267
	Loading Eigen-Value = 1268
	Loading Eigen-Value = 1269
	Loading Eigen-Value = 1270
	Loading Eigen-Value = 1271
	Loading Eigen-Value = 1272
	Loading Eigen-Value = 1273
	Loading Eigen-Value = 1274
	Loading Eigen-Value = 1275
	Loading Eigen-Value = 1276
	Loading Eigen-Value = 1277
	Loading Eigen-Value = 1278
	Loading Eigen-Value = 1279
	Loading Eigen-Value = 1280
	Loading Eigen-Value = 1281
	Loading Eigen-Value = 1282
	Loading Eigen-Value = 1283
	Loading Eigen-Value = 1284
	Loading Eigen-Value = 1285
	Loading Eigen-Value = 1286
	Loading Eigen-Value = 1287
	Loading Eigen-Value = 1288
	Loading Eigen-Value = 1289
	Loading Eigen-Value = 1290
	Loading Eigen-Value = 1291
	Loading Eigen-Value = 1292
	Loading Eigen-Value = 1293
	Loading Eigen-Value = 1294
	Loading Eigen-Value = 1295
	Loading Eigen-Value = 1296
	Loading Eigen-Value = 1297
	Loading Eigen-Value = 1298
	Loading Eigen-Value = 1299
	Loading Eigen-Value = 1300
	Loading Eigen-Value = 1301
	Loading Eigen-Value = 1302
	Loading Eigen-Value = 1303
	Loading Eigen-Value = 1304
	Loading Eigen-Value = 1305
	Loading Eigen-Value = 1306
	Loading Eigen-Value = 1307
	Loading Eigen-Value = 1308
	Loading Eigen-Value = 1309
	Loading Eigen-Value = 1310
	Loading Eigen-Value = 1311
	Loading Eigen-Value = 1312
	Loading Eigen-Value = 1313
	Loading Eigen-Value = 1314
	Loading Eigen-Value = 1315
	Loading Eigen-Value = 1316
	Loading Eigen-Value = 1317
	Loading Eigen-Value = 1318
	Loading Eigen-Value = 1319
	Loading Eigen-Value = 1320
	Loading Eigen-Value = 1321
	Loading Eigen-Value = 1322
	Loading Eigen-Value = 1323
	Loading Eigen-Value = 1324
	Loading Eigen-Value = 1325
	Loading Eigen-Value = 1326
	Loading Eigen-Value = 1327
	Loading Eigen-Value = 1328
	Loading Eigen-Value = 1329
	Loading Eigen-Value = 1330
	Loading Eigen-Value = 1331
	Loading Eigen-Value = 1332
	Loading Eigen-Value = 1333
	Loading Eigen-Value = 1334
	Loading Eigen-Value = 1335
	Loading Eigen-Value = 1336
	Loading Eigen-Value = 1337
	Loading Eigen-Value = 1338
	Loading Eigen-Value = 1339
	Loading Eigen-Value = 1340
	Loading Eigen-Value = 1341
	Loading Eigen-Value = 1342
	Loading Eigen-Value = 1343
	Loading Eigen-Value = 1344
	Loading Eigen-Value = 1345
	Loading Eigen-Value = 1346
	Loading Eigen-Value = 1347
	Loading Eigen-Value = 1348
	Loading Eigen-Value = 1349
	Loading Eigen-Value = 1350
	Loading Eigen-Value = 1351
	Loading Eigen-Value = 1352
	Loading Eigen-Value = 1353
	Loading Eigen-Value = 1354
	Loading Eigen-Value = 1355
	Loading Eigen-Value = 1356
	Loading Eigen-Value = 1357
	Loading Eigen-Value = 1358
	Loading Eigen-Value = 1359
	Loading Eigen-Value = 1360
	Loading Eigen-Value = 1361
	Loading Eigen-Value = 1362
	Loading Eigen-Value = 1363
	Loading Eigen-Value = 1364
	Loading Eigen-Value = 1365
	Loading Eigen-Value = 1366
	Loading Eigen-Value = 1367
	Loading Eigen-Value = 1368
	Loading Eigen-Value = 1369
	Loading Eigen-Value = 1370
	Loading Eigen-Value = 1371
	Loading Eigen-Value = 1372
	Loading Eigen-Value = 1373
	Loading Eigen-Value = 1374
	Loading Eigen-Value = 1375
	Loading Eigen-Value = 1376
	Loading Eigen-Value = 1377
	Loading Eigen-Value = 1378
	Loading Eigen-Value = 1379
	Loading Eigen-Value = 1380
	Loading Eigen-Value = 1381
	Loading Eigen-Value = 1382
	Loading Eigen-Value = 1383
	Loading Eigen-Value = 1384
	Loading Eigen-Value = 1385
	Loading Eigen-Value = 1386
	Loading Eigen-Value = 1387
	Loading Eigen-Value = 1388
	Loading Eigen-Value = 1389
	Loading Eigen-Value = 1390
	Loading Eigen-Value = 1391
	Loading Eigen-Value = 1392
	Loading Eigen-Value = 1393
	Loading Eigen-Value = 1394
	Loading Eigen-Value = 1395
	Loading Eigen-Value = 1396
	Loading Eigen-Value = 1397
	Loading Eigen-Value = 1398
	Loading Eigen-Value = 1399
	Loading Eigen-Value = 1400
	Loading Eigen-Value = 1401
	Loading Eigen-Value = 1402
	Loading Eigen-Value = 1403
	Loading Eigen-Value = 1404
	Loading Eigen-Value = 1405
	Loading Eigen-Value = 1406
	Loading Eigen-Value = 1407
	Loading Eigen-Value = 1408
	Loading Eigen-Value = 1409
	Loading Eigen-Value = 1410
	Loading Eigen-Value = 1411
	Loading Eigen-Value = 1412
	Loading Eigen-Value = 1413
	Loading Eigen-Value = 1414
	Loading Eigen-Value = 1415
	Loading Eigen-Value = 1416
	Loading Eigen-Value = 1417
	Loading Eigen-Value = 1418
	Loading Eigen-Value = 1419
	Loading Eigen-Value = 1420
	Loading Eigen-Value = 1421
	Loading Eigen-Value = 1422
	Loading Eigen-Value = 1423
	Loading Eigen-Value = 1424
	Loading Eigen-Value = 1425
	Loading Eigen-Value = 1426
	Loading Eigen-Value = 1427
	Loading Eigen-Value = 1428
	Loading Eigen-Value = 1429
	Loading Eigen-Value = 1430
	Loading Eigen-Value = 1431
	Loading Eigen-Value = 1432
	Loading Eigen-Value = 1433
	Loading Eigen-Value = 1434
	Loading Eigen-Value = 1435
	Loading Eigen-Value = 1436
	Loading Eigen-Value = 1437
	Loading Eigen-Value = 1438
	Loading Eigen-Value = 1439
	Loading Eigen-Value = 1440
	Loading Eigen-Value = 1441
	Loading Eigen-Value = 1442
	Loading Eigen-Value = 1443
	Loading Eigen-Value = 1444
	Loading Eigen-Value = 1445
	Loading Eigen-Value = 1446
	Loading Eigen-Value = 1447
	Loading Eigen-Value = 1448
	Loading Eigen-Value = 1449
	Loading Eigen-Value = 1450
	Loading Eigen-Value = 1451
	Loading Eigen-Value = 1452
	Loading Eigen-Value = 1453
	Loading Eigen-Value = 1454
	Loading Eigen-Value = 1455
	Loading Eigen-Value = 1456
	Loading Eigen-Value = 1457
	Loading Eigen-Value = 1458
	Loading Eigen-Value = 1459
	Loading Eigen-Value = 1460
	Loading Eigen-Value = 1461
	Loading Eigen-Value = 1462
	Loading Eigen-Value = 1463
	Loading Eigen-Value = 1464
	Loading Eigen-Value = 1465
	Loading Eigen-Value = 1466
	Loading Eigen-Value = 1467
	Loading Eigen-Value = 1468
	Loading Eigen-Value = 1469
	Loading Eigen-Value = 1470
	Loading Eigen-Value = 1471
	Loading Eigen-Value = 1472
	Loading Eigen-Value = 1473
	Loading Eigen-Value = 1474
	Loading Eigen-Value = 1475
	Loading Eigen-Value = 1476
	Loading Eigen-Value = 1477
	Loading Eigen-Value = 1478
	Loading Eigen-Value = 1479
	Loading Eigen-Value = 1480
	Loading Eigen-Value = 1481
	Loading Eigen-Value = 1482
	Loading Eigen-Value = 1483
	Loading Eigen-Value = 1484
	Loading Eigen-Value = 1485
	Loading Eigen-Value = 1486
	Loading Eigen-Value = 1487
	Loading Eigen-Value = 1488
	Loading Eigen-Value = 1489
	Loading Eigen-Value = 1490
	Loading Eigen-Value = 1491
	Loading Eigen-Value = 1492
	Loading Eigen-Value = 1493
	Loading Eigen-Value = 1494
	Loading Eigen-Value = 1495
	Loading Eigen-Value = 1496
	Loading Eigen-Value = 1497
	Loading Eigen-Value = 1498
	Loading Eigen-Value = 1499
	Loading Eigen-Value = 1500
	Loading Eigen-Value = 1501
	Loading Eigen-Value = 1502
	Loading Eigen-Value = 1503
	Loading Eigen-Value = 1504
	Loading Eigen-Value = 1505
	Loading Eigen-Value = 1506
	Loading Eigen-Value = 1507
	Loading Eigen-Value = 1508
	Loading Eigen-Value = 1509
	Loading Eigen-Value = 1510
	Loading Eigen-Value = 1511
	Loading Eigen-Value = 1512
	Loading Eigen-Value = 1513
	Loading Eigen-Value = 1514
	Loading Eigen-Value = 1515
	Loading Eigen-Value = 1516
	Loading Eigen-Value = 1517
	Loading Eigen-Value = 1518
	Loading Eigen-Value = 1519
	Loading Eigen-Value = 1520
	Loading Eigen-Value = 1521
	Loading Eigen-Value = 1522
	Loading Eigen-Value = 1523
	Loading Eigen-Value = 1524
	Loading Eigen-Value = 1525
	Loading Eigen-Value = 1526
	Loading Eigen-Value = 1527
	Loading Eigen-Value = 1528
	Loading Eigen-Value = 1529
	Loading Eigen-Value = 1530
	Loading Eigen-Value = 1531
	Loading Eigen-Value = 1532
	Loading Eigen-Value = 1533
	Loading Eigen-Value = 1534
	Loading Eigen-Value = 1535
	Loading Eigen-Value = 1536
	Loading Eigen-Value = 1537
	Loading Eigen-Value = 1538
	Loading Eigen-Value = 1539
	Loading Eigen-Value = 1540
	Loading Eigen-Value = 1541
	Loading Eigen-Value = 1542
	Loading Eigen-Value = 1543
	Loading Eigen-Value = 1544
	Loading Eigen-Value = 1545
	Loading Eigen-Value = 1546
	Loading Eigen-Value = 1547
	Loading Eigen-Value = 1548
	Loading Eigen-Value = 1549
	Loading Eigen-Value = 1550
	Loading Eigen-Value = 1551
	Loading Eigen-Value = 1552
	Loading Eigen-Value = 1553
	Loading Eigen-Value = 1554
	Loading Eigen-Value = 1555
	Loading Eigen-Value = 1556
	Loading Eigen-Value = 1557
	Loading Eigen-Value = 1558
	Loading Eigen-Value = 1559
	Loading Eigen-Value = 1560
	Loading Eigen-Value = 1561
	Loading Eigen-Value = 1562
	Loading Eigen-Value = 1563
	Loading Eigen-Value = 1564
	Loading Eigen-Value = 1565
	Loading Eigen-Value = 1566
	Loading Eigen-Value = 1567
	Loading Eigen-Value = 1568
	Loading Eigen-Value = 1569
	Loading Eigen-Value = 1570
	Loading Eigen-Value = 1571
	Loading Eigen-Value = 1572
	Loading Eigen-Value = 1573
	Loading Eigen-Value = 1574
	Loading Eigen-Value = 1575
	Loading Eigen-Value = 1576
	Loading Eigen-Value = 1577
	Loading Eigen-Value = 1578
	Loading Eigen-Value = 1579
	Loading Eigen-Value = 1580
	Loading Eigen-Value = 1581
	Loading Eigen-Value = 1582
	Loading Eigen-Value = 1583
	Loading Eigen-Value = 1584
	Loading Eigen-Value = 1585
	Loading Eigen-Value = 1586
	Loading Eigen-Value = 1587
	Loading Eigen-Value = 1588
	Loading Eigen-Value = 1589
	Loading Eigen-Value = 1590
	Loading Eigen-Value = 1591
	Loading Eigen-Value = 1592
	Loading Eigen-Value = 1593
	Loading Eigen-Value = 1594
	Loading Eigen-Value = 1595
	Loading Eigen-Value = 1596
	Loading Eigen-Value = 1597
	Loading Eigen-Value = 1598
	Loading Eigen-Value = 1599
	Loading Eigen-Value = 1600
	Loading Eigen-Value = 1601
	Loading Eigen-Value = 1602
	Loading Eigen-Value = 1603
	Loading Eigen-Value = 1604
	Loading Eigen-Value = 1605
	Loading Eigen-Value = 1606
	Loading Eigen-Value = 1607
	Loading Eigen-Value = 1608
	Loading Eigen-Value = 1609
	Loading Eigen-Value = 1610
	Loading Eigen-Value = 1611
	Loading Eigen-Value = 1612
	Loading Eigen-Value = 1613
	Loading Eigen-Value = 1614
	Loading Eigen-Value = 1615
	Loading Eigen-Value = 1616
	Loading Eigen-Value = 1617
	Loading Eigen-Value = 1618
	Loading Eigen-Value = 1619
	Loading Eigen-Value = 1620
	Loading Eigen-Value = 1621
	Loading Eigen-Value = 1622
	Loading Eigen-Value = 1623
	Loading Eigen-Value = 1624
	Loading Eigen-Value = 1625
	Loading Eigen-Value = 1626
	Loading Eigen-Value = 1627
	Loading Eigen-Value = 1628
	Loading Eigen-Value = 1629
	Loading Eigen-Value = 1630
	Loading Eigen-Value = 1631
	Loading Eigen-Value = 1632
	Loading Eigen-Value = 1633
	Loading Eigen-Value = 1634
	Loading Eigen-Value = 1635
	Loading Eigen-Value = 1636
	Loading Eigen-Value = 1637
	Loading Eigen-Value = 1638
	Loading Eigen-Value = 1639
	Loading Eigen-Value = 1640
	Loading Eigen-Value = 1641
	Loading Eigen-Value = 1642
	Loading Eigen-Value = 1643
	Loading Eigen-Value = 1644
	Loading Eigen-Value = 1645
	Loading Eigen-Value = 1646
	Loading Eigen-Value = 1647
	Loading Eigen-Value = 1648
	Loading Eigen-Value = 1649
	Loading Eigen-Value = 1650
	Loading Eigen-Value = 1651
	Loading Eigen-Value = 1652
	Loading Eigen-Value = 1653
	Loading Eigen-Value = 1654
	Loading Eigen-Value = 1655
	Loading Eigen-Value = 1656
	Loading Eigen-Value = 1657
	Loading Eigen-Value = 1658
	Loading Eigen-Value = 1659
	Loading Eigen-Value = 1660
	Loading Eigen-Value = 1661
	Loading Eigen-Value = 1662
	Loading Eigen-Value = 1663
	Loading Eigen-Value = 1664
	Loading Eigen-Value = 1665
	Loading Eigen-Value = 1666
	Loading Eigen-Value = 1667
	Loading Eigen-Value = 1668
	Loading Eigen-Value = 1669
	Loading Eigen-Value = 1670
	Loading Eigen-Value = 1671
	Loading Eigen-Value = 1672
	Loading Eigen-Value = 1673
	Loading Eigen-Value = 1674
	Loading Eigen-Value = 1675
	Loading Eigen-Value = 1676
	Loading Eigen-Value = 1677
	Loading Eigen-Value = 1678
	Loading Eigen-Value = 1679
	Loading Eigen-Value = 1680
	Loading Eigen-Value = 1681
	Loading Eigen-Value = 1682
	Loading Eigen-Value = 1683
	Loading Eigen-Value = 1684
	Loading Eigen-Value = 1685
	Loading Eigen-Value = 1686
	Loading Eigen-Value = 1687
	Loading Eigen-Value = 1688
	Loading Eigen-Value = 1689
	Loading Eigen-Value = 1690
	Loading Eigen-Value = 1691
	Loading Eigen-Value = 1692
	Loading Eigen-Value = 1693
	Loading Eigen-Value = 1694
	Loading Eigen-Value = 1695
	Loading Eigen-Value = 1696
	Loading Eigen-Value = 1697
	Loading Eigen-Value = 1698
	Loading Eigen-Value = 1699
	Loading Eigen-Value = 1700
	Loading Eigen-Value = 1701
	Loading Eigen-Value = 1702
	Loading Eigen-Value = 1703
	Loading Eigen-Value = 1704
	Loading Eigen-Value = 1705
	Loading Eigen-Value = 1706
	Loading Eigen-Value = 1707
	Loading Eigen-Value = 1708
	Loading Eigen-Value = 1709
	Loading Eigen-Value = 1710
	Loading Eigen-Value = 1711
	Loading Eigen-Value = 1712
	Loading Eigen-Value = 1713
	Loading Eigen-Value = 1714
	Loading Eigen-Value = 1715
	Loading Eigen-Value = 1716
	Loading Eigen-Value = 1717
	Loading Eigen-Value = 1718
	Loading Eigen-Value = 1719
	Loading Eigen-Value = 1720
	Loading Eigen-Value = 1721
	Loading Eigen-Value = 1722
	Loading Eigen-Value = 1723
	Loading Eigen-Value = 1724
	Loading Eigen-Value = 1725
	Loading Eigen-Value = 1726
	Loading Eigen-Value = 1727
	Loading Eigen-Value = 1728
	Loading Eigen-Value = 1729
	Loading Eigen-Value = 1730
	Loading Eigen-Value = 1731
	Loading Eigen-Value = 1732
	Loading Eigen-Value = 1733
	Loading Eigen-Value = 1734
	Loading Eigen-Value = 1735
	Loading Eigen-Value = 1736
	Loading Eigen-Value = 1737
	Loading Eigen-Value = 1738
	Loading Eigen-Value = 1739
	Loading Eigen-Value = 1740
	Loading Eigen-Value = 1741
	Loading Eigen-Value = 1742
	Loading Eigen-Value = 1743
	Loading Eigen-Value = 1744
	Loading Eigen-Value = 1745
	Loading Eigen-Value = 1746
	Loading Eigen-Value = 1747
	Loading Eigen-Value = 1748
	Loading Eigen-Value = 1749
	Loading Eigen-Value = 1750
	Loading Eigen-Value = 1751
	Loading Eigen-Value = 1752
	Loading Eigen-Value = 1753
	Loading Eigen-Value = 1754
	Loading Eigen-Value = 1755
	Loading Eigen-Value = 1756
	Loading Eigen-Value = 1757
	Loading Eigen-Value = 1758
	Loading Eigen-Value = 1759
	Loading Eigen-Value = 1760
	Loading Eigen-Value = 1761
	Loading Eigen-Value = 1762
	Loading Eigen-Value = 1763
	Loading Eigen-Value = 1764
	Loading Eigen-Value = 1765
	Loading Eigen-Value = 1766
	Loading Eigen-Value = 1767
	Loading Eigen-Value = 1768
	Loading Eigen-Value = 1769
	Loading Eigen-Value = 1770
	Loading Eigen-Value = 1771
	Loading Eigen-Value = 1772
	Loading Eigen-Value = 1773
	Loading Eigen-Value = 1774
	Loading Eigen-Value = 1775
	Loading Eigen-Value = 1776
	Loading Eigen-Value = 1777
	Loading Eigen-Value = 1778
	Loading Eigen-Value = 1779
Natural freq (Mode 1) = 5.91752 (Hz)
Natural freq (Mode 2) = 29.92398 (Hz)
Natural freq (Mode 3) = 40.01939 (Hz)
Natural freq (Mode 4) = 78.26336 (Hz)
Natural freq (Mode 5) = 102.48770 (Hz)
Natural freq (Mode 6) = 148.28700 (Hz)
Natural freq (Mode 7) = 182.97520 (Hz)
Natural freq (Mode 8) = 238.39370 (Hz)
Natural freq (Mode 9) = 285.36330 (Hz)
Natural freq (Mode 10) = 321.90370 (Hz)
Natural freq (Mode 11) = 338.36210 (Hz)
Natural freq (Mode 12) = 347.87480 (Hz)
Natural freq (Mode 13) = 412.76490 (Hz)
Natural freq (Mode 14) = 446.89790 (Hz)
Natural freq (Mode 15) = 477.26050 (Hz)
Natural freq (Mode 16) = 556.73130 (Hz)
Natural freq (Mode 17) = 582.55570 (Hz)
Natural freq (Mode 18) = 627.20430 (Hz)
Natural freq (Mode 19) = 696.67300 (Hz)
Natural freq (Mode 20) = 750.94670 (Hz)
Natural freq (Mode 21) = 757.10910 (Hz)
Natural freq (Mode 22) = 797.86110 (Hz)
Natural freq (Mode 23) = 847.03330 (Hz)
Natural freq (Mode 24) = 944.72760 (Hz)
Natural freq (Mode 25) = 956.33970 (Hz)
Natural freq (Mode 26) = 978.56320 (Hz)
Natural freq (Mode 27) = 1011.29500 (Hz)
Natural freq (Mode 28) = 1121.40300 (Hz)
Natural freq (Mode 29) = 1155.17800 (Hz)
Natural freq (Mode 30) = 1174.22000 (Hz)
Natural freq (Mode 31) = 1218.32400 (Hz)
Natural freq (Mode 32) = 1289.59300 (Hz)
Natural freq (Mode 33) = 1300.85200 (Hz)
Natural freq (Mode 34) = 1332.20600 (Hz)
Natural freq (Mode 35) = 1359.39700 (Hz)
Natural freq (Mode 36) = 1412.35900 (Hz)
Natural freq (Mode 37) = 1457.87000 (Hz)
Natural freq (Mode 38) = 1504.80200 (Hz)
Natural freq (Mode 39) = 1555.90000 (Hz)
Natural freq (Mode 40) = 1607.07800 (Hz)
Natural freq (Mode 41) = 1655.47400 (Hz)
Natural freq (Mode 42) = 1717.08000 (Hz)
Natural freq (Mode 43) = 1741.97300 (Hz)
Natural freq (Mode 44) = 1801.38700 (Hz)
Natural freq (Mode 45) = 1873.31100 (Hz)
Natural freq (Mode 46) = 1913.09800 (Hz)
Natural freq (Mode 47) = 1980.26900 (Hz)
Natural freq (Mode 48) = 1991.99800 (Hz)
Natural freq (Mode 49) = 2069.91300 (Hz)
Natural freq (Mode 50) = 2113.76400 (Hz)
Natural freq (Mode 51) = 2145.78500 (Hz)
Natural freq (Mode 52) = 2175.50900 (Hz)
Natural freq (Mode 53) = 2224.13400 (Hz)
Natural freq (Mode 54) = 2298.75800 (Hz)
Natural freq (Mode 55) = 2349.76500 (Hz)
Natural freq (Mode 56) = 2413.31600 (Hz)
Natural freq (Mode 57) = 2439.34000 (Hz)
Natural freq (Mode 58) = 2497.21500 (Hz)
Natural freq (Mode 59) = 2499.99000 (Hz)
Natural freq (Mode 60) = 2549.47200 (Hz)
Natural freq (Mode 61) = 2608.88800 (Hz)
Natural freq (Mode 62) = 2632.75600 (Hz)
Natural freq (Mode 63) = 2710.43000 (Hz)
Natural freq (Mode 64) = 2747.45500 (Hz)
Natural freq (Mode 65) = 2787.56600 (Hz)
Natural freq (Mode 66) = 2804.88200 (Hz)
Natural freq (Mode 67) = 2828.01000 (Hz)
Natural freq (Mode 68) = 2891.33900 (Hz)
Natural freq (Mode 69) = 2943.88700 (Hz)
Natural freq (Mode 70) = 2996.34500 (Hz)
Natural freq (Mode 71) = 3038.47900 (Hz)
Natural freq (Mode 72) = 3110.97300 (Hz)
Natural freq (Mode 73) = 3155.74800 (Hz)
Natural freq (Mode 74) = 3171.54500 (Hz)
Natural freq (Mode 75) = 3208.80000 (Hz)
Natural freq (Mode 76) = 3270.76600 (Hz)
Natural freq (Mode 77) = 3337.48000 (Hz)
Natural freq (Mode 78) = 3397.62800 (Hz)
Natural freq (Mode 79) = 3430.15700 (Hz)
Natural freq (Mode 80) = 3486.27900 (Hz)
Natural freq (Mode 81) = 3519.90500 (Hz)
Natural freq (Mode 82) = 3582.41700 (Hz)
Natural freq (Mode 83) = 3644.34000 (Hz)
Natural freq (Mode 84) = 3690.50500 (Hz)
Natural freq (Mode 85) = 3709.94700 (Hz)
Natural freq (Mode 86) = 3751.86800 (Hz)
Natural freq (Mode 87) = 3847.60300 (Hz)
Natural freq (Mode 88) = 3881.69700 (Hz)
Natural freq (Mode 89) = 3929.56900 (Hz)
Natural freq (Mode 90) = 4030.33000 (Hz)
Natural freq (Mode 91) = 4075.24600 (Hz)
Natural freq (Mode 92) = 4112.23100 (Hz)
Natural freq (Mode 93) = 4125.08800 (Hz)
Natural freq (Mode 94) = 4175.94300 (Hz)
Natural freq (Mode 95) = 4249.31900 (Hz)
Natural freq (Mode 96) = 4326.93400 (Hz)
Natural freq (Mode 97) = 4350.07800 (Hz)
Natural freq (Mode 98) = 4422.66200 (Hz)
Natural freq (Mode 99) = 4433.83300 (Hz)
Natural freq (Mode 100) = 4490.80200 (Hz)
Natural freq (Mode 101) = 4533.85600 (Hz)
Natural freq (Mode 102) = 4575.81800 (Hz)
Natural freq (Mode 103) = 4650.17200 (Hz)
Natural freq (Mode 104) = 4653.01800 (Hz)
Natural freq (Mode 105) = 4762.06400 (Hz)
Natural freq (Mode 106) = 4783.26800 (Hz)
Natural freq (Mode 107) = 4833.77500 (Hz)
Natural freq (Mode 108) = 4859.19300 (Hz)
Natural freq (Mode 109) = 4906.46000 (Hz)
Natural freq (Mode 110) = 4983.49100 (Hz)
Natural freq (Mode 111) = 5036.52400 (Hz)
Natural freq (Mode 112) = 5088.89300 (Hz)
Natural freq (Mode 113) = 5131.49800 (Hz)
Natural freq (Mode 114) = 5189.45600 (Hz)
Natural freq (Mode 115) = 5226.69000 (Hz)
Natural freq (Mode 116) = 5312.39900 (Hz)
Natural freq (Mode 117) = 5337.54300 (Hz)
Natural freq (Mode 118) = 5412.15200 (Hz)
Natural freq (Mode 119) = 5468.34800 (Hz)
Natural freq (Mode 120) = 5515.48600 (Hz)
Natural freq (Mode 121) = 5524.08000 (Hz)
Natural freq (Mode 122) = 5619.29500 (Hz)
Natural freq (Mode 123) = 5653.70400 (Hz)
Natural freq (Mode 124) = 5733.63600 (Hz)
Natural freq (Mode 125) = 5773.94900 (Hz)
Natural freq (Mode 126) = 5844.35200 (Hz)
Natural freq (Mode 127) = 5867.65000 (Hz)
Natural freq (Mode 128) = 5906.70100 (Hz)
Natural freq (Mode 129) = 5971.92900 (Hz)
Natural freq (Mode 130) = 6009.02100 (Hz)
Natural freq (Mode 131) = 6072.23100 (Hz)
Natural freq (Mode 132) = 6114.32400 (Hz)
Natural freq (Mode 133) = 6217.45300 (Hz)
Natural freq (Mode 134) = 6258.33500 (Hz)
Natural freq (Mode 135) = 6280.35900 (Hz)
Natural freq (Mode 136) = 6328.06800 (Hz)
Natural freq (Mode 137) = 6380.03600 (Hz)
Natural freq (Mode 138) = 6420.51900 (Hz)
Natural freq (Mode 139) = 6443.62300 (Hz)
Natural freq (Mode 140) = 6482.95600 (Hz)
Natural freq (Mode 141) = 6556.30700 (Hz)
Natural freq (Mode 142) = 6581.93700 (Hz)
Natural freq (Mode 143) = 6681.89000 (Hz)
Natural freq (Mode 144) = 6710.49400 (Hz)
Natural freq (Mode 145) = 6712.56300 (Hz)
Natural freq (Mode 146) = 6757.85200 (Hz)
Natural freq (Mode 147) = 6773.85300 (Hz)
Natural freq (Mode 148) = 6855.24800 (Hz)
Natural freq (Mode 149) = 6906.85000 (Hz)
Natural freq (Mode 150) = 6964.86500 (Hz)
Natural freq (Mode 151) = 7005.47200 (Hz)
Natural freq (Mode 152) = 7093.12700 (Hz)
Natural freq (Mode 153) = 7172.58500 (Hz)
Natural freq (Mode 154) = 7235.36700 (Hz)
Natural freq (Mode 155) = 7284.38800 (Hz)
Natural freq (Mode 156) = 7339.50900 (Hz)
Natural freq (Mode 157) = 7387.76000 (Hz)
Natural freq (Mode 158) = 7432.07800 (Hz)
Natural freq (Mode 159) = 7484.19100 (Hz)
Natural freq (Mode 160) = 7505.65500 (Hz)
Natural freq (Mode 161) = 7575.40800 (Hz)
Natural freq (Mode 162) = 7619.31300 (Hz)
Natural freq (Mode 163) = 7645.70400 (Hz)
Natural freq (Mode 164) = 7763.99600 (Hz)
Natural freq (Mode 165) = 7804.56500 (Hz)
Natural freq (Mode 166) = 7847.62900 (Hz)
Natural freq (Mode 167) = 7884.94000 (Hz)
Natural freq (Mode 168) = 7971.14100 (Hz)
Natural freq (Mode 169) = 7981.26000 (Hz)
Natural freq (Mode 170) = 8018.25500 (Hz)
Natural freq (Mode 171) = 8065.35200 (Hz)
Natural freq (Mode 172) = 8190.58300 (Hz)
Natural freq (Mode 173) = 8219.15300 (Hz)
Natural freq (Mode 174) = 8242.49900 (Hz)
Natural freq (Mode 175) = 8305.01600 (Hz)
Natural freq (Mode 176) = 8338.74300 (Hz)
Natural freq (Mode 177) = 8449.34200 (Hz)
Natural freq (Mode 178) = 8515.47200 (Hz)
Natural freq (Mode 179) = 8589.43700 (Hz)
Natural freq (Mode 180) = 8616.56100 (Hz)
Natural freq (Mode 181) = 8640.13700 (Hz)
Natural freq (Mode 182) = 8712.28800 (Hz)
Natural freq (Mode 183) = 8716.81500 (Hz)
Natural freq (Mode 184) = 8787.58300 (Hz)
Natural freq (Mode 185) = 8846.56900 (Hz)
Natural freq (Mode 186) = 8875.50500 (Hz)
Natural freq (Mode 187) = 8964.94700 (Hz)
Natural freq (Mode 188) = 8992.86500 (Hz)
Natural freq (Mode 189) = 9077.22400 (Hz)
Natural freq (Mode 190) = 9096.26100 (Hz)
Natural freq (Mode 191) = 9145.99500 (Hz)
Natural freq (Mode 192) = 9199.71100 (Hz)
Natural freq (Mode 193) = 9239.19700 (Hz)
Natural freq (Mode 194) = 9335.28900 (Hz)
Natural freq (Mode 195) = 9367.16700 (Hz)
Natural freq (Mode 196) = 9496.20700 (Hz)
Natural freq (Mode 197) = 9506.20900 (Hz)
Natural freq (Mode 198) = 9530.04800 (Hz)
Natural freq (Mode 199) = 9569.59000 (Hz)
Natural freq (Mode 200) = 9612.48400 (Hz)
Natural freq (Mode 201) = 9670.18300 (Hz)
Natural freq (Mode 202) = 9702.23300 (Hz)
Natural freq (Mode 203) = 9772.30000 (Hz)
Natural freq (Mode 204) = 9825.17600 (Hz)
Natural freq (Mode 205) = 9883.47700 (Hz)
Natural freq (Mode 206) = 9901.35100 (Hz)
Natural freq (Mode 207) = 9952.14500 (Hz)
Natural freq (Mode 208) = 10096.61000 (Hz)
Natural freq (Mode 209) = 10117.51000 (Hz)
Natural freq (Mode 210) = 10152.60000 (Hz)
Natural freq (Mode 211) = 10241.89000 (Hz)
Natural freq (Mode 212) = 10283.19000 (Hz)
Natural freq (Mode 213) = 10290.01000 (Hz)
Natural freq (Mode 214) = 10313.76000 (Hz)
Natural freq (Mode 215) = 10380.63000 (Hz)
Natural freq (Mode 216) = 10423.29000 (Hz)
Natural freq (Mode 217) = 10489.16000 (Hz)
Natural freq (Mode 218) = 10534.94000 (Hz)
Natural freq (Mode 219) = 10617.34000 (Hz)
Natural freq (Mode 220) = 10692.66000 (Hz)
Natural freq (Mode 221) = 10724.57000 (Hz)
Natural freq (Mode 222) = 10783.30000 (Hz)
Natural freq (Mode 223) = 10796.14000 (Hz)
Natural freq (Mode 224) = 10837.42000 (Hz)
Natural freq (Mode 225) = 10917.22000 (Hz)
Natural freq (Mode 226) = 10990.39000 (Hz)
Natural freq (Mode 227) = 11032.01000 (Hz)
Natural freq (Mode 228) = 11066.56000 (Hz)
Natural freq (Mode 229) = 11107.64000 (Hz)
Natural freq (Mode 230) = 11181.18000 (Hz)
Natural freq (Mode 231) = 11203.75000 (Hz)
Natural freq (Mode 232) = 11301.06000 (Hz)
Natural freq (Mode 233) = 11368.84000 (Hz)
Natural freq (Mode 234) = 11405.65000 (Hz)
Natural freq (Mode 235) = 11479.89000 (Hz)
Natural freq (Mode 236) = 11556.38000 (Hz)
Natural freq (Mode 237) = 11582.24000 (Hz)
Natural freq (Mode 238) = 11608.71000 (Hz)
Natural freq (Mode 239) = 11663.11000 (Hz)
Natural freq (Mode 240) = 11767.24000 (Hz)
Natural freq (Mode 241) = 11809.88000 (Hz)
Natural freq (Mode 242) = 11869.78000 (Hz)
Natural freq (Mode 243) = 11968.82000 (Hz)
Natural freq (Mode 244) = 11983.42000 (Hz)
Natural freq (Mode 245) = 12042.58000 (Hz)
Natural freq (Mode 246) = 12116.63000 (Hz)
Natural freq (Mode 247) = 12143.37000 (Hz)
Natural freq (Mode 248) = 12143.61000 (Hz)
Natural freq (Mode 249) = 12189.26000 (Hz)
Natural freq (Mode 250) = 12256.66000 (Hz)
Natural freq (Mode 251) = 12310.75000 (Hz)
Natural freq (Mode 252) = 12364.03000 (Hz)
Natural freq (Mode 253) = 12370.65000 (Hz)
Natural freq (Mode 254) = 12548.26000 (Hz)
Natural freq (Mode 255) = 12565.68000 (Hz)
Natural freq (Mode 256) = 12594.88000 (Hz)
Natural freq (Mode 257) = 12712.07000 (Hz)
Natural freq (Mode 258) = 12770.17000 (Hz)
Natural freq (Mode 259) = 12775.62000 (Hz)
Natural freq (Mode 260) = 12825.19000 (Hz)
Natural freq (Mode 261) = 12905.15000 (Hz)
Natural freq (Mode 262) = 12955.70000 (Hz)
Natural freq (Mode 263) = 13036.73000 (Hz)
Natural freq (Mode 264) = 13054.72000 (Hz)
Natural freq (Mode 265) = 13161.42000 (Hz)
Natural freq (Mode 266) = 13192.61000 (Hz)
Natural freq (Mode 267) = 13239.57000 (Hz)
Natural freq (Mode 268) = 13284.37000 (Hz)
Natural freq (Mode 269) = 13384.14000 (Hz)
Natural freq (Mode 270) = 13408.39000 (Hz)
Natural freq (Mode 271) = 13456.16000 (Hz)
Natural freq (Mode 272) = 13472.22000 (Hz)
Natural freq (Mode 273) = 13530.73000 (Hz)
Natural freq (Mode 274) = 13593.85000 (Hz)
Natural freq (Mode 275) = 13760.49000 (Hz)
Natural freq (Mode 276) = 13785.68000 (Hz)
Natural freq (Mode 277) = 13876.39000 (Hz)
Natural freq (Mode 278) = 13897.87000 (Hz)
Natural freq (Mode 279) = 13949.89000 (Hz)
Natural freq (Mode 280) = 13982.83000 (Hz)
Natural freq (Mode 281) = 14036.06000 (Hz)
Natural freq (Mode 282) = 14061.26000 (Hz)
Natural freq (Mode 283) = 14126.31000 (Hz)
Natural freq (Mode 284) = 14289.37000 (Hz)
Natural freq (Mode 285) = 14326.99000 (Hz)
Natural freq (Mode 286) = 14398.55000 (Hz)
Natural freq (Mode 287) = 14484.76000 (Hz)
Natural freq (Mode 288) = 14489.28000 (Hz)
Natural freq (Mode 289) = 14522.37000 (Hz)
Natural freq (Mode 290) = 14565.89000 (Hz)
Natural freq (Mode 291) = 14606.46000 (Hz)
Natural freq (Mode 292) = 14649.44000 (Hz)
Natural freq (Mode 293) = 14786.59000 (Hz)
Natural freq (Mode 294) = 14893.02000 (Hz)
Natural freq (Mode 295) = 14975.89000 (Hz)
Natural freq (Mode 296) = 14990.37000 (Hz)
Natural freq (Mode 297) = 15048.04000 (Hz)
Natural freq (Mode 298) = 15137.92000 (Hz)
Natural freq (Mode 299) = 15180.15000 (Hz)
Natural freq (Mode 300) = 15208.71000 (Hz)
Natural freq (Mode 301) = 15324.33000 (Hz)
Natural freq (Mode 302) = 15358.41000 (Hz)
Natural freq (Mode 303) = 15371.80000 (Hz)
Natural freq (Mode 304) = 15469.29000 (Hz)
Natural freq (Mode 305) = 15502.22000 (Hz)
Natural freq (Mode 306) = 15582.06000 (Hz)
Natural freq (Mode 307) = 15697.16000 (Hz)
Natural freq (Mode 308) = 15716.81000 (Hz)
Natural freq (Mode 309) = 15838.63000 (Hz)
Natural freq (Mode 310) = 15881.20000 (Hz)
Natural freq (Mode 311) = 15983.89000 (Hz)
Natural freq (Mode 312) = 15994.51000 (Hz)
Natural freq (Mode 313) = 16002.53000 (Hz)
Natural freq (Mode 314) = 16137.48000 (Hz)
Natural freq (Mode 315) = 16143.49000 (Hz)
Natural freq (Mode 316) = 16191.25000 (Hz)
Natural freq (Mode 317) = 16444.55000 (Hz)
Natural freq (Mode 318) = 16465.20000 (Hz)
Natural freq (Mode 319) = 16540.14000 (Hz)
Natural freq (Mode 320) = 16545.05000 (Hz)
Natural freq (Mode 321) = 16607.63000 (Hz)
Natural freq (Mode 322) = 16787.41000 (Hz)
Natural freq (Mode 323) = 16809.01000 (Hz)
Natural freq (Mode 324) = 16854.44000 (Hz)
Natural freq (Mode 325) = 16898.50000 (Hz)
Natural freq (Mode 326) = 16931.53000 (Hz)
Natural freq (Mode 327) = 16952.62000 (Hz)
Natural freq (Mode 328) = 17074.71000 (Hz)
Natural freq (Mode 329) = 17099.57000 (Hz)
Natural freq (Mode 330) = 17119.86000 (Hz)
Natural freq (Mode 331) = 17222.80000 (Hz)
Natural freq (Mode 332) = 17266.61000 (Hz)
Natural freq (Mode 333) = 17383.30000 (Hz)
Natural freq (Mode 334) = 17418.65000 (Hz)
Natural freq (Mode 335) = 17488.28000 (Hz)
Natural freq (Mode 336) = 17541.06000 (Hz)
Natural freq (Mode 337) = 17694.88000 (Hz)
Natural freq (Mode 338) = 17700.81000 (Hz)
Natural freq (Mode 339) = 17741.71000 (Hz)
Natural freq (Mode 340) = 17800.10000 (Hz)
Natural freq (Mode 341) = 17816.33000 (Hz)
Natural freq (Mode 342) = 17925.23000 (Hz)
Natural freq (Mode 343) = 17964.70000 (Hz)
Natural freq (Mode 344) = 18050.17000 (Hz)
Natural freq (Mode 345) = 18098.53000 (Hz)
Natural freq (Mode 346) = 18131.22000 (Hz)
Natural freq (Mode 347) = 18183.38000 (Hz)
Natural freq (Mode 348) = 18215.32000 (Hz)
Natural freq (Mode 349) = 18334.29000 (Hz)
Natural freq (Mode 350) = 18362.53000 (Hz)
Natural freq (Mode 351) = 18486.87000 (Hz)
Natural freq (Mode 352) = 18591.83000 (Hz)
Natural freq (Mode 353) = 18709.08000 (Hz)
Natural freq (Mode 354) = 18712.34000 (Hz)
Natural freq (Mode 355) = 18799.42000 (Hz)
Natural freq (Mode 356) = 18829.22000 (Hz)
Natural freq (Mode 357) = 18853.39000 (Hz)
Natural freq (Mode 358) = 18976.00000 (Hz)
Natural freq (Mode 359) = 19059.20000 (Hz)
Natural freq (Mode 360) = 19125.02000 (Hz)
Natural freq (Mode 361) = 19157.08000 (Hz)
Natural freq (Mode 362) = 19255.37000 (Hz)
Natural freq (Mode 363) = 19304.60000 (Hz)
Natural freq (Mode 364) = 19419.35000 (Hz)
Natural freq (Mode 365) = 19455.45000 (Hz)
Natural freq (Mode 366) = 19511.95000 (Hz)
Natural freq (Mode 367) = 19591.56000 (Hz)
Natural freq (Mode 368) = 19646.65000 (Hz)
Natural freq (Mode 369) = 19757.04000 (Hz)
Natural freq (Mode 370) = 19782.00000 (Hz)
Natural freq (Mode 371) = 19921.47000 (Hz)
Natural freq (Mode 372) = 20038.24000 (Hz)
Natural freq (Mode 373) = 20087.59000 (Hz)
Natural freq (Mode 374) = 20247.26000 (Hz)
Natural freq (Mode 375) = 20314.55000 (Hz)
Natural freq (Mode 376) = 20347.61000 (Hz)
Natural freq (Mode 377) = 20409.15000 (Hz)
Natural freq (Mode 378) = 20555.38000 (Hz)
Natural freq (Mode 379) = 20745.27000 (Hz)
Natural freq (Mode 380) = 20826.08000 (Hz)
Natural freq (Mode 381) = 20926.47000 (Hz)
Natural freq (Mode 382) = 20927.93000 (Hz)
Natural freq (Mode 383) = 20961.74000 (Hz)
Natural freq (Mode 384) = 21049.74000 (Hz)
Natural freq (Mode 385) = 21086.09000 (Hz)
Natural freq (Mode 386) = 21226.15000 (Hz)
Natural freq (Mode 387) = 21285.19000 (Hz)
Natural freq (Mode 388) = 21322.08000 (Hz)
Natural freq (Mode 389) = 21443.02000 (Hz)
Natural freq (Mode 390) = 21485.59000 (Hz)
Natural freq (Mode 391) = 21498.71000 (Hz)
Natural freq (Mode 392) = 21600.59000 (Hz)
Natural freq (Mode 393) = 21699.40000 (Hz)
Natural freq (Mode 394) = 21749.01000 (Hz)
Natural freq (Mode 395) = 21760.19000 (Hz)
Natural freq (Mode 396) = 21871.83000 (Hz)
Natural freq (Mode 397) = 21968.82000 (Hz)
Natural freq (Mode 398) = 22004.93000 (Hz)
Natural freq (Mode 399) = 22037.06000 (Hz)
Natural freq (Mode 400) = 22132.05000 (Hz)
Natural freq (Mode 401) = 22272.75000 (Hz)
Natural freq (Mode 402) = 22284.71000 (Hz)
Natural freq (Mode 403) = 22343.19000 (Hz)
Natural freq (Mode 404) = 22492.85000 (Hz)
Natural freq (Mode 405) = 22675.22000 (Hz)
Natural freq (Mode 406) = 22726.67000 (Hz)
Natural freq (Mode 407) = 22795.38000 (Hz)
Natural freq (Mode 408) = 22847.12000 (Hz)
Natural freq (Mode 409) = 23027.21000 (Hz)
Natural freq (Mode 410) = 23066.16000 (Hz)
Natural freq (Mode 411) = 23111.55000 (Hz)
Natural freq (Mode 412) = 23264.07000 (Hz)
Natural freq (Mode 413) = 23277.39000 (Hz)
Natural freq (Mode 414) = 23280.87000 (Hz)
Natural freq (Mode 415) = 23489.27000 (Hz)
Natural freq (Mode 416) = 23508.29000 (Hz)
Natural freq (Mode 417) = 23538.90000 (Hz)
Natural freq (Mode 418) = 23734.87000 (Hz)
Natural freq (Mode 419) = 23748.21000 (Hz)
Natural freq (Mode 420) = 23776.47000 (Hz)
Natural freq (Mode 421) = 23836.88000 (Hz)
Natural freq (Mode 422) = 23851.33000 (Hz)
Natural freq (Mode 423) = 23996.21000 (Hz)
Natural freq (Mode 424) = 24072.71000 (Hz)
Natural freq (Mode 425) = 24231.38000 (Hz)
Natural freq (Mode 426) = 24326.89000 (Hz)
Natural freq (Mode 427) = 24335.46000 (Hz)
Natural freq (Mode 428) = 24378.13000 (Hz)
Natural freq (Mode 429) = 24422.91000 (Hz)
Natural freq (Mode 430) = 24535.55000 (Hz)
Natural freq (Mode 431) = 24612.28000 (Hz)
Natural freq (Mode 432) = 24749.69000 (Hz)
Natural freq (Mode 433) = 24864.25000 (Hz)
Natural freq (Mode 434) = 25020.23000 (Hz)
Natural freq (Mode 435) = 25036.26000 (Hz)
Natural freq (Mode 436) = 25255.07000 (Hz)
Natural freq (Mode 437) = 25348.07000 (Hz)
Natural freq (Mode 438) = 25376.09000 (Hz)
Natural freq (Mode 439) = 25408.28000 (Hz)
Natural freq (Mode 440) = 25484.80000 (Hz)
Natural freq (Mode 441) = 25615.76000 (Hz)
Natural freq (Mode 442) = 25669.87000 (Hz)
Natural freq (Mode 443) = 25819.13000 (Hz)
Natural freq (Mode 444) = 25981.25000 (Hz)
Natural freq (Mode 445) = 25999.63000 (Hz)
Natural freq (Mode 446) = 26070.56000 (Hz)
Natural freq (Mode 447) = 26145.77000 (Hz)
Natural freq (Mode 448) = 26279.59000 (Hz)
Natural freq (Mode 449) = 26351.51000 (Hz)
Natural freq (Mode 450) = 26395.38000 (Hz)
Natural freq (Mode 451) = 26502.02000 (Hz)
Natural freq (Mode 452) = 26532.53000 (Hz)
Natural freq (Mode 453) = 26637.85000 (Hz)
Natural freq (Mode 454) = 26643.48000 (Hz)
Natural freq (Mode 455) = 26745.91000 (Hz)
Natural freq (Mode 456) = 26934.27000 (Hz)
Natural freq (Mode 457) = 27070.38000 (Hz)
Natural freq (Mode 458) = 27164.86000 (Hz)
Natural freq (Mode 459) = 27237.99000 (Hz)
Natural freq (Mode 460) = 27380.39000 (Hz)
Natural freq (Mode 461) = 27500.71000 (Hz)
Natural freq (Mode 462) = 27556.49000 (Hz)
Natural freq (Mode 463) = 27702.19000 (Hz)
Natural freq (Mode 464) = 27702.94000 (Hz)
Natural freq (Mode 465) = 27916.39000 (Hz)
Natural freq (Mode 466) = 28012.95000 (Hz)
Natural freq (Mode 467) = 28161.58000 (Hz)
Natural freq (Mode 468) = 28179.12000 (Hz)
Natural freq (Mode 469) = 28422.62000 (Hz)
Natural freq (Mode 470) = 28474.77000 (Hz)
Natural freq (Mode 471) = 28560.92000 (Hz)
Natural freq (Mode 472) = 28566.15000 (Hz)
Natural freq (Mode 473) = 28710.87000 (Hz)
Natural freq (Mode 474) = 28781.45000 (Hz)
Natural freq (Mode 475) = 28999.03000 (Hz)
Natural freq (Mode 476) = 29078.86000 (Hz)
Natural freq (Mode 477) = 29154.48000 (Hz)
Natural freq (Mode 478) = 29296.92000 (Hz)
Natural freq (Mode 479) = 29356.81000 (Hz)
Natural freq (Mode 480) = 29380.71000 (Hz)
Natural freq (Mode 481) = 29478.38000 (Hz)
Natural freq (Mode 482) = 29553.13000 (Hz)
Natural freq (Mode 483) = 29622.04000 (Hz)
Natural freq (Mode 484) = 29712.53000 (Hz)
Natural freq (Mode 485) = 30011.06000 (Hz)
Natural freq (Mode 486) = 30035.66000 (Hz)
Natural freq (Mode 487) = 30102.46000 (Hz)
Natural freq (Mode 488) = 30209.47000 (Hz)
Natural freq (Mode 489) = 30280.31000 (Hz)
Natural freq (Mode 490) = 30323.96000 (Hz)
Natural freq (Mode 491) = 30365.31000 (Hz)
Natural freq (Mode 492) = 30520.68000 (Hz)
Natural freq (Mode 493) = 30541.57000 (Hz)
Natural freq (Mode 494) = 30606.26000 (Hz)
Natural freq (Mode 495) = 30742.72000 (Hz)
Natural freq (Mode 496) = 30869.45000 (Hz)
Natural freq (Mode 497) = 30969.95000 (Hz)
Natural freq (Mode 498) = 31100.58000 (Hz)
Natural freq (Mode 499) = 31169.65000 (Hz)
Natural freq (Mode 500) = 31244.07000 (Hz)
Natural freq (Mode 501) = 31425.86000 (Hz)
Natural freq (Mode 502) = 31537.51000 (Hz)
Natural freq (Mode 503) = 31639.96000 (Hz)
Natural freq (Mode 504) = 31754.34000 (Hz)
Natural freq (Mode 505) = 31760.84000 (Hz)
Natural freq (Mode 506) = 31883.20000 (Hz)
Natural freq (Mode 507) = 32002.92000 (Hz)
Natural freq (Mode 508) = 32220.74000 (Hz)
Natural freq (Mode 509) = 32290.88000 (Hz)
Natural freq (Mode 510) = 32391.40000 (Hz)
Natural freq (Mode 511) = 32608.03000 (Hz)
Natural freq (Mode 512) = 32647.91000 (Hz)
Natural freq (Mode 513) = 32720.89000 (Hz)
Natural freq (Mode 514) = 32949.41000 (Hz)
Natural freq (Mode 515) = 32988.75000 (Hz)
Natural freq (Mode 516) = 33115.60000 (Hz)
Natural freq (Mode 517) = 33200.03000 (Hz)
Natural freq (Mode 518) = 33318.92000 (Hz)
Natural freq (Mode 519) = 33330.25000 (Hz)
Natural freq (Mode 520) = 33333.78000 (Hz)
Natural freq (Mode 521) = 33486.56000 (Hz)
Natural freq (Mode 522) = 33531.17000 (Hz)
Natural freq (Mode 523) = 33683.28000 (Hz)
Natural freq (Mode 524) = 33797.57000 (Hz)
Natural freq (Mode 525) = 33906.94000 (Hz)
Natural freq (Mode 526) = 33914.80000 (Hz)
Natural freq (Mode 527) = 33989.41000 (Hz)
Natural freq (Mode 528) = 34210.63000 (Hz)
Natural freq (Mode 529) = 34378.73000 (Hz)
Natural freq (Mode 530) = 34494.40000 (Hz)
Natural freq (Mode 531) = 34582.28000 (Hz)
Natural freq (Mode 532) = 34836.82000 (Hz)
Natural freq (Mode 533) = 34902.17000 (Hz)
Natural freq (Mode 534) = 34987.61000 (Hz)
Natural freq (Mode 535) = 35067.79000 (Hz)
Natural freq (Mode 536) = 35153.96000 (Hz)
Natural freq (Mode 537) = 35173.18000 (Hz)
Natural freq (Mode 538) = 35315.79000 (Hz)
Natural freq (Mode 539) = 35452.04000 (Hz)
Natural freq (Mode 540) = 35564.39000 (Hz)
Natural freq (Mode 541) = 35577.60000 (Hz)
Natural freq (Mode 542) = 35671.63000 (Hz)
Natural freq (Mode 543) = 35764.36000 (Hz)
Natural freq (Mode 544) = 35817.39000 (Hz)
Natural freq (Mode 545) = 35987.39000 (Hz)
Natural freq (Mode 546) = 35988.65000 (Hz)
Natural freq (Mode 547) = 36149.87000 (Hz)
Natural freq (Mode 548) = 36216.11000 (Hz)
Natural freq (Mode 549) = 36374.59000 (Hz)
Natural freq (Mode 550) = 36456.40000 (Hz)
Natural freq (Mode 551) = 36643.81000 (Hz)
Natural freq (Mode 552) = 36841.90000 (Hz)
Natural freq (Mode 553) = 36898.49000 (Hz)
Natural freq (Mode 554) = 36940.48000 (Hz)
Natural freq (Mode 555) = 37109.42000 (Hz)
Natural freq (Mode 556) = 37109.45000 (Hz)
Natural freq (Mode 557) = 37157.88000 (Hz)
Natural freq (Mode 558) = 37177.07000 (Hz)
Natural freq (Mode 559) = 37287.62000 (Hz)
Natural freq (Mode 560) = 37387.53000 (Hz)
Natural freq (Mode 561) = 37522.76000 (Hz)
Natural freq (Mode 562) = 37628.77000 (Hz)
Natural freq (Mode 563) = 37734.15000 (Hz)
Natural freq (Mode 564) = 37824.32000 (Hz)
Natural freq (Mode 565) = 37936.66000 (Hz)
Natural freq (Mode 566) = 38054.42000 (Hz)
Natural freq (Mode 567) = 38287.95000 (Hz)
Natural freq (Mode 568) = 38432.25000 (Hz)
Natural freq (Mode 569) = 38489.84000 (Hz)
Natural freq (Mode 570) = 38652.49000 (Hz)
Natural freq (Mode 571) = 38702.59000 (Hz)
Natural freq (Mode 572) = 38877.29000 (Hz)
Natural freq (Mode 573) = 39004.32000 (Hz)
Natural freq (Mode 574) = 39191.21000 (Hz)
Natural freq (Mode 575) = 39286.07000 (Hz)
Natural freq (Mode 576) = 39329.37000 (Hz)
Natural freq (Mode 577) = 39574.73000 (Hz)
Natural freq (Mode 578) = 39720.89000 (Hz)
Natural freq (Mode 579) = 40162.23000 (Hz)
Natural freq (Mode 580) = 40253.22000 (Hz)
Natural freq (Mode 581) = 40293.79000 (Hz)
Natural freq (Mode 582) = 40337.32000 (Hz)
Natural freq (Mode 583) = 40474.10000 (Hz)
Natural freq (Mode 584) = 40602.31000 (Hz)
Natural freq (Mode 585) = 40635.95000 (Hz)
Natural freq (Mode 586) = 40660.85000 (Hz)
Natural freq (Mode 587) = 40743.75000 (Hz)
Natural freq (Mode 588) = 40756.84000 (Hz)
Natural freq (Mode 589) = 40949.57000 (Hz)
Natural freq (Mode 590) = 40995.24000 (Hz)
Natural freq (Mode 591) = 41223.55000 (Hz)
Natural freq (Mode 592) = 41359.39000 (Hz)
Natural freq (Mode 593) = 41528.88000 (Hz)
Natural freq (Mode 594) = 41791.72000 (Hz)
Natural freq (Mode 595) = 41887.48000 (Hz)
Natural freq (Mode 596) = 42118.45000 (Hz)
Natural freq (Mode 597) = 42198.64000 (Hz)
Natural freq (Mode 598) = 42348.55000 (Hz)
Natural freq (Mode 599) = 42370.13000 (Hz)
Natural freq (Mode 600) = 42416.97000 (Hz)
Natural freq (Mode 601) = 42462.20000 (Hz)
Natural freq (Mode 602) = 42642.21000 (Hz)
Natural freq (Mode 603) = 42726.17000 (Hz)
Natural freq (Mode 604) = 42854.97000 (Hz)
Natural freq (Mode 605) = 42962.25000 (Hz)
Natural freq (Mode 606) = 43123.13000 (Hz)
Natural freq (Mode 607) = 43203.68000 (Hz)
Natural freq (Mode 608) = 43400.77000 (Hz)
Natural freq (Mode 609) = 43508.95000 (Hz)
Natural freq (Mode 610) = 43597.38000 (Hz)
Natural freq (Mode 611) = 43700.77000 (Hz)
Natural freq (Mode 612) = 43704.76000 (Hz)
Natural freq (Mode 613) = 43877.68000 (Hz)
Natural freq (Mode 614) = 44012.25000 (Hz)
Natural freq (Mode 615) = 44106.74000 (Hz)
Natural freq (Mode 616) = 44292.90000 (Hz)
Natural freq (Mode 617) = 44314.06000 (Hz)
Natural freq (Mode 618) = 44374.05000 (Hz)
Natural freq (Mode 619) = 44397.46000 (Hz)
Natural freq (Mode 620) = 44586.68000 (Hz)
Natural freq (Mode 621) = 44696.46000 (Hz)
Natural freq (Mode 622) = 44741.60000 (Hz)
Natural freq (Mode 623) = 45054.47000 (Hz)
Natural freq (Mode 624) = 45140.14000 (Hz)
Natural freq (Mode 625) = 45249.72000 (Hz)
Natural freq (Mode 626) = 45385.59000 (Hz)
Natural freq (Mode 627) = 45567.35000 (Hz)
Natural freq (Mode 628) = 45605.37000 (Hz)
Natural freq (Mode 629) = 45735.81000 (Hz)
Natural freq (Mode 630) = 45752.43000 (Hz)
Natural freq (Mode 631) = 46051.15000 (Hz)
Natural freq (Mode 632) = 46420.19000 (Hz)
Natural freq (Mode 633) = 46488.60000 (Hz)
Natural freq (Mode 634) = 46552.35000 (Hz)
Natural freq (Mode 635) = 46577.11000 (Hz)
Natural freq (Mode 636) = 46578.90000 (Hz)
Natural freq (Mode 637) = 46694.76000 (Hz)
Natural freq (Mode 638) = 46912.64000 (Hz)
Natural freq (Mode 639) = 46981.14000 (Hz)
Natural freq (Mode 640) = 47193.58000 (Hz)
Natural freq (Mode 641) = 47238.25000 (Hz)
Natural freq (Mode 642) = 47338.20000 (Hz)
Natural freq (Mode 643) = 47429.59000 (Hz)
Natural freq (Mode 644) = 47576.44000 (Hz)
Natural freq (Mode 645) = 47611.71000 (Hz)
Natural freq (Mode 646) = 47691.93000 (Hz)
Natural freq (Mode 647) = 47807.08000 (Hz)
Natural freq (Mode 648) = 47890.22000 (Hz)
Natural freq (Mode 649) = 47917.94000 (Hz)
Natural freq (Mode 650) = 48003.06000 (Hz)
Natural freq (Mode 651) = 48405.16000 (Hz)
Natural freq (Mode 652) = 48501.56000 (Hz)
Natural freq (Mode 653) = 48589.31000 (Hz)
Natural freq (Mode 654) = 48598.45000 (Hz)
Natural freq (Mode 655) = 48779.29000 (Hz)
Natural freq (Mode 656) = 48883.09000 (Hz)
Natural freq (Mode 657) = 48930.20000 (Hz)
Natural freq (Mode 658) = 49088.71000 (Hz)
Natural freq (Mode 659) = 49207.57000 (Hz)
Natural freq (Mode 660) = 49256.51000 (Hz)
Natural freq (Mode 661) = 49376.35000 (Hz)
Natural freq (Mode 662) = 49480.93000 (Hz)
Natural freq (Mode 663) = 49565.85000 (Hz)
Natural freq (Mode 664) = 49718.37000 (Hz)
Natural freq (Mode 665) = 49722.37000 (Hz)
Natural freq (Mode 666) = 49790.09000 (Hz)
Natural freq (Mode 667) = 49897.80000 (Hz)
Natural freq (Mode 668) = 50054.08000 (Hz)
Natural freq (Mode 669) = 50090.88000 (Hz)
Natural freq (Mode 670) = 50160.08000 (Hz)
Natural freq (Mode 671) = 50228.52000 (Hz)
Natural freq (Mode 672) = 50465.21000 (Hz)
Natural freq (Mode 673) = 50484.11000 (Hz)
Natural freq (Mode 674) = 50692.21000 (Hz)
Natural freq (Mode 675) = 50853.68000 (Hz)
Natural freq (Mode 676) = 50857.21000 (Hz)
Natural freq (Mode 677) = 50936.92000 (Hz)
Natural freq (Mode 678) = 51135.05000 (Hz)
Natural freq (Mode 679) = 51171.95000 (Hz)
Natural freq (Mode 680) = 51382.60000 (Hz)
Natural freq (Mode 681) = 51500.84000 (Hz)
Natural freq (Mode 682) = 51551.45000 (Hz)
Natural freq (Mode 683) = 51604.40000 (Hz)
Natural freq (Mode 684) = 51794.87000 (Hz)
Natural freq (Mode 685) = 51921.50000 (Hz)
Natural freq (Mode 686) = 52077.61000 (Hz)
Natural freq (Mode 687) = 52106.14000 (Hz)
Natural freq (Mode 688) = 52156.48000 (Hz)
Natural freq (Mode 689) = 52196.38000 (Hz)
Natural freq (Mode 690) = 52375.95000 (Hz)
Natural freq (Mode 691) = 52511.88000 (Hz)
Natural freq (Mode 692) = 52690.02000 (Hz)
Natural freq (Mode 693) = 52760.29000 (Hz)
Natural freq (Mode 694) = 52983.51000 (Hz)
Natural freq (Mode 695) = 53151.14000 (Hz)
Natural freq (Mode 696) = 53168.78000 (Hz)
Natural freq (Mode 697) = 53351.66000 (Hz)
Natural freq (Mode 698) = 53457.94000 (Hz)
Natural freq (Mode 699) = 53501.50000 (Hz)
Natural freq (Mode 700) = 53568.66000 (Hz)
Natural freq (Mode 701) = 53771.08000 (Hz)
Natural freq (Mode 702) = 53815.28000 (Hz)
Natural freq (Mode 703) = 53819.51000 (Hz)
Natural freq (Mode 704) = 54018.69000 (Hz)
Natural freq (Mode 705) = 54206.11000 (Hz)
Natural freq (Mode 706) = 54242.44000 (Hz)
Natural freq (Mode 707) = 54451.73000 (Hz)
Natural freq (Mode 708) = 54504.73000 (Hz)
Natural freq (Mode 709) = 54515.07000 (Hz)
Natural freq (Mode 710) = 54603.34000 (Hz)
Natural freq (Mode 711) = 54798.02000 (Hz)
Natural freq (Mode 712) = 54826.34000 (Hz)
Natural freq (Mode 713) = 54976.60000 (Hz)
Natural freq (Mode 714) = 55099.90000 (Hz)
Natural freq (Mode 715) = 55233.76000 (Hz)
Natural freq (Mode 716) = 55312.55000 (Hz)
Natural freq (Mode 717) = 55359.35000 (Hz)
Natural freq (Mode 718) = 55622.14000 (Hz)
Natural freq (Mode 719) = 55794.26000 (Hz)
Natural freq (Mode 720) = 55892.18000 (Hz)
Natural freq (Mode 721) = 56015.41000 (Hz)
Natural freq (Mode 722) = 56088.41000 (Hz)
Natural freq (Mode 723) = 56115.56000 (Hz)
Natural freq (Mode 724) = 56334.32000 (Hz)
Natural freq (Mode 725) = 56351.92000 (Hz)
Natural freq (Mode 726) = 56609.43000 (Hz)
Natural freq (Mode 727) = 56690.62000 (Hz)
Natural freq (Mode 728) = 56781.62000 (Hz)
Natural freq (Mode 729) = 56865.87000 (Hz)
Natural freq (Mode 730) = 56948.31000 (Hz)
Natural freq (Mode 731) = 57119.90000 (Hz)
Natural freq (Mode 732) = 57228.48000 (Hz)
Natural freq (Mode 733) = 57330.72000 (Hz)
Natural freq (Mode 734) = 57473.44000 (Hz)
Natural freq (Mode 735) = 57547.01000 (Hz)
Natural freq (Mode 736) = 57627.58000 (Hz)
Natural freq (Mode 737) = 57732.92000 (Hz)
Natural freq (Mode 738) = 57822.45000 (Hz)
Natural freq (Mode 739) = 57992.67000 (Hz)
Natural freq (Mode 740) = 58178.70000 (Hz)
Natural freq (Mode 741) = 58235.37000 (Hz)
Natural freq (Mode 742) = 58342.95000 (Hz)
Natural freq (Mode 743) = 58393.04000 (Hz)
Natural freq (Mode 744) = 58548.01000 (Hz)
Natural freq (Mode 745) = 58743.37000 (Hz)
Natural freq (Mode 746) = 58747.77000 (Hz)
Natural freq (Mode 747) = 58763.92000 (Hz)
Natural freq (Mode 748) = 58967.43000 (Hz)
Natural freq (Mode 749) = 59096.52000 (Hz)
Natural freq (Mode 750) = 59102.65000 (Hz)
Natural freq (Mode 751) = 59219.30000 (Hz)
Natural freq (Mode 752) = 59386.15000 (Hz)
Natural freq (Mode 753) = 59562.50000 (Hz)
Natural freq (Mode 754) = 59631.56000 (Hz)
Natural freq (Mode 755) = 59639.75000 (Hz)
Natural freq (Mode 756) = 59712.64000 (Hz)
Natural freq (Mode 757) = 59838.64000 (Hz)
Natural freq (Mode 758) = 59903.59000 (Hz)
Natural freq (Mode 759) = 60006.47000 (Hz)
Natural freq (Mode 760) = 60127.36000 (Hz)
Natural freq (Mode 761) = 60224.49000 (Hz)
Natural freq (Mode 762) = 60294.48000 (Hz)
Natural freq (Mode 763) = 60324.69000 (Hz)
Natural freq (Mode 764) = 60396.43000 (Hz)
Natural freq (Mode 765) = 60515.33000 (Hz)
Natural freq (Mode 766) = 60559.32000 (Hz)
Natural freq (Mode 767) = 60678.05000 (Hz)
Natural freq (Mode 768) = 60828.19000 (Hz)
Natural freq (Mode 769) = 60907.92000 (Hz)
Natural freq (Mode 770) = 61254.36000 (Hz)
Natural freq (Mode 771) = 61307.17000 (Hz)
Natural freq (Mode 772) = 61381.37000 (Hz)
Natural freq (Mode 773) = 61481.29000 (Hz)
Natural freq (Mode 774) = 61562.68000 (Hz)
Natural freq (Mode 775) = 61716.24000 (Hz)
Natural freq (Mode 776) = 61781.28000 (Hz)
Natural freq (Mode 777) = 61795.57000 (Hz)
Natural freq (Mode 778) = 61994.89000 (Hz)
Natural freq (Mode 779) = 62094.15000 (Hz)
Natural freq (Mode 780) = 62113.02000 (Hz)
Natural freq (Mode 781) = 62222.04000 (Hz)
Natural freq (Mode 782) = 62288.52000 (Hz)
Natural freq (Mode 783) = 62385.94000 (Hz)
Natural freq (Mode 784) = 62396.24000 (Hz)
Natural freq (Mode 785) = 62527.74000 (Hz)
Natural freq (Mode 786) = 62579.81000 (Hz)
Natural freq (Mode 787) = 62721.25000 (Hz)
Natural freq (Mode 788) = 62738.94000 (Hz)
Natural freq (Mode 789) = 62865.63000 (Hz)
Natural freq (Mode 790) = 62948.16000 (Hz)
Natural freq (Mode 791) = 63042.76000 (Hz)
Natural freq (Mode 792) = 63143.53000 (Hz)
Natural freq (Mode 793) = 63170.49000 (Hz)
Natural freq (Mode 794) = 63233.18000 (Hz)
Natural freq (Mode 795) = 63391.41000 (Hz)
Natural freq (Mode 796) = 63540.32000 (Hz)
Natural freq (Mode 797) = 63602.34000 (Hz)
Natural freq (Mode 798) = 63750.55000 (Hz)
Natural freq (Mode 799) = 63885.63000 (Hz)
Natural freq (Mode 800) = 63965.49000 (Hz)
Natural freq (Mode 801) = 64042.26000 (Hz)
Natural freq (Mode 802) = 64146.40000 (Hz)
Natural freq (Mode 803) = 64163.32000 (Hz)
Natural freq (Mode 804) = 64321.53000 (Hz)
Natural freq (Mode 805) = 64416.47000 (Hz)
Natural freq (Mode 806) = 64596.16000 (Hz)
Natural freq (Mode 807) = 64668.98000 (Hz)
Natural freq (Mode 808) = 64816.43000 (Hz)
Natural freq (Mode 809) = 64962.29000 (Hz)
Natural freq (Mode 810) = 65109.30000 (Hz)
Natural freq (Mode 811) = 65160.50000 (Hz)
Natural freq (Mode 812) = 65187.46000 (Hz)
Natural freq (Mode 813) = 65332.37000 (Hz)
Natural freq (Mode 814) = 65388.61000 (Hz)
Natural freq (Mode 815) = 65410.63000 (Hz)
Natural freq (Mode 816) = 65475.19000 (Hz)
Natural freq (Mode 817) = 65597.51000 (Hz)
Natural freq (Mode 818) = 65661.34000 (Hz)
Natural freq (Mode 819) = 65720.16000 (Hz)
Natural freq (Mode 820) = 65867.98000 (Hz)
Natural freq (Mode 821) = 66059.62000 (Hz)
Natural freq (Mode 822) = 66131.58000 (Hz)
Natural freq (Mode 823) = 66322.35000 (Hz)
Natural freq (Mode 824) = 66464.03000 (Hz)
Natural freq (Mode 825) = 66530.87000 (Hz)
Natural freq (Mode 826) = 66564.12000 (Hz)
Natural freq (Mode 827) = 66605.34000 (Hz)
Natural freq (Mode 828) = 66789.47000 (Hz)
Natural freq (Mode 829) = 66945.90000 (Hz)
Natural freq (Mode 830) = 66998.07000 (Hz)
Natural freq (Mode 831) = 67080.26000 (Hz)
Natural freq (Mode 832) = 67189.01000 (Hz)
Natural freq (Mode 833) = 67243.66000 (Hz)
Natural freq (Mode 834) = 67296.74000 (Hz)
Natural freq (Mode 835) = 67376.41000 (Hz)
Natural freq (Mode 836) = 67513.82000 (Hz)
Natural freq (Mode 837) = 67567.81000 (Hz)
Natural freq (Mode 838) = 67666.32000 (Hz)
Natural freq (Mode 839) = 67841.24000 (Hz)
Natural freq (Mode 840) = 67908.45000 (Hz)
Natural freq (Mode 841) = 68016.58000 (Hz)
Natural freq (Mode 842) = 68079.98000 (Hz)
Natural freq (Mode 843) = 68176.81000 (Hz)
Natural freq (Mode 844) = 68460.19000 (Hz)
Natural freq (Mode 845) = 68554.47000 (Hz)
Natural freq (Mode 846) = 68590.22000 (Hz)
Natural freq (Mode 847) = 68651.88000 (Hz)
Natural freq (Mode 848) = 68687.21000 (Hz)
Natural freq (Mode 849) = 68786.12000 (Hz)
Natural freq (Mode 850) = 68856.07000 (Hz)
Natural freq (Mode 851) = 68911.45000 (Hz)
Natural freq (Mode 852) = 68921.30000 (Hz)
Natural freq (Mode 853) = 69021.59000 (Hz)
Natural freq (Mode 854) = 69065.40000 (Hz)
Natural freq (Mode 855) = 69205.85000 (Hz)
Natural freq (Mode 856) = 69252.89000 (Hz)
Natural freq (Mode 857) = 69340.47000 (Hz)
Natural freq (Mode 858) = 69375.84000 (Hz)
Natural freq (Mode 859) = 69440.12000 (Hz)
Natural freq (Mode 860) = 69512.06000 (Hz)
Natural freq (Mode 861) = 69654.96000 (Hz)
Natural freq (Mode 862) = 69777.94000 (Hz)
Natural freq (Mode 863) = 69802.79000 (Hz)
Natural freq (Mode 864) = 69841.16000 (Hz)
Natural freq (Mode 865) = 69862.84000 (Hz)
Natural freq (Mode 866) = 70097.50000 (Hz)
Natural freq (Mode 867) = 70162.36000 (Hz)
Natural freq (Mode 868) = 70263.24000 (Hz)
Natural freq (Mode 869) = 70382.94000 (Hz)
Natural freq (Mode 870) = 70458.26000 (Hz)
Natural freq (Mode 871) = 70518.42000 (Hz)
Natural freq (Mode 872) = 70586.77000 (Hz)
Natural freq (Mode 873) = 70696.01000 (Hz)
Natural freq (Mode 874) = 70815.79000 (Hz)
Natural freq (Mode 875) = 70909.97000 (Hz)
Natural freq (Mode 876) = 70983.21000 (Hz)
Natural freq (Mode 877) = 71056.86000 (Hz)
Natural freq (Mode 878) = 71154.90000 (Hz)
Natural freq (Mode 879) = 71186.77000 (Hz)
Natural freq (Mode 880) = 71297.27000 (Hz)
Natural freq (Mode 881) = 71311.62000 (Hz)
Natural freq (Mode 882) = 71367.08000 (Hz)
Natural freq (Mode 883) = 71546.12000 (Hz)
Natural freq (Mode 884) = 71616.69000 (Hz)
Natural freq (Mode 885) = 71716.84000 (Hz)
Natural freq (Mode 886) = 71918.26000 (Hz)
Natural freq (Mode 887) = 72018.71000 (Hz)
Natural freq (Mode 888) = 72140.89000 (Hz)
Natural freq (Mode 889) = 72189.70000 (Hz)
Natural freq (Mode 890) = 72303.92000 (Hz)
Natural freq (Mode 891) = 72392.19000 (Hz)
Natural freq (Mode 892) = 72479.59000 (Hz)
Natural freq (Mode 893) = 72685.64000 (Hz)
Natural freq (Mode 894) = 72758.08000 (Hz)
Natural freq (Mode 895) = 72772.19000 (Hz)
Natural freq (Mode 896) = 72899.19000 (Hz)
Natural freq (Mode 897) = 73060.15000 (Hz)
Natural freq (Mode 898) = 73133.38000 (Hz)
Natural freq (Mode 899) = 73302.51000 (Hz)
Natural freq (Mode 900) = 73340.19000 (Hz)
Natural freq (Mode 901) = 73393.19000 (Hz)
Natural freq (Mode 902) = 73522.47000 (Hz)
Natural freq (Mode 903) = 73626.04000 (Hz)
Natural freq (Mode 904) = 73721.49000 (Hz)
Natural freq (Mode 905) = 73739.77000 (Hz)
Natural freq (Mode 906) = 73766.51000 (Hz)
Natural freq (Mode 907) = 73944.32000 (Hz)
Natural freq (Mode 908) = 74006.82000 (Hz)
Natural freq (Mode 909) = 74121.25000 (Hz)
Natural freq (Mode 910) = 74153.07000 (Hz)
Natural freq (Mode 911) = 74175.30000 (Hz)
Natural freq (Mode 912) = 74249.00000 (Hz)
Natural freq (Mode 913) = 74364.63000 (Hz)
Natural freq (Mode 914) = 74494.14000 (Hz)
Natural freq (Mode 915) = 74538.38000 (Hz)
Natural freq (Mode 916) = 74634.16000 (Hz)
Natural freq (Mode 917) = 74679.94000 (Hz)
Natural freq (Mode 918) = 74739.85000 (Hz)
Natural freq (Mode 919) = 74803.58000 (Hz)
Natural freq (Mode 920) = 74993.28000 (Hz)
Natural freq (Mode 921) = 75053.98000 (Hz)
Natural freq (Mode 922) = 75093.93000 (Hz)
Natural freq (Mode 923) = 75299.71000 (Hz)
Natural freq (Mode 924) = 75358.80000 (Hz)
Natural freq (Mode 925) = 75425.58000 (Hz)
Natural freq (Mode 926) = 75536.12000 (Hz)
Natural freq (Mode 927) = 75713.14000 (Hz)
Natural freq (Mode 928) = 75834.39000 (Hz)
Natural freq (Mode 929) = 75884.56000 (Hz)
Natural freq (Mode 930) = 76007.14000 (Hz)
Natural freq (Mode 931) = 76120.42000 (Hz)
Natural freq (Mode 932) = 76225.74000 (Hz)
Natural freq (Mode 933) = 76255.57000 (Hz)
Natural freq (Mode 934) = 76430.79000 (Hz)
Natural freq (Mode 935) = 76638.92000 (Hz)
Natural freq (Mode 936) = 76687.01000 (Hz)
Natural freq (Mode 937) = 76810.80000 (Hz)
Natural freq (Mode 938) = 76828.09000 (Hz)
Natural freq (Mode 939) = 76925.01000 (Hz)
Natural freq (Mode 940) = 77008.94000 (Hz)
Natural freq (Mode 941) = 77102.92000 (Hz)
Natural freq (Mode 942) = 77151.28000 (Hz)
Natural freq (Mode 943) = 77289.38000 (Hz)
Natural freq (Mode 944) = 77372.04000 (Hz)
Natural freq (Mode 945) = 77376.51000 (Hz)
Natural freq (Mode 946) = 77440.76000 (Hz)
Natural freq (Mode 947) = 77523.43000 (Hz)
Natural freq (Mode 948) = 77561.89000 (Hz)
Natural freq (Mode 949) = 77587.38000 (Hz)
Natural freq (Mode 950) = 77748.95000 (Hz)
Natural freq (Mode 951) = 77853.38000 (Hz)
Natural freq (Mode 952) = 77858.82000 (Hz)
Natural freq (Mode 953) = 77953.25000 (Hz)
Natural freq (Mode 954) = 78000.41000 (Hz)
Natural freq (Mode 955) = 78099.35000 (Hz)
Natural freq (Mode 956) = 78253.68000 (Hz)
Natural freq (Mode 957) = 78382.22000 (Hz)
Natural freq (Mode 958) = 78418.48000 (Hz)
Natural freq (Mode 959) = 78515.48000 (Hz)
Natural freq (Mode 960) = 78610.92000 (Hz)
Natural freq (Mode 961) = 78645.10000 (Hz)
Natural freq (Mode 962) = 78727.57000 (Hz)
Natural freq (Mode 963) = 78863.91000 (Hz)
Natural freq (Mode 964) = 78937.32000 (Hz)
Natural freq (Mode 965) = 79053.58000 (Hz)
Natural freq (Mode 966) = 79077.26000 (Hz)
Natural freq (Mode 967) = 79215.24000 (Hz)
Natural freq (Mode 968) = 79294.12000 (Hz)
Natural freq (Mode 969) = 79324.82000 (Hz)
Natural freq (Mode 970) = 79362.91000 (Hz)
Natural freq (Mode 971) = 79527.23000 (Hz)
Natural freq (Mode 972) = 79611.69000 (Hz)
Natural freq (Mode 973) = 79647.10000 (Hz)
Natural freq (Mode 974) = 79832.89000 (Hz)
Natural freq (Mode 975) = 79866.64000 (Hz)
Natural freq (Mode 976) = 79970.43000 (Hz)
Natural freq (Mode 977) = 80030.32000 (Hz)
Natural freq (Mode 978) = 80104.74000 (Hz)
Natural freq (Mode 979) = 80123.64000 (Hz)
Natural freq (Mode 980) = 80182.67000 (Hz)
Natural freq (Mode 981) = 80321.53000 (Hz)
Natural freq (Mode 982) = 80385.61000 (Hz)
Natural freq (Mode 983) = 80444.38000 (Hz)
Natural freq (Mode 984) = 80581.53000 (Hz)
Natural freq (Mode 985) = 80665.28000 (Hz)
Natural freq (Mode 986) = 80757.29000 (Hz)
Natural freq (Mode 987) = 80846.96000 (Hz)
Natural freq (Mode 988) = 81004.13000 (Hz)
Natural freq (Mode 989) = 81044.79000 (Hz)
Natural freq (Mode 990) = 81140.53000 (Hz)
Natural freq (Mode 991) = 81244.66000 (Hz)
Natural freq (Mode 992) = 81434.94000 (Hz)
Natural freq (Mode 993) = 81460.92000 (Hz)
Natural freq (Mode 994) = 81502.50000 (Hz)
Natural freq (Mode 995) = 81572.23000 (Hz)
Natural freq (Mode 996) = 81703.12000 (Hz)
Natural freq (Mode 997) = 81809.87000 (Hz)
Natural freq (Mode 998) = 81917.77000 (Hz)
Natural freq (Mode 999) = 81922.97000 (Hz)
Natural freq (Mode 1000) = 82100.35000 (Hz)
Natural freq (Mode 1001) = 82120.03000 (Hz)
Natural freq (Mode 1002) = 82160.63000 (Hz)
Natural freq (Mode 1003) = 82272.67000 (Hz)
Natural freq (Mode 1004) = 82375.92000 (Hz)
Natural freq (Mode 1005) = 82426.08000 (Hz)
Natural freq (Mode 1006) = 82607.53000 (Hz)
Natural freq (Mode 1007) = 82667.54000 (Hz)
Natural freq (Mode 1008) = 82795.73000 (Hz)
Natural freq (Mode 1009) = 82830.25000 (Hz)
Natural freq (Mode 1010) = 82913.56000 (Hz)
Natural freq (Mode 1011) = 83117.39000 (Hz)
Natural freq (Mode 1012) = 83264.48000 (Hz)
Natural freq (Mode 1013) = 83303.87000 (Hz)
Natural freq (Mode 1014) = 83383.77000 (Hz)
Natural freq (Mode 1015) = 83474.57000 (Hz)
Natural freq (Mode 1016) = 83564.55000 (Hz)
Natural freq (Mode 1017) = 83612.36000 (Hz)
Natural freq (Mode 1018) = 83635.59000 (Hz)
Natural freq (Mode 1019) = 83660.44000 (Hz)
Natural freq (Mode 1020) = 83784.58000 (Hz)
Natural freq (Mode 1021) = 83861.33000 (Hz)
Natural freq (Mode 1022) = 83937.67000 (Hz)
Natural freq (Mode 1023) = 84023.90000 (Hz)
Natural freq (Mode 1024) = 84139.57000 (Hz)
Natural freq (Mode 1025) = 84188.86000 (Hz)
Natural freq (Mode 1026) = 84266.69000 (Hz)
Natural freq (Mode 1027) = 84269.75000 (Hz)
Natural freq (Mode 1028) = 84309.34000 (Hz)
Natural freq (Mode 1029) = 84427.03000 (Hz)
Natural freq (Mode 1030) = 84673.20000 (Hz)
Natural freq (Mode 1031) = 84725.60000 (Hz)
Natural freq (Mode 1032) = 84802.77000 (Hz)
Natural freq (Mode 1033) = 84921.77000 (Hz)
Natural freq (Mode 1034) = 84960.34000 (Hz)
Natural freq (Mode 1035) = 85091.32000 (Hz)
Natural freq (Mode 1036) = 85116.43000 (Hz)
Natural freq (Mode 1037) = 85264.96000 (Hz)
Natural freq (Mode 1038) = 85286.54000 (Hz)
Natural freq (Mode 1039) = 85306.32000 (Hz)
Natural freq (Mode 1040) = 85421.91000 (Hz)
Natural freq (Mode 1041) = 85547.09000 (Hz)
Natural freq (Mode 1042) = 85661.92000 (Hz)
Natural freq (Mode 1043) = 85719.86000 (Hz)
Natural freq (Mode 1044) = 85749.15000 (Hz)
Natural freq (Mode 1045) = 85924.99000 (Hz)
Natural freq (Mode 1046) = 86089.57000 (Hz)
Natural freq (Mode 1047) = 86148.53000 (Hz)
Natural freq (Mode 1048) = 86302.17000 (Hz)
Natural freq (Mode 1049) = 86373.30000 (Hz)
Natural freq (Mode 1050) = 86491.27000 (Hz)
Natural freq (Mode 1051) = 86624.46000 (Hz)
Natural freq (Mode 1052) = 86658.50000 (Hz)
Natural freq (Mode 1053) = 86688.69000 (Hz)
Natural freq (Mode 1054) = 86846.44000 (Hz)
Natural freq (Mode 1055) = 86952.64000 (Hz)
Natural freq (Mode 1056) = 87074.96000 (Hz)
Natural freq (Mode 1057) = 87237.35000 (Hz)
Natural freq (Mode 1058) = 87398.33000 (Hz)
Natural freq (Mode 1059) = 87464.73000 (Hz)
Natural freq (Mode 1060) = 87561.27000 (Hz)
Natural freq (Mode 1061) = 87628.88000 (Hz)
Natural freq (Mode 1062) = 87672.54000 (Hz)
Natural freq (Mode 1063) = 87868.90000 (Hz)
Natural freq (Mode 1064) = 87909.61000 (Hz)
Natural freq (Mode 1065) = 87948.39000 (Hz)
Natural freq (Mode 1066) = 88031.61000 (Hz)
Natural freq (Mode 1067) = 88056.46000 (Hz)
Natural freq (Mode 1068) = 88172.09000 (Hz)
Natural freq (Mode 1069) = 88206.87000 (Hz)
Natural freq (Mode 1070) = 88308.04000 (Hz)
Natural freq (Mode 1071) = 88352.02000 (Hz)
Natural freq (Mode 1072) = 88465.10000 (Hz)
Natural freq (Mode 1073) = 88565.23000 (Hz)
Natural freq (Mode 1074) = 88657.34000 (Hz)
Natural freq (Mode 1075) = 88700.26000 (Hz)
Natural freq (Mode 1076) = 88709.47000 (Hz)
Natural freq (Mode 1077) = 88724.85000 (Hz)
Natural freq (Mode 1078) = 88816.78000 (Hz)
Natural freq (Mode 1079) = 88873.34000 (Hz)
Natural freq (Mode 1080) = 89020.17000 (Hz)
Natural freq (Mode 1081) = 89078.82000 (Hz)
Natural freq (Mode 1082) = 89146.32000 (Hz)
Natural freq (Mode 1083) = 89216.51000 (Hz)
Natural freq (Mode 1084) = 89285.04000 (Hz)
Natural freq (Mode 1085) = 89306.96000 (Hz)
Natural freq (Mode 1086) = 89439.18000 (Hz)
Natural freq (Mode 1087) = 89528.18000 (Hz)
Natural freq (Mode 1088) = 89620.32000 (Hz)
Natural freq (Mode 1089) = 89716.06000 (Hz)
Natural freq (Mode 1090) = 89813.61000 (Hz)
Natural freq (Mode 1091) = 89915.21000 (Hz)
Natural freq (Mode 1092) = 89957.09000 (Hz)
Natural freq (Mode 1093) = 90076.36000 (Hz)
Natural freq (Mode 1094) = 90217.64000 (Hz)
Natural freq (Mode 1095) = 90281.78000 (Hz)
Natural freq (Mode 1096) = 90337.50000 (Hz)
Natural freq (Mode 1097) = 90383.03000 (Hz)
Natural freq (Mode 1098) = 90467.45000 (Hz)
Natural freq (Mode 1099) = 90504.77000 (Hz)
Natural freq (Mode 1100) = 90625.35000 (Hz)
Natural freq (Mode 1101) = 90713.12000 (Hz)
Natural freq (Mode 1102) = 90740.85000 (Hz)
Natural freq (Mode 1103) = 90752.30000 (Hz)
Natural freq (Mode 1104) = 90845.66000 (Hz)
Natural freq (Mode 1105) = 90901.66000 (Hz)
Natural freq (Mode 1106) = 91071.76000 (Hz)
Natural freq (Mode 1107) = 91110.43000 (Hz)
Natural freq (Mode 1108) = 91256.23000 (Hz)
Natural freq (Mode 1109) = 91418.58000 (Hz)
Natural freq (Mode 1110) = 91547.07000 (Hz)
Natural freq (Mode 1111) = 91607.19000 (Hz)
Natural freq (Mode 1112) = 91650.98000 (Hz)
Natural freq (Mode 1113) = 91713.15000 (Hz)
Natural freq (Mode 1114) = 91833.30000 (Hz)
Natural freq (Mode 1115) = 91977.28000 (Hz)
Natural freq (Mode 1116) = 92097.01000 (Hz)
Natural freq (Mode 1117) = 92197.90000 (Hz)
Natural freq (Mode 1118) = 92227.72000 (Hz)
Natural freq (Mode 1119) = 92254.49000 (Hz)
Natural freq (Mode 1120) = 92434.76000 (Hz)
Natural freq (Mode 1121) = 92530.93000 (Hz)
Natural freq (Mode 1122) = 92547.32000 (Hz)
Natural freq (Mode 1123) = 92617.38000 (Hz)
Natural freq (Mode 1124) = 92860.10000 (Hz)
Natural freq (Mode 1125) = 92989.60000 (Hz)
Natural freq (Mode 1126) = 93070.57000 (Hz)
Natural freq (Mode 1127) = 93135.01000 (Hz)
Natural freq (Mode 1128) = 93268.29000 (Hz)
Natural freq (Mode 1129) = 93358.34000 (Hz)
Natural freq (Mode 1130) = 93369.00000 (Hz)
Natural freq (Mode 1131) = 93384.06000 (Hz)
Natural freq (Mode 1132) = 93491.51000 (Hz)
Natural freq (Mode 1133) = 93537.09000 (Hz)
Natural freq (Mode 1134) = 93562.33000 (Hz)
Natural freq (Mode 1135) = 93754.73000 (Hz)
Natural freq (Mode 1136) = 93814.21000 (Hz)
Natural freq (Mode 1137) = 93871.80000 (Hz)
Natural freq (Mode 1138) = 93938.57000 (Hz)
Natural freq (Mode 1139) = 94024.20000 (Hz)
Natural freq (Mode 1140) = 94128.21000 (Hz)
Natural freq (Mode 1141) = 94232.26000 (Hz)
Natural freq (Mode 1142) = 94351.51000 (Hz)
Natural freq (Mode 1143) = 94409.17000 (Hz)
Natural freq (Mode 1144) = 94558.20000 (Hz)
Natural freq (Mode 1145) = 94631.15000 (Hz)
Natural freq (Mode 1146) = 94732.62000 (Hz)
Natural freq (Mode 1147) = 94826.06000 (Hz)
Natural freq (Mode 1148) = 94976.99000 (Hz)
Natural freq (Mode 1149) = 95048.56000 (Hz)
Natural freq (Mode 1150) = 95181.86000 (Hz)
Natural freq (Mode 1151) = 95192.30000 (Hz)
Natural freq (Mode 1152) = 95297.16000 (Hz)
Natural freq (Mode 1153) = 95436.33000 (Hz)
Natural freq (Mode 1154) = 95618.01000 (Hz)
Natural freq (Mode 1155) = 95702.23000 (Hz)
Natural freq (Mode 1156) = 95750.83000 (Hz)
Natural freq (Mode 1157) = 95867.23000 (Hz)
Natural freq (Mode 1158) = 95962.79000 (Hz)
Natural freq (Mode 1159) = 96041.91000 (Hz)
Natural freq (Mode 1160) = 96091.17000 (Hz)
Natural freq (Mode 1161) = 96284.30000 (Hz)
Natural freq (Mode 1162) = 96348.77000 (Hz)
Natural freq (Mode 1163) = 96411.30000 (Hz)
Natural freq (Mode 1164) = 96457.12000 (Hz)
Natural freq (Mode 1165) = 96570.81000 (Hz)
Natural freq (Mode 1166) = 96623.90000 (Hz)
Natural freq (Mode 1167) = 96696.38000 (Hz)
Natural freq (Mode 1168) = 96737.32000 (Hz)
Natural freq (Mode 1169) = 96846.65000 (Hz)
Natural freq (Mode 1170) = 97008.36000 (Hz)
Natural freq (Mode 1171) = 97119.42000 (Hz)
Natural freq (Mode 1172) = 97233.69000 (Hz)
Natural freq (Mode 1173) = 97270.07000 (Hz)
Natural freq (Mode 1174) = 97447.92000 (Hz)
Natural freq (Mode 1175) = 97506.07000 (Hz)
Natural freq (Mode 1176) = 97594.28000 (Hz)
Natural freq (Mode 1177) = 97805.04000 (Hz)
Natural freq (Mode 1178) = 97894.72000 (Hz)
Natural freq (Mode 1179) = 97928.87000 (Hz)
Natural freq (Mode 1180) = 97981.40000 (Hz)
Natural freq (Mode 1181) = 98086.96000 (Hz)
Natural freq (Mode 1182) = 98117.62000 (Hz)
Natural freq (Mode 1183) = 98245.71000 (Hz)
Natural freq (Mode 1184) = 98360.74000 (Hz)
Natural freq (Mode 1185) = 98519.72000 (Hz)
Natural freq (Mode 1186) = 98691.42000 (Hz)
Natural freq (Mode 1187) = 98754.68000 (Hz)
Natural freq (Mode 1188) = 98877.99000 (Hz)
Natural freq (Mode 1189) = 98986.09000 (Hz)
Natural freq (Mode 1190) = 99067.69000 (Hz)
Natural freq (Mode 1191) = 99222.21000 (Hz)
Natural freq (Mode 1192) = 99324.10000 (Hz)
Natural freq (Mode 1193) = 99363.49000 (Hz)
Natural freq (Mode 1194) = 99552.85000 (Hz)
Natural freq (Mode 1195) = 99565.86000 (Hz)
Natural freq (Mode 1196) = 99651.71000 (Hz)
Natural freq (Mode 1197) = 99914.16000 (Hz)
Natural freq (Mode 1198) = 99997.05000 (Hz)
Natural freq (Mode 1199) = 100086.10000 (Hz)
Natural freq (Mode 1200) = 100112.50000 (Hz)
Natural freq (Mode 1201) = 100320.50000 (Hz)
Natural freq (Mode 1202) = 100334.10000 (Hz)
Natural freq (Mode 1203) = 100410.10000 (Hz)
Natural freq (Mode 1204) = 100520.60000 (Hz)
Natural freq (Mode 1205) = 100611.10000 (Hz)
Natural freq (Mode 1206) = 100756.50000 (Hz)
Natural freq (Mode 1207) = 100857.90000 (Hz)
Natural freq (Mode 1208) = 100906.60000 (Hz)
Natural freq (Mode 1209) = 101024.70000 (Hz)
Natural freq (Mode 1210) = 101217.30000 (Hz)
Natural freq (Mode 1211) = 101378.20000 (Hz)
Natural freq (Mode 1212) = 101425.90000 (Hz)
Natural freq (Mode 1213) = 101568.40000 (Hz)
Natural freq (Mode 1214) = 101649.20000 (Hz)
Natural freq (Mode 1215) = 101854.50000 (Hz)
Natural freq (Mode 1216) = 101859.60000 (Hz)
Natural freq (Mode 1217) = 102032.30000 (Hz)
Natural freq (Mode 1218) = 102118.70000 (Hz)
Natural freq (Mode 1219) = 102163.20000 (Hz)
Natural freq (Mode 1220) = 102309.80000 (Hz)
Natural freq (Mode 1221) = 102376.90000 (Hz)
Natural freq (Mode 1222) = 102475.10000 (Hz)
Natural freq (Mode 1223) = 102587.10000 (Hz)
Natural freq (Mode 1224) = 102626.40000 (Hz)
Natural freq (Mode 1225) = 102808.10000 (Hz)
Natural freq (Mode 1226) = 102999.10000 (Hz)
Natural freq (Mode 1227) = 103055.40000 (Hz)
Natural freq (Mode 1228) = 103153.30000 (Hz)
Natural freq (Mode 1229) = 103210.50000 (Hz)
Natural freq (Mode 1230) = 103389.80000 (Hz)
Natural freq (Mode 1231) = 103567.90000 (Hz)
Natural freq (Mode 1232) = 103741.10000 (Hz)
Natural freq (Mode 1233) = 103800.40000 (Hz)
Natural freq (Mode 1234) = 103844.10000 (Hz)
Natural freq (Mode 1235) = 103957.40000 (Hz)
Natural freq (Mode 1236) = 104142.80000 (Hz)
Natural freq (Mode 1237) = 104186.80000 (Hz)
Natural freq (Mode 1238) = 104368.90000 (Hz)
Natural freq (Mode 1239) = 104521.90000 (Hz)
Natural freq (Mode 1240) = 104605.60000 (Hz)
Natural freq (Mode 1241) = 104640.40000 (Hz)
Natural freq (Mode 1242) = 104752.90000 (Hz)
Natural freq (Mode 1243) = 104877.60000 (Hz)
Natural freq (Mode 1244) = 104974.20000 (Hz)
Natural freq (Mode 1245) = 105069.10000 (Hz)
Natural freq (Mode 1246) = 105261.70000 (Hz)
Natural freq (Mode 1247) = 105316.40000 (Hz)
Natural freq (Mode 1248) = 105535.40000 (Hz)
Natural freq (Mode 1249) = 105616.20000 (Hz)
Natural freq (Mode 1250) = 105792.20000 (Hz)
Natural freq (Mode 1251) = 105817.40000 (Hz)
Natural freq (Mode 1252) = 105974.60000 (Hz)
Natural freq (Mode 1253) = 106104.30000 (Hz)
Natural freq (Mode 1254) = 106143.00000 (Hz)
Natural freq (Mode 1255) = 106291.00000 (Hz)
Natural freq (Mode 1256) = 106393.00000 (Hz)
Natural freq (Mode 1257) = 106517.20000 (Hz)
Natural freq (Mode 1258) = 106601.60000 (Hz)
Natural freq (Mode 1259) = 106776.20000 (Hz)
Natural freq (Mode 1260) = 106847.60000 (Hz)
Natural freq (Mode 1261) = 106928.10000 (Hz)
Natural freq (Mode 1262) = 107010.40000 (Hz)
Natural freq (Mode 1263) = 107146.40000 (Hz)
Natural freq (Mode 1264) = 107311.10000 (Hz)
Natural freq (Mode 1265) = 107361.80000 (Hz)
Natural freq (Mode 1266) = 107415.20000 (Hz)
Natural freq (Mode 1267) = 107609.10000 (Hz)
Natural freq (Mode 1268) = 107719.30000 (Hz)
Natural freq (Mode 1269) = 108001.00000 (Hz)
Natural freq (Mode 1270) = 108061.80000 (Hz)
Natural freq (Mode 1271) = 108076.50000 (Hz)
Natural freq (Mode 1272) = 108252.70000 (Hz)
Natural freq (Mode 1273) = 108325.20000 (Hz)
Natural freq (Mode 1274) = 108375.60000 (Hz)
Natural freq (Mode 1275) = 108506.50000 (Hz)
Natural freq (Mode 1276) = 108549.10000 (Hz)
Natural freq (Mode 1277) = 108709.70000 (Hz)
Natural freq (Mode 1278) = 108776.70000 (Hz)
Natural freq (Mode 1279) = 108840.10000 (Hz)
Natural freq (Mode 1280) = 109176.60000 (Hz)
Natural freq (Mode 1281) = 109253.60000 (Hz)
Natural freq (Mode 1282) = 109305.80000 (Hz)
Natural freq (Mode 1283) = 109383.00000 (Hz)
Natural freq (Mode 1284) = 109470.60000 (Hz)
Natural freq (Mode 1285) = 109580.90000 (Hz)
Natural freq (Mode 1286) = 109637.50000 (Hz)
Natural freq (Mode 1287) = 109903.10000 (Hz)
Natural freq (Mode 1288) = 109941.40000 (Hz)
Natural freq (Mode 1289) = 109970.10000 (Hz)
Natural freq (Mode 1290) = 110176.20000 (Hz)
Natural freq (Mode 1291) = 110262.20000 (Hz)
Natural freq (Mode 1292) = 110397.60000 (Hz)
Natural freq (Mode 1293) = 110469.50000 (Hz)
Natural freq (Mode 1294) = 110498.80000 (Hz)
Natural freq (Mode 1295) = 110660.80000 (Hz)
Natural freq (Mode 1296) = 110709.90000 (Hz)
Natural freq (Mode 1297) = 110855.40000 (Hz)
Natural freq (Mode 1298) = 111003.50000 (Hz)
Natural freq (Mode 1299) = 111108.40000 (Hz)
Natural freq (Mode 1300) = 111239.20000 (Hz)
Natural freq (Mode 1301) = 111263.50000 (Hz)
Natural freq (Mode 1302) = 111446.80000 (Hz)
Natural freq (Mode 1303) = 111644.50000 (Hz)
Natural freq (Mode 1304) = 111765.20000 (Hz)
Natural freq (Mode 1305) = 111843.10000 (Hz)
Natural freq (Mode 1306) = 111987.60000 (Hz)
Natural freq (Mode 1307) = 112035.40000 (Hz)
Natural freq (Mode 1308) = 112128.30000 (Hz)
Natural freq (Mode 1309) = 112392.30000 (Hz)
Natural freq (Mode 1310) = 112433.70000 (Hz)
Natural freq (Mode 1311) = 112461.80000 (Hz)
Natural freq (Mode 1312) = 112598.60000 (Hz)
Natural freq (Mode 1313) = 112674.70000 (Hz)
Natural freq (Mode 1314) = 112785.90000 (Hz)
Natural freq (Mode 1315) = 112877.40000 (Hz)
Natural freq (Mode 1316) = 112951.70000 (Hz)
Natural freq (Mode 1317) = 113078.10000 (Hz)
Natural freq (Mode 1318) = 113182.60000 (Hz)
Natural freq (Mode 1319) = 113251.80000 (Hz)
Natural freq (Mode 1320) = 113572.60000 (Hz)
Natural freq (Mode 1321) = 113614.80000 (Hz)
Natural freq (Mode 1322) = 113655.60000 (Hz)
Natural freq (Mode 1323) = 114032.30000 (Hz)
Natural freq (Mode 1324) = 114186.80000 (Hz)
Natural freq (Mode 1325) = 114294.00000 (Hz)
Natural freq (Mode 1326) = 114354.20000 (Hz)
Natural freq (Mode 1327) = 114521.20000 (Hz)
Natural freq (Mode 1328) = 114551.30000 (Hz)
Natural freq (Mode 1329) = 114600.10000 (Hz)
Natural freq (Mode 1330) = 114716.60000 (Hz)
Natural freq (Mode 1331) = 114808.50000 (Hz)
Natural freq (Mode 1332) = 114961.50000 (Hz)
Natural freq (Mode 1333) = 115052.60000 (Hz)
Natural freq (Mode 1334) = 115156.20000 (Hz)
Natural freq (Mode 1335) = 115377.20000 (Hz)
Natural freq (Mode 1336) = 115484.80000 (Hz)
Natural freq (Mode 1337) = 115597.90000 (Hz)
Natural freq (Mode 1338) = 115718.90000 (Hz)
Natural freq (Mode 1339) = 115960.20000 (Hz)
Natural freq (Mode 1340) = 116114.10000 (Hz)
Natural freq (Mode 1341) = 116243.00000 (Hz)
Natural freq (Mode 1342) = 116262.40000 (Hz)
Natural freq (Mode 1343) = 116413.40000 (Hz)
Natural freq (Mode 1344) = 116477.70000 (Hz)
Natural freq (Mode 1345) = 116555.20000 (Hz)
Natural freq (Mode 1346) = 116672.70000 (Hz)
Natural freq (Mode 1347) = 116713.00000 (Hz)
Natural freq (Mode 1348) = 116874.30000 (Hz)
Natural freq (Mode 1349) = 117031.80000 (Hz)
Natural freq (Mode 1350) = 117183.70000 (Hz)
Natural freq (Mode 1351) = 117264.80000 (Hz)
Natural freq (Mode 1352) = 117412.80000 (Hz)
Natural freq (Mode 1353) = 117527.50000 (Hz)
Natural freq (Mode 1354) = 117697.90000 (Hz)
Natural freq (Mode 1355) = 117771.70000 (Hz)
Natural freq (Mode 1356) = 117868.10000 (Hz)
Natural freq (Mode 1357) = 117969.50000 (Hz)
Natural freq (Mode 1358) = 118129.50000 (Hz)
Natural freq (Mode 1359) = 118302.40000 (Hz)
Natural freq (Mode 1360) = 118370.90000 (Hz)
Natural freq (Mode 1361) = 118419.00000 (Hz)
Natural freq (Mode 1362) = 118571.50000 (Hz)
Natural freq (Mode 1363) = 118877.20000 (Hz)
Natural freq (Mode 1364) = 118947.70000 (Hz)
Natural freq (Mode 1365) = 118997.70000 (Hz)
Natural freq (Mode 1366) = 119126.20000 (Hz)
Natural freq (Mode 1367) = 119270.50000 (Hz)
Natural freq (Mode 1368) = 119406.20000 (Hz)
Natural freq (Mode 1369) = 119511.30000 (Hz)
Natural freq (Mode 1370) = 119574.30000 (Hz)
Natural freq (Mode 1371) = 119781.00000 (Hz)
Natural freq (Mode 1372) = 119933.60000 (Hz)
Natural freq (Mode 1373) = 120145.60000 (Hz)
Natural freq (Mode 1374) = 120190.00000 (Hz)
Natural freq (Mode 1375) = 120321.80000 (Hz)
Natural freq (Mode 1376) = 120353.10000 (Hz)
Natural freq (Mode 1377) = 120597.80000 (Hz)
Natural freq (Mode 1378) = 120644.50000 (Hz)
Natural freq (Mode 1379) = 120725.60000 (Hz)
Natural freq (Mode 1380) = 120837.90000 (Hz)
Natural freq (Mode 1381) = 120870.10000 (Hz)
Natural freq (Mode 1382) = 121080.50000 (Hz)
Natural freq (Mode 1383) = 121177.30000 (Hz)
Natural freq (Mode 1384) = 121278.30000 (Hz)
Natural freq (Mode 1385) = 121504.70000 (Hz)
Natural freq (Mode 1386) = 121567.70000 (Hz)
Natural freq (Mode 1387) = 121628.50000 (Hz)
Natural freq (Mode 1388) = 121743.40000 (Hz)
Natural freq (Mode 1389) = 121787.00000 (Hz)
Natural freq (Mode 1390) = 122020.70000 (Hz)
Natural freq (Mode 1391) = 122085.30000 (Hz)
Natural freq (Mode 1392) = 122227.70000 (Hz)
Natural freq (Mode 1393) = 122430.00000 (Hz)
Natural freq (Mode 1394) = 122517.90000 (Hz)
Natural freq (Mode 1395) = 122566.40000 (Hz)
Natural freq (Mode 1396) = 122794.80000 (Hz)
Natural freq (Mode 1397) = 122905.20000 (Hz)
Natural freq (Mode 1398) = 123064.90000 (Hz)
Natural freq (Mode 1399) = 123171.70000 (Hz)
Natural freq (Mode 1400) = 123264.40000 (Hz)
Natural freq (Mode 1401) = 123359.30000 (Hz)
Natural freq (Mode 1402) = 123494.90000 (Hz)
Natural freq (Mode 1403) = 123758.80000 (Hz)
Natural freq (Mode 1404) = 123897.70000 (Hz)
Natural freq (Mode 1405) = 124106.20000 (Hz)
Natural freq (Mode 1406) = 124163.70000 (Hz)
Natural freq (Mode 1407) = 124297.60000 (Hz)
Natural freq (Mode 1408) = 124377.30000 (Hz)
Natural freq (Mode 1409) = 124544.60000 (Hz)
Natural freq (Mode 1410) = 124658.30000 (Hz)
Natural freq (Mode 1411) = 124674.60000 (Hz)
Natural freq (Mode 1412) = 124969.70000 (Hz)
Natural freq (Mode 1413) = 125010.20000 (Hz)
Natural freq (Mode 1414) = 125106.50000 (Hz)
Natural freq (Mode 1415) = 125287.30000 (Hz)
Natural freq (Mode 1416) = 125364.30000 (Hz)
Natural freq (Mode 1417) = 125496.00000 (Hz)
Natural freq (Mode 1418) = 125668.20000 (Hz)
Natural freq (Mode 1419) = 125806.90000 (Hz)
Natural freq (Mode 1420) = 125859.20000 (Hz)
Natural freq (Mode 1421) = 126124.10000 (Hz)
Natural freq (Mode 1422) = 126336.10000 (Hz)
Natural freq (Mode 1423) = 126512.70000 (Hz)
Natural freq (Mode 1424) = 126539.10000 (Hz)
Natural freq (Mode 1425) = 126620.50000 (Hz)
Natural freq (Mode 1426) = 126877.60000 (Hz)
Natural freq (Mode 1427) = 126962.30000 (Hz)
Natural freq (Mode 1428) = 127132.20000 (Hz)
Natural freq (Mode 1429) = 127254.70000 (Hz)
Natural freq (Mode 1430) = 127477.10000 (Hz)
Natural freq (Mode 1431) = 127659.30000 (Hz)
Natural freq (Mode 1432) = 127893.90000 (Hz)
Natural freq (Mode 1433) = 127957.60000 (Hz)
Natural freq (Mode 1434) = 128099.20000 (Hz)
Natural freq (Mode 1435) = 128180.30000 (Hz)
Natural freq (Mode 1436) = 128320.40000 (Hz)
Natural freq (Mode 1437) = 128363.50000 (Hz)
Natural freq (Mode 1438) = 128546.60000 (Hz)
Natural freq (Mode 1439) = 128764.90000 (Hz)
Natural freq (Mode 1440) = 128804.00000 (Hz)
Natural freq (Mode 1441) = 128925.30000 (Hz)
Natural freq (Mode 1442) = 128959.00000 (Hz)
Natural freq (Mode 1443) = 128969.90000 (Hz)
Natural freq (Mode 1444) = 129220.00000 (Hz)
Natural freq (Mode 1445) = 129323.20000 (Hz)
Natural freq (Mode 1446) = 129474.70000 (Hz)
Natural freq (Mode 1447) = 129675.90000 (Hz)
Natural freq (Mode 1448) = 129703.10000 (Hz)
Natural freq (Mode 1449) = 130113.10000 (Hz)
Natural freq (Mode 1450) = 130185.80000 (Hz)
Natural freq (Mode 1451) = 130348.10000 (Hz)
Natural freq (Mode 1452) = 130578.30000 (Hz)
Natural freq (Mode 1453) = 130708.50000 (Hz)
Natural freq (Mode 1454) = 130869.20000 (Hz)
Natural freq (Mode 1455) = 130922.50000 (Hz)
Natural freq (Mode 1456) = 131020.90000 (Hz)
Natural freq (Mode 1457) = 131122.90000 (Hz)
Natural freq (Mode 1458) = 131424.50000 (Hz)
Natural freq (Mode 1459) = 131584.80000 (Hz)
Natural freq (Mode 1460) = 131684.30000 (Hz)
Natural freq (Mode 1461) = 131809.90000 (Hz)
Natural freq (Mode 1462) = 131858.60000 (Hz)
Natural freq (Mode 1463) = 131958.50000 (Hz)
Natural freq (Mode 1464) = 132233.70000 (Hz)
Natural freq (Mode 1465) = 132449.40000 (Hz)
Natural freq (Mode 1466) = 132607.40000 (Hz)
Natural freq (Mode 1467) = 132729.70000 (Hz)
Natural freq (Mode 1468) = 132880.40000 (Hz)
Natural freq (Mode 1469) = 133046.80000 (Hz)
Natural freq (Mode 1470) = 133201.30000 (Hz)
Natural freq (Mode 1471) = 133234.10000 (Hz)
Natural freq (Mode 1472) = 133629.50000 (Hz)
Natural freq (Mode 1473) = 133796.90000 (Hz)
Natural freq (Mode 1474) = 133948.40000 (Hz)
Natural freq (Mode 1475) = 134006.30000 (Hz)
Natural freq (Mode 1476) = 134324.40000 (Hz)
Natural freq (Mode 1477) = 134507.70000 (Hz)
Natural freq (Mode 1478) = 134620.10000 (Hz)
Natural freq (Mode 1479) = 134837.70000 (Hz)
Natural freq (Mode 1480) = 134916.50000 (Hz)
Natural freq (Mode 1481) = 135097.00000 (Hz)
Natural freq (Mode 1482) = 135137.40000 (Hz)
Natural freq (Mode 1483) = 135476.30000 (Hz)
Natural freq (Mode 1484) = 135553.40000 (Hz)
Natural freq (Mode 1485) = 135680.90000 (Hz)
Natural freq (Mode 1486) = 135723.70000 (Hz)
Natural freq (Mode 1487) = 136137.20000 (Hz)
Natural freq (Mode 1488) = 136254.00000 (Hz)
Natural freq (Mode 1489) = 136531.70000 (Hz)
Natural freq (Mode 1490) = 136629.60000 (Hz)
Natural freq (Mode 1491) = 136739.30000 (Hz)
Natural freq (Mode 1492) = 136927.00000 (Hz)
Natural freq (Mode 1493) = 136989.70000 (Hz)
Natural freq (Mode 1494) = 137183.70000 (Hz)
Natural freq (Mode 1495) = 137230.00000 (Hz)
Natural freq (Mode 1496) = 137313.30000 (Hz)
Natural freq (Mode 1497) = 137520.90000 (Hz)
Natural freq (Mode 1498) = 137639.00000 (Hz)
Natural freq (Mode 1499) = 138090.60000 (Hz)
Natural freq (Mode 1500) = 138387.40000 (Hz)
Natural freq (Mode 1501) = 138465.10000 (Hz)
Natural freq (Mode 1502) = 138815.80000 (Hz)
Natural freq (Mode 1503) = 138915.10000 (Hz)
Natural freq (Mode 1504) = 138942.60000 (Hz)
Natural freq (Mode 1505) = 139174.70000 (Hz)
Natural freq (Mode 1506) = 139199.90000 (Hz)
Natural freq (Mode 1507) = 139357.90000 (Hz)
Natural freq (Mode 1508) = 139425.70000 (Hz)
Natural freq (Mode 1509) = 139577.30000 (Hz)
Natural freq (Mode 1510) = 139690.00000 (Hz)
Natural freq (Mode 1511) = 139888.50000 (Hz)
Natural freq (Mode 1512) = 140098.70000 (Hz)
Natural freq (Mode 1513) = 140249.80000 (Hz)
Natural freq (Mode 1514) = 140367.30000 (Hz)
Natural freq (Mode 1515) = 140657.00000 (Hz)
Natural freq (Mode 1516) = 140786.00000 (Hz)
Natural freq (Mode 1517) = 141026.50000 (Hz)
Natural freq (Mode 1518) = 141186.20000 (Hz)
Natural freq (Mode 1519) = 141405.70000 (Hz)
Natural freq (Mode 1520) = 141619.60000 (Hz)
Natural freq (Mode 1521) = 141793.30000 (Hz)
Natural freq (Mode 1522) = 142003.20000 (Hz)
Natural freq (Mode 1523) = 142060.70000 (Hz)
Natural freq (Mode 1524) = 142212.40000 (Hz)
Natural freq (Mode 1525) = 142235.00000 (Hz)
Natural freq (Mode 1526) = 142422.80000 (Hz)
Natural freq (Mode 1527) = 142663.20000 (Hz)
Natural freq (Mode 1528) = 143052.20000 (Hz)
Natural freq (Mode 1529) = 143084.90000 (Hz)
Natural freq (Mode 1530) = 143132.30000 (Hz)
Natural freq (Mode 1531) = 143274.40000 (Hz)
Natural freq (Mode 1532) = 143396.20000 (Hz)
Natural freq (Mode 1533) = 143756.70000 (Hz)
Natural freq (Mode 1534) = 143943.30000 (Hz)
Natural freq (Mode 1535) = 144127.80000 (Hz)
Natural freq (Mode 1536) = 144235.40000 (Hz)
Natural freq (Mode 1537) = 144542.10000 (Hz)
Natural freq (Mode 1538) = 144662.30000 (Hz)
Natural freq (Mode 1539) = 144690.70000 (Hz)
Natural freq (Mode 1540) = 144771.30000 (Hz)
Natural freq (Mode 1541) = 145039.90000 (Hz)
Natural freq (Mode 1542) = 145151.10000 (Hz)
Natural freq (Mode 1543) = 145284.10000 (Hz)
Natural freq (Mode 1544) = 145642.50000 (Hz)
Natural freq (Mode 1545) = 146249.40000 (Hz)
Natural freq (Mode 1546) = 146402.00000 (Hz)
Natural freq (Mode 1547) = 146685.30000 (Hz)
Natural freq (Mode 1548) = 146725.90000 (Hz)
Natural freq (Mode 1549) = 146784.20000 (Hz)
Natural freq (Mode 1550) = 146916.60000 (Hz)
Natural freq (Mode 1551) = 147213.30000 (Hz)
Natural freq (Mode 1552) = 147379.50000 (Hz)
Natural freq (Mode 1553) = 147702.80000 (Hz)
Natural freq (Mode 1554) = 148135.00000 (Hz)
Natural freq (Mode 1555) = 148211.80000 (Hz)
Natural freq (Mode 1556) = 148385.40000 (Hz)
Natural freq (Mode 1557) = 148579.80000 (Hz)
Natural freq (Mode 1558) = 148840.20000 (Hz)
Natural freq (Mode 1559) = 148989.20000 (Hz)
Natural freq (Mode 1560) = 149117.70000 (Hz)
Natural freq (Mode 1561) = 149384.50000 (Hz)
Natural freq (Mode 1562) = 149901.10000 (Hz)
Natural freq (Mode 1563) = 150012.00000 (Hz)
Natural freq (Mode 1564) = 150026.60000 (Hz)
Natural freq (Mode 1565) = 150123.80000 (Hz)
Natural freq (Mode 1566) = 150212.80000 (Hz)
Natural freq (Mode 1567) = 150535.40000 (Hz)
Natural freq (Mode 1568) = 150791.90000 (Hz)
Natural freq (Mode 1569) = 151291.00000 (Hz)
Natural freq (Mode 1570) = 151469.60000 (Hz)
Natural freq (Mode 1571) = 151604.60000 (Hz)
Natural freq (Mode 1572) = 151672.40000 (Hz)
Natural freq (Mode 1573) = 151822.30000 (Hz)
Natural freq (Mode 1574) = 152226.20000 (Hz)
Natural freq (Mode 1575) = 152338.60000 (Hz)
Natural freq (Mode 1576) = 152687.80000 (Hz)
Natural freq (Mode 1577) = 152820.80000 (Hz)
Natural freq (Mode 1578) = 153515.50000 (Hz)
Natural freq (Mode 1579) = 153649.70000 (Hz)
Natural freq (Mode 1580) = 153716.80000 (Hz)
Natural freq (Mode 1581) = 154080.40000 (Hz)
Natural freq (Mode 1582) = 154227.00000 (Hz)
Natural freq (Mode 1583) = 154281.30000 (Hz)
Natural freq (Mode 1584) = 154350.30000 (Hz)
Natural freq (Mode 1585) = 154510.10000 (Hz)
Natural freq (Mode 1586) = 154829.60000 (Hz)
Natural freq (Mode 1587) = 155355.80000 (Hz)
Natural freq (Mode 1588) = 155436.70000 (Hz)
Natural freq (Mode 1589) = 155641.50000 (Hz)
Natural freq (Mode 1590) = 155881.40000 (Hz)
Natural freq (Mode 1591) = 155898.70000 (Hz)
Natural freq (Mode 1592) = 156045.80000 (Hz)
Natural freq (Mode 1593) = 156632.20000 (Hz)
Natural freq (Mode 1594) = 156715.70000 (Hz)
Natural freq (Mode 1595) = 156944.30000 (Hz)
Natural freq (Mode 1596) = 156959.70000 (Hz)
Natural freq (Mode 1597) = 157074.30000 (Hz)
Natural freq (Mode 1598) = 157281.40000 (Hz)
Natural freq (Mode 1599) = 157509.00000 (Hz)
Natural freq (Mode 1600) = 157672.90000 (Hz)
Natural freq (Mode 1601) = 157765.50000 (Hz)
Natural freq (Mode 1602) = 157847.60000 (Hz)
Natural freq (Mode 1603) = 157987.50000 (Hz)
Natural freq (Mode 1604) = 158062.80000 (Hz)
Natural freq (Mode 1605) = 158390.60000 (Hz)
Natural freq (Mode 1606) = 158600.10000 (Hz)
Natural freq (Mode 1607) = 158957.10000 (Hz)
Natural freq (Mode 1608) = 159008.80000 (Hz)
Natural freq (Mode 1609) = 159347.70000 (Hz)
Natural freq (Mode 1610) = 159448.00000 (Hz)
Natural freq (Mode 1611) = 160017.90000 (Hz)
Natural freq (Mode 1612) = 160125.80000 (Hz)
Natural freq (Mode 1613) = 160197.70000 (Hz)
Natural freq (Mode 1614) = 160403.10000 (Hz)
Natural freq (Mode 1615) = 160624.50000 (Hz)
Natural freq (Mode 1616) = 160755.70000 (Hz)
Natural freq (Mode 1617) = 160803.50000 (Hz)
Natural freq (Mode 1618) = 160976.60000 (Hz)
Natural freq (Mode 1619) = 161448.10000 (Hz)
Natural freq (Mode 1620) = 161586.90000 (Hz)
Natural freq (Mode 1621) = 161815.20000 (Hz)
Natural freq (Mode 1622) = 161986.90000 (Hz)
Natural freq (Mode 1623) = 162466.80000 (Hz)
Natural freq (Mode 1624) = 162566.50000 (Hz)
Natural freq (Mode 1625) = 162608.40000 (Hz)
Natural freq (Mode 1626) = 162717.60000 (Hz)
Natural freq (Mode 1627) = 162844.00000 (Hz)
Natural freq (Mode 1628) = 163278.60000 (Hz)
Natural freq (Mode 1629) = 163309.40000 (Hz)
Natural freq (Mode 1630) = 163964.70000 (Hz)
Natural freq (Mode 1631) = 164005.10000 (Hz)
Natural freq (Mode 1632) = 164261.60000 (Hz)
Natural freq (Mode 1633) = 164326.10000 (Hz)
Natural freq (Mode 1634) = 164590.90000 (Hz)
Natural freq (Mode 1635) = 164656.90000 (Hz)
Natural freq (Mode 1636) = 165096.90000 (Hz)
Natural freq (Mode 1637) = 165297.50000 (Hz)
Natural freq (Mode 1638) = 165804.30000 (Hz)
Natural freq (Mode 1639) = 166068.20000 (Hz)
Natural freq (Mode 1640) = 166457.30000 (Hz)
Natural freq (Mode 1641) = 166514.40000 (Hz)
Natural freq (Mode 1642) = 166618.00000 (Hz)
Natural freq (Mode 1643) = 167181.10000 (Hz)
Natural freq (Mode 1644) = 167769.30000 (Hz)
Natural freq (Mode 1645) = 167803.40000 (Hz)
Natural freq (Mode 1646) = 167887.70000 (Hz)
Natural freq (Mode 1647) = 167937.00000 (Hz)
Natural freq (Mode 1648) = 168171.80000 (Hz)
Natural freq (Mode 1649) = 168637.70000 (Hz)
Natural freq (Mode 1650) = 168827.00000 (Hz)
Natural freq (Mode 1651) = 168918.90000 (Hz)
Natural freq (Mode 1652) = 169013.80000 (Hz)
Natural freq (Mode 1653) = 169143.70000 (Hz)
Natural freq (Mode 1654) = 169595.50000 (Hz)
Natural freq (Mode 1655) = 169874.10000 (Hz)
Natural freq (Mode 1656) = 169886.40000 (Hz)
Natural freq (Mode 1657) = 169891.20000 (Hz)
Natural freq (Mode 1658) = 169934.80000 (Hz)
Natural freq (Mode 1659) = 170188.10000 (Hz)
Natural freq (Mode 1660) = 170651.40000 (Hz)
Natural freq (Mode 1661) = 170659.80000 (Hz)
Natural freq (Mode 1662) = 171236.50000 (Hz)
Natural freq (Mode 1663) = 171387.80000 (Hz)
Natural freq (Mode 1664) = 171667.50000 (Hz)
Natural freq (Mode 1665) = 171785.20000 (Hz)
Natural freq (Mode 1666) = 172104.00000 (Hz)
Natural freq (Mode 1667) = 172379.30000 (Hz)
Natural freq (Mode 1668) = 172531.20000 (Hz)
Natural freq (Mode 1669) = 173061.80000 (Hz)
Natural freq (Mode 1670) = 173218.80000 (Hz)
Natural freq (Mode 1671) = 173992.60000 (Hz)
Natural freq (Mode 1672) = 174199.60000 (Hz)
Natural freq (Mode 1673) = 174311.20000 (Hz)
Natural freq (Mode 1674) = 174609.30000 (Hz)
Natural freq (Mode 1675) = 174851.40000 (Hz)
Natural freq (Mode 1676) = 175088.40000 (Hz)
Natural freq (Mode 1677) = 175104.80000 (Hz)
Natural freq (Mode 1678) = 175240.60000 (Hz)
Natural freq (Mode 1679) = 175725.80000 (Hz)
Natural freq (Mode 1680) = 175958.00000 (Hz)
Natural freq (Mode 1681) = 176785.50000 (Hz)
Natural freq (Mode 1682) = 176887.90000 (Hz)
Natural freq (Mode 1683) = 176960.70000 (Hz)
Natural freq (Mode 1684) = 177004.30000 (Hz)
Natural freq (Mode 1685) = 177410.10000 (Hz)
Natural freq (Mode 1686) = 177613.00000 (Hz)
Natural freq (Mode 1687) = 177999.40000 (Hz)
Natural freq (Mode 1688) = 178203.10000 (Hz)
Natural freq (Mode 1689) = 178443.20000 (Hz)
Natural freq (Mode 1690) = 179265.20000 (Hz)
Natural freq (Mode 1691) = 179577.40000 (Hz)
Natural freq (Mode 1692) = 179735.20000 (Hz)
Natural freq (Mode 1693) = 179903.20000 (Hz)
Natural freq (Mode 1694) = 180130.10000 (Hz)
Natural freq (Mode 1695) = 180359.50000 (Hz)
Natural freq (Mode 1696) = 180434.90000 (Hz)
Natural freq (Mode 1697) = 181385.00000 (Hz)
Natural freq (Mode 1698) = 181992.60000 (Hz)
Natural freq (Mode 1699) = 182050.10000 (Hz)
Natural freq (Mode 1700) = 182062.40000 (Hz)
Natural freq (Mode 1701) = 183019.60000 (Hz)
Natural freq (Mode 1702) = 183208.80000 (Hz)
Natural freq (Mode 1703) = 183609.70000 (Hz)
Natural freq (Mode 1704) = 184158.80000 (Hz)
Natural freq (Mode 1705) = 184251.30000 (Hz)
Natural freq (Mode 1706) = 184789.50000 (Hz)
Natural freq (Mode 1707) = 184832.80000 (Hz)
Natural freq (Mode 1708) = 185132.10000 (Hz)
Natural freq (Mode 1709) = 185327.30000 (Hz)
Natural freq (Mode 1710) = 185472.20000 (Hz)
Natural freq (Mode 1711) = 185901.70000 (Hz)
Natural freq (Mode 1712) = 186622.70000 (Hz)
Natural freq (Mode 1713) = 187198.40000 (Hz)
Natural freq (Mode 1714) = 187443.40000 (Hz)
Natural freq (Mode 1715) = 187507.80000 (Hz)
Natural freq (Mode 1716) = 187872.30000 (Hz)
Natural freq (Mode 1717) = 188187.00000 (Hz)
Natural freq (Mode 1718) = 188741.90000 (Hz)
Natural freq (Mode 1719) = 188959.60000 (Hz)
Natural freq (Mode 1720) = 189275.20000 (Hz)
Natural freq (Mode 1721) = 190410.90000 (Hz)
Natural freq (Mode 1722) = 190828.60000 (Hz)
Natural freq (Mode 1723) = 191294.90000 (Hz)
Natural freq (Mode 1724) = 191352.10000 (Hz)
Natural freq (Mode 1725) = 191490.70000 (Hz)
Natural freq (Mode 1726) = 191801.40000 (Hz)
Natural freq (Mode 1727) = 192067.80000 (Hz)
Natural freq (Mode 1728) = 192128.50000 (Hz)
Natural freq (Mode 1729) = 192910.30000 (Hz)
Natural freq (Mode 1730) = 193493.10000 (Hz)
Natural freq (Mode 1731) = 193667.50000 (Hz)
Natural freq (Mode 1732) = 193707.10000 (Hz)
Natural freq (Mode 1733) = 194562.50000 (Hz)
Natural freq (Mode 1734) = 194671.90000 (Hz)
Natural freq (Mode 1735) = 194895.90000 (Hz)
Natural freq (Mode 1736) = 195986.20000 (Hz)
Natural freq (Mode 1737) = 196046.40000 (Hz)
Natural freq (Mode 1738) = 196164.80000 (Hz)
Natural freq (Mode 1739) = 196916.80000 (Hz)
Natural freq (Mode 1740) = 196945.90000 (Hz)
Natural freq (Mode 1741) = 196963.30000 (Hz)
Natural freq (Mode 1742) = 198742.00000 (Hz)
Natural freq (Mode 1743) = 198832.90000 (Hz)
Natural freq (Mode 1744) = 199305.40000 (Hz)
Natural freq (Mode 1745) = 200294.70000 (Hz)
Natural freq (Mode 1746) = 200419.80000 (Hz)
Natural freq (Mode 1747) = 201244.20000 (Hz)
Natural freq (Mode 1748) = 201284.70000 (Hz)
Natural freq (Mode 1749) = 201362.20000 (Hz)
Natural freq (Mode 1750) = 201875.70000 (Hz)
Natural freq (Mode 1751) = 202090.90000 (Hz)
Natural freq (Mode 1752) = 202691.80000 (Hz)
Natural freq (Mode 1753) = 203016.30000 (Hz)
Natural freq (Mode 1754) = 204512.00000 (Hz)
Natural freq (Mode 1755) = 205046.80000 (Hz)
Natural freq (Mode 1756) = 205539.70000 (Hz)
Natural freq (Mode 1757) = 206255.10000 (Hz)
Natural freq (Mode 1758) = 209931.40000 (Hz)
Natural freq (Mode 1759) = 210310.70000 (Hz)
Natural freq (Mode 1760) = 211454.20000 (Hz)
Natural freq (Mode 1761) = 211898.10000 (Hz)
Natural freq (Mode 1762) = 212483.80000 (Hz)
Natural freq (Mode 1763) = 213805.00000 (Hz)
Natural freq (Mode 1764) = 215284.00000 (Hz)
Natural freq (Mode 1765) = 216529.80000 (Hz)
Natural freq (Mode 1766) = 217898.60000 (Hz)
Natural freq (Mode 1767) = 219200.70000 (Hz)
Natural freq (Mode 1768) = 220852.30000 (Hz)
Natural freq (Mode 1769) = 222877.80000 (Hz)
Natural freq (Mode 1770) = 223804.40000 (Hz)
Natural freq (Mode 1771) = 230522.70000 (Hz)
Natural freq (Mode 1772) = 231395.10000 (Hz)
Natural freq (Mode 1773) = 234055.50000 (Hz)
Natural freq (Mode 1774) = 237433.60000 (Hz)
Natural freq (Mode 1775) = 240144.30000 (Hz)
Natural freq (Mode 1776) = 240535.30000 (Hz)
Natural freq (Mode 1777) = 243767.00000 (Hz)
Natural freq (Mode 1778) = 253575.70000 (Hz)
Natural freq (Mode 1779) = 267124.30000 (Hz)

real	0m1.989s
user	0m1.239s
sys	0m0.415s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_CompositeWingFreq_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_Composite_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_Composite_PyTest.py test;
+ python -u nastran_Composite_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 49
Number of elements = 36
Number of triangle elements      = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes    = 49
Total number of elements = 36
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = plate, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - plate
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plateTip, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 49
	Number of elements = 36
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 36
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - cantilever
	No "constraintType" specified for Constraint tuple cantilever, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Warning: No loads specified for case EigenAnalysis!!!!
	Writing mass increment cards
	Writing analysis cards, 0
	Writing combined constraint cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing coordinate system cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m0.977s
user	0m0.671s
sys	0m0.401s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_Composite_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_Flutter_15degree.py test;
+ python -u nastran_Flutter_15degree.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 133
Number of elements = 108
Number of triangle elements      = 0
Number of quadrilateral elements = 108
Body 2 (of 2)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 134
Total number of elements = 108
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Root_Point, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = WingSurface, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
	Name = Wing, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
	Name = Wing, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 133
	Number of elements = 108
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 108
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 134
	Combined Number of elements = 109
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 108
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 133
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - aluminum
	No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Body
	Property name - Edge
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - PointConstraint
	No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Root
	No "groupName" specified for Connection tuple Root!
	Looking for automatic connections from the use of capsConnectLink for Root
	7 automatic connections were made for capsConnect Root (node id 134)
	Done getting FEA connections
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Flutter
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No loads specified for case Flutter!!!!
	Writing mass increment cards
	Writing aero card
	Writing analysis cards, 0
	Writing constraint ADD cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing aeroelastic cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m0.983s
user	0m0.726s
sys	0m0.375s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_Flutter_15degree.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_MultiLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_MultiLoadCase_PyTest.py test;
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u nastran_MultiLoadCase_PyTest.py -outLevel=0 -noAnalysis
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 49
Number of elements = 36
Number of triangle elements      = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes    = 49
Total number of elements = 36
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 49
	Number of elements = 36
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 36
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 5
	Load name - load_0
	Load name - load_1
	Load name - load_2
	Load name - load_3
	Load name - load_4
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 5
	Analysis name - load_0
	Analysis name - load_1
	Analysis name - load_2
	Analysis name - load_3
	Analysis name - load_4
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_2, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_3, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_4, assuming all constraints are applied!!!!
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing combined constraint cards
	Writing load ADD cards
	Writing combined constraint cards
	Writing load ADD cards
	Writing combined constraint cards
	Writing load ADD cards
	Writing combined constraint cards
	Writing load ADD cards
	Writing combined constraint cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m1.019s
user	0m0.706s
sys	0m0.411s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_MultiLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_OptimizationMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_OptimizationMultiLoad_PyTest.py test;
+ python -u nastran_OptimizationMultiLoad_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 49
Number of elements = 36
Number of triangle elements      = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes    = 49
Total number of elements = 36
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 49
	Number of elements = 36
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 36
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 2
	Load name - load_0
	Load name - load_1
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - materialDV
	Design_Variable name - propertyDV
	Design_Variable_Relation name - materialDVR
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - propertyDVR
	Number of design variable relations - 2
	Done getting FEA design variables

Getting FEA design constraints.......
	Number of design constraints - 2
	Design_Constraint name - stress1
	Design_Constraint name - stress2
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 2
	Analysis name - load_0
	Analysis name - load_1
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing combined constraint cards
	Writing design constraint ADD cards
	Writing load ADD cards
	Writing combined constraint cards
	Writing design constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
	Writing design constraints and responses cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running NASTRAN!

real	0m1.015s
user	0m0.696s
sys	0m0.405s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_OptimizationMultiLoad_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_PlateMisc_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_PlateMisc_PyTest.py test;
+ python -u nastran_PlateMisc_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 49
Number of elements = 36
Number of triangle elements      = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes    = 49
Total number of elements = 36
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 49
	Number of elements = 36
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 36
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 3
	Load name - moment
	Load name - pressure
	Load name - thermal
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - pltvar
	Number of design variable relations - 0
	Done getting FEA design variables

Getting FEA design constraints.......
	Number of design constraints - 1
	Design_Constraint name - pltcon
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing constraint ADD cards
	Writing design constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design constraints and responses cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m0.989s
user	0m0.682s
sys	0m0.395s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_PlateMisc_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_PyTest.py test;
+ python -u nastran_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 2091
Number of elements = 1845
Number of triangle elements      = 0
Number of quadrilateral elements = 1845
----------------------------
Total number of nodes    = 2091
Total number of elements = 1845
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2091
	Number of elements = 1845
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 1845
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - Ribs_and_Spars
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - ribConstraint
	No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Warning: No loads specified for case EigenAnalysis!!!!
	Writing mass increment cards
	Writing analysis cards, 0
	Writing combined constraint cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

Getting results for natural frequencies.....
Reading Nastran FO6 file - extracting Eigen-Values!
	Number of Eigen-Values = 10
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
	Loading Eigen-Value = 4
	Loading Eigen-Value = 5
	Loading Eigen-Value = 6
	Loading Eigen-Value = 7
	Loading Eigen-Value = 8
	Loading Eigen-Value = 9
	Loading Eigen-Value = 10
Natural freq (Mode 1) = 0.02165 (Hz)
Natural freq (Mode 2) = 0.02165 (Hz)
Natural freq (Mode 3) = 0.10665 (Hz)
Natural freq (Mode 4) = 0.10665 (Hz)
Natural freq (Mode 5) = 0.13547 (Hz)
Natural freq (Mode 6) = 0.13547 (Hz)
Natural freq (Mode 7) = 0.23092 (Hz)
Natural freq (Mode 8) = 0.23092 (Hz)
Natural freq (Mode 9) = 0.27609 (Hz)
Natural freq (Mode 10) = 0.27609 (Hz)

real	0m6.246s
user	0m11.677s
sys	0m8.053s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_SingleLoadCase_PyTest.py test;
+ python -u nastran_SingleLoadCase_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of triangle elements      = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes    = 25
Total number of elements = 16
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m1.008s
user	0m0.684s
sys	0m0.403s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_SingleLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_ThreeBarDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_ThreeBarDesign_PyTest.py test;
+ python -u nastran_ThreeBarDesign_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 4
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4
Total number of elements = 0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedForce
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 3
	Design_Variable name - Bar1A
	Design_Variable name - Bar2A
	Design_Variable name - Bar3A
	Design_Variable_Relation name - Bar1A
	Design_Variable_Relation name - Bar2A
	Design_Variable_Relation name - Bar3A
	Number of design variable relations - 3
	Done getting FEA design variables

Getting FEA design constraints.......
	Number of design constraints - 3
	Design_Constraint name - stress1
	Design_Constraint name - stress2
	Design_Constraint name - stress3
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - SingleLoadCase
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing constraint ADD cards
	Writing design constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
	Writing design constraints and responses cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m1.010s
user	0m0.689s
sys	0m0.404s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBarDesign_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_ThreeBarFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_ThreeBarFreq_PyTest.py test;
+ python -u nastran_ThreeBarFreq_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 4
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4
Total number of elements = 0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Warning: No loads specified for case EigenAnalysis!!!!
	Writing mass increment cards
	Writing analysis cards, 0
	Writing combined constraint cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m1.007s
user	0m0.698s
sys	0m0.408s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBarFreq_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_ThreeBarLinkDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_ThreeBarLinkDesign_PyTest.py test;
+ python -u nastran_ThreeBarLinkDesign_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 4
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4
Total number of elements = 0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedForce
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 3
	Design_Variable name - Bar1A
	Design_Variable name - Bar2A
	Design_Variable name - Bar3A
	Design_Variable_Relation name - Bar1A
	Design_Variable_Relation name - Bar2A
	Design_Variable_Relation name - Bar3A
	Number of design variable relations - 3
	Done getting FEA design variables

Getting FEA design constraints.......
	Number of design constraints - 3
	Design_Constraint name - stress1
	Design_Constraint name - stress2
	Design_Constraint name - stress3
Done getting FEA design constraints
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - SingleLoadCase
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing constraint ADD cards
	Writing design constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
	Writing design constraints and responses cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m1.027s
user	0m0.698s
sys	0m0.404s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBarLinkDesign_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_ThreeBarMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_ThreeBarMultiLoad_PyTest.py test;
+ python -u nastran_ThreeBarMultiLoad_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 4
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4
Total number of elements = 0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 2
	Constraint name - conOne
	No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement"
	Constraint name - conTwo
	No "constraintType" specified for Constraint tuple conTwo, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 2
	Load name - loadOne
	Load name - loadTwo
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 2
	Analysis name - caseOne
	Analysis name - caseTwo
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m1.019s
user	0m0.695s
sys	0m0.407s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBarMultiLoad_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_ThreeBar_PyTest.py test;
+ python -u nastran_ThreeBar_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 4
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4
Total number of elements = 0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedForce
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - SingleLoadCase
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Writing mass increment cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m1.029s
user	0m0.698s
sys	0m0.410s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_ThreeBar_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'nastran_Trim_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nastran_Trim_15degree.py test;
+ python -u nastran_Trim_15degree.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 117
Number of elements = 96
Number of triangle elements      = 0
Number of quadrilateral elements = 96
Body 2 (of 2)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 118
Total number of elements = 96
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Root_Point, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = WingSurface, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
	Name = Wing, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Edge, index = 1
	Name = Body, index = 2
	Name = Root, index = 3
	Name = Wing, index = 4
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 117
	Number of elements = 96
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 96
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 118
	Combined Number of elements = 97
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 96
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 117
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - aluminum
	No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 3
	Property name - Body
	Property name - Edge
	Property name - Root
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - PointConstraint
	No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA supports.......
	Number of supports - 1
	Support name - PointSupport
	Done getting FEA supports

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Root
	No "groupName" specified for Connection tuple Root!
	Looking for automatic connections from the use of capsConnectLink for Root
	9 automatic connections were made for capsConnect Root (node id 118)
	Done getting FEA connections

Getting FEA loads.......
	Number of loads - 2
	Load name - GravityLoad
	No "groupName" specified for Load tuple GravityLoad, going to use load name
	Load name - PointLoad
	Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Mass_Increment tuple is NULL - No mass increments applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Trim
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in free field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
	Writing mass increment set

Writing Nastran instruction file....
	Warning: No loads specified for case Trim, assuming all loads are applied!!!!
	Writing mass increment cards
	Writing aeros card
	Writing aestat cards
	Writing analysis cards, 0
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing support cards
	Writing material cards
	Writing property cards
	Writing aeroelastic cards
	Done writing aeroelastic cards
	Done writing files


Running Nastran......
Done running Nastran!

real	0m1.023s
user	0m0.713s
sys	0m0.387s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case nastran_Trim_15degree.py passed (as expected)
=================================================

Running.... AEROELASTIC PyTests


=================================================
+ echo 'aeroelasticSimple_Pressure_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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/ESP125/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          =     0.149   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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  1.9292e+00|   -1.298444|    0.998175|    0.628773|    4.170662|   -1.025477|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.9586e+00|   -1.701949|    0.831442|    0.450794|    3.754061|   -0.652898|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.9432e+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|         &lt; -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	0m22.167s
user	0m18.754s
sys	0m2.289s
+ 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/ESP125/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/ESP125/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          =     0.144   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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- 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 19.606095 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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  1.6235e+00|   -0.620749|    1.814328|    1.306826|    4.848357|    0.056579|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.6418e+00|   -1.097282|    1.519547|    1.164533|    4.374272|    0.038462|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.6266e+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|         &lt; -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	0m47.628s
user	0m40.069s
sys	0m4.388s
+ 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/ESP125/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/ESP125/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          =     0.072   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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  2.6799e-01|   -0.752613|    1.603074|    1.223267|    4.716493|   -1.311926|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.7795e-01|   -1.082205|    1.490442|    1.104154|    4.374404|   -1.114824|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.7861e-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|         &lt; -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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- 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 1.013410 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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  3.0964e-01|    1.850145|    4.803488|    4.927158|    7.319250|   -0.010446|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  3.0979e-01|    2.131732|    4.741224|    4.926819|    7.571356|   -0.035666|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  3.1353e-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|         &lt; -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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- 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 2.770529 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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  2.7248e-01|    4.427863|    7.391414|    7.171071|    9.896969|   -0.048645|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.9912e-01|    4.500985|    7.273408|    7.111650|    9.918170|   -0.069453|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.9455e-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|         &lt; -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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- 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 35.455804 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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  3.1470e-01|    7.060281|   10.027137|    9.994175|   12.529387|   -0.052400|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  3.2638e-01|    7.556625|   10.163626|   10.009975|   12.932925|   -0.051576|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  3.3781e-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|         &lt; -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	0m57.226s
user	0m52.980s
sys	0m4.247s
+ 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/ESP125/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/ESP125/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          =     0.072   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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  3.0393e-01|   -0.752613|    1.603074|    1.223267|    4.716493|   -1.311926|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  3.0437e-01|   -1.082205|    1.490442|    1.104154|    4.374404|   -1.114824|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  3.1101e-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|         &lt; -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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- 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 1.119666 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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  3.4274e-01|    2.878121|    5.830029|    6.291368|    8.347227|    0.331982|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  3.5735e-01|    3.320027|    5.828884|    6.170839|    8.765605|   -0.263310|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  3.6159e-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|         &lt; -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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- 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 32.857833 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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  3.1082e-01|    4.070526|    7.024857|    7.285496|    9.539632|    0.080019|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  3.2301e-01|    4.500756|    7.017601|    7.167392|    9.890627|    0.101047|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  3.1458e-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|         &lt; -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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

----------------- 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 32.194350 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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  3.1580e-01|    7.447666|   10.414518|   10.335403|   12.916772|    0.024748|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  3.2848e-01|    7.872151|   10.374304|   10.394736|   13.266411|    0.025398|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  3.3212e-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|         &lt; -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	1m50.205s
user	1m55.647s
sys	0m10.547s
+ 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/ESP125/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/ESP125/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          =     0.136   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: <a href='https://su2code.github.io'>https://su2code.github.io</a>                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (<a href='http://su2foundation.org'>http://su2foundation.org</a>)                                            |
-------------------------------------------------------------------------
| 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 &lt;<a href='http://www.gnu.org/licenses/'>http://www.gnu.org/licenses/</a>&gt;.   |
-------------------------------------------------------------------------

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 &amp; 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 <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see <a href='https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations'>https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations</a>
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  1.6890e+00|   -1.298444|    0.998175|    0.628773|    4.170662|   -1.025477|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.6921e+00|   -1.701949|    0.831442|    0.450794|    3.754061|   -0.652898|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.6726e+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|         &lt; -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	0m17.561s
user	0m16.523s
sys	0m1.858s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
gp.py test;
+ python -u gp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m11.488s
user	0m1.574s
sys	0m0.339s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
qp.py test;
+ python -u qp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m1.766s
user	0m1.730s
sys	0m0.201s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
sp.py test;
+ python -u sp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m1.607s
user	0m1.613s
sys	0m0.210s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
boydBox.py test;
+ python -u boydBox.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m1.444s
user	0m1.434s
sys	0m0.195s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hoburg_gp.py test;
+ python -u hoburg_gp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m11.399s
user	0m11.288s
sys	0m0.329s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hoburg_blackbox.py test;
+ python -u hoburg_blackbox.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m43.631s
user	0m43.369s
sys	0m0.376s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/sizeWing.py test;
+ python -u pyCAPS/sizeWing.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nrock 2

Objective
---------
   0.075 dimensionless

Variables
---------
   AR     :  10.000        [-]         Wing aspect ratio
   CD     :   0.075        [-]         Drag Coefficient 
   CL     :   0.999        [-]         Lift Coefficient 
   S      :   2.642     meter ** 2     Wing area        
   V      :   2.722   meter / second   Airspeed         
   W      :  11.979       newton       Aircraft weight  
   Wwing  :   1.598       newton       Wing weight      

Constants
---------
   ARmax     :  10                [-]            Max AR                                         
   CD0       :   0.040            [-]            Profile drag                                   
   CLmax     :   1                [-]            Max CL                                         
   E0        :  10               joule           Maximum elastic potential energy in rubber band
   Wfixed    :   0.100           newton          Weight of fixed components                     
   Wrock     :   2               newton          Weight of each rock                            
   e         :   0.900            [-]            Oswawld efficiency factor                      
   g         :   9.810    meter / second ** 2    Gravitational constant                         
   nrock     :   2                [-]            Number of rocks to carry                       
   rho       :   1.225   kilogram / meter ** 3   Density of air                                 
   rho_wing  :   1       kilogram / meter ** 3   Weight density of wing                         
   tau       :   0.120            [-]            Airfoil thickness as t/c                       

Sensitivities
-------------
   Sensitivities not computed

Solve Report
------------
   Solve Method           :  Geometric Program 
   Classification         :  Convex 
   Solver                 :  cvxopt 

Optimized L/D: 13.267784561972134
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!

real	0m2.078s
user	0m1.975s
sys	0m0.257s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/sizeWing.py passed (as expected)
=================================================

avl: /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/bin/avl

=================================================
+ echo 'pyCAPS/optTaperAvl.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/optTaperAvl.py test;
+ python -u pyCAPS/optTaperAvl.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m8.001s
user	0m5.103s
sys	0m2.775s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/optWingAvl.py test;
+ python -u pyCAPS/optWingAvl.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nrock 2
Starting iteration 0 at 0.3522 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: [&lt;Quantity(0.06083473495512859, 'dimensionless')&gt;, &lt;Quantity(-0.0014769756676574763, 'dimensionless')&gt;]
Calling cvxopt.solvers.cp at 1.6937 seconds
Got sol from cvxopt at 1.7141 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: [&lt;Quantity(0.06359341837318677, 'dimensionless')&gt;, &lt;Quantity(-0.0014812479871501028, 'dimensionless')&gt;]
logspace stuff at 3.0783 seconds
Starting iteration 1 at 3.1217 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 3.1314 seconds
Got sol from cvxopt at 3.1455 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: [&lt;Quantity(0.06135879009172007, 'dimensionless')&gt;, &lt;Quantity(-0.0014697917150108264, 'dimensionless')&gt;]
logspace stuff at 4.5600 seconds
Starting iteration 2 at 4.6044 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 4.6136 seconds
Got sol from cvxopt at 4.6293 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: [&lt;Quantity(0.0507308561720321, 'dimensionless')&gt;, &lt;Quantity(-0.0014191909882388387, 'dimensionless')&gt;]
logspace stuff at 6.0147 seconds
Starting iteration 3 at 6.0638 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 6.0758 seconds
Got sol from cvxopt at 6.0929 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: [&lt;Quantity(0.009583432731846697, 'dimensionless')&gt;, &lt;Quantity(-0.0013533445524949173, 'dimensionless')&gt;]
logspace stuff at 7.5029 seconds
Starting iteration 4 at 7.5505 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 7.5601 seconds
Got sol from cvxopt at 7.5728 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: [&lt;Quantity(-0.0008541793291738653, 'dimensionless')&gt;, &lt;Quantity(-0.0013850816280497336, 'dimensionless')&gt;]
logspace stuff at 9.0073 seconds
Starting iteration 5 at 9.0562 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 9.0660 seconds
Got sol from cvxopt at 9.0813 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: [&lt;Quantity(-6.436455185498957e-06, 'dimensionless')&gt;, &lt;Quantity(-0.0013814190269140214, 'dimensionless')&gt;]
logspace stuff at 10.5525 seconds
Starting iteration 6 at 10.6026 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 10.6148 seconds
Got sol from cvxopt at 10.6306 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: [&lt;Quantity(-5.709554107280468e-07, 'dimensionless')&gt;, &lt;Quantity(-0.0013813957757918827, 'dimensionless')&gt;]
logspace stuff at 12.0394 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	0m14.127s
user	0m9.104s
sys	0m4.897s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/GPSize.py test;
+ python -u pyCAPS/GPSize.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	0m11.887s
user	0m11.543s
sys	0m0.518s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/GPSize.py passed (as expected)
=================================================

mses: /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/bin/mses

=================================================
+ echo 'pyCAPS/MSES.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/MSES.py test;
+ python -u pyCAPS/MSES.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	4m54.255s
user	4m36.614s
sys	0m10.457s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/Camber.py test;
+ python -u pyCAPS/Camber.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	15m6.790s
user	13m46.135s
sys	0m32.493s
+ 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/ESP125/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/CMConstraint.py test;
+ python -u pyCAPS/CMConstraint.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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	4m50.052s
user	4m13.416s
sys	0m9.568s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/CMConstraint.py passed (as expected)
=================================================

Traceback (most recent call last):
  File "&lt;string&gt;", line 1, in &lt;module&gt;
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/ESP125/EngSketchPad/data/Plugs -name 'plugs0*.csm'
+ sort -f
+ awk '{ n=split($0, a, ";"); for(i=1; i&lt;=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 May 24 19:50 ASTRO.D01
-rw-r--r--  1 jenkins  staff   277K May 24 19:50 ASTRO.IDX
-rwxr-xr-x  1 jenkins  staff   129K May 24 19:51 ESPxddm
-rwxr-xr-x  1 jenkins  staff   210K May 24 19:51 Slugs
-rwxr-xr-x  1 jenkins  staff    85K May 24 19:51 TestFit
-rwxr-xr-x  1 jenkins  staff   1.8M May 24 19:50 avl
-rwxr-xr-x  1 jenkins  staff    34K May 24 19:51 cart3dTest
-rwxr-xr-x  1 jenkins  staff    34K May 28 16:21 egads2cart
-rwxr-xr-x  1 jenkins  staff    70K May 24 19:51 egads2cgt
-rwxr-xr-x  1 jenkins  staff   416K May 24 19:50 friction
-rwxr-xr-x  1 jenkins  staff   8.9M May 24 19:50 mastros.exe
-rwxr-xr-x  1 jenkins  staff   2.2M May 24 19:50 mses
-rwxr-xr-x  1 jenkins  staff   2.5M May 24 19:50 mset
-rwxr-xr-x  1 jenkins  staff    34K May 24 19:51 phaseUtil
-rw-r--r--  1 jenkins  staff   1.6K May 31 15:02 pod.egads
-rw-r--r--  1 jenkins  staff     0B May 31 15:02 port7681.jrnl
-rwxr-xr-x  1 jenkins  staff   1.2M May 24 19:50 pplot
-rwxr-xr-x  1 jenkins  staff   1.2M May 24 19:50 pxplot
-rwxr-xr-x  1 jenkins  staff    68K May 30 12:20 sensCSM
-rwxr-xr-x  1 jenkins  staff   206K May 30 12:20 serveCSM
-rwxr-xr-x  1 jenkins  staff   174K May 30 12:20 serveESP
-rwxr-xr-x  1 jenkins  staff    51K May 24 19:51 vCurvature
-rwxr-xr-x  1 jenkins  staff    35K May 24 19:51 vGeom
-rwxr-xr-x  1 jenkins  staff    52K May 24 19:51 vTess
-rwxr-xr-x  1 jenkins  staff   1.9M May 24 19:51 vTesstatic
-rw-r--r--  1 jenkins  staff   195K May 31 15:02 wingMultiModel.bdf
-rwxr-xr-x  1 jenkins  staff   1.8M May 24 19:50 xfoil
( 1 / 4 )
data/Plugs/plugs0a.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/Plugs/plugs0a.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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


==&gt; Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/Plugs/buildFinal.jrnl"


==&gt; Closing input journal file

==&gt; serveCSM completed successfully with no verification data

real	0m10.163s
user	0m9.737s
sys	0m0.585s
++ set +x
data/Plugs/plugs0a                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 2 / 4 )
data/Plugs/plugs0b.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/Plugs/plugs0b.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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


==&gt; Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/Plugs/buildFinal.jrnl"


==&gt; Closing input journal file

==&gt; serveCSM completed successfully with no verification data

real	0m10.361s
user	0m11.930s
sys	0m0.111s
++ set +x
data/Plugs/plugs0b                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 3 / 4 )
data/Plugs/plugs0c.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/Plugs/plugs0c.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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


==&gt; Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/Plugs/buildFinal.jrnl"


==&gt; Closing input journal file

==&gt; serveCSM completed successfully with no verification data

real	0m27.017s
user	0m36.675s
sys	0m0.259s
++ set +x
data/Plugs/plugs0c                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 4 / 4 )
data/Plugs/plugs0d.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/Plugs/plugs0d.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/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


==&gt; Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESP125/EngSketchPad/data/Plugs/buildFinal.jrnl"


==&gt; Closing input journal file

==&gt; serveCSM completed successfully with no verification data

real	0m29.846s
user	0m37.416s
sys	0m0.246s
++ 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)] -&gt; 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] -&gt; found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Clang] -&gt; found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -&gt; 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] -&gt; 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] -&gt; 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] -&gt; found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -&gt; found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -&gt; 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=125,buildnode=macys #74'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS