Started by upstream project "ESP_bPreBuilt" build number 67
originally caused by:
 Started by user galbramc
Running as galbramc
[EnvInject] - Loading node environment variables.
Building remotely on viggen 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 '2024-03-06T20:30:32.471 -0500' --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 2473

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 '2024-03-06T20:30:32.471 -0500' --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 850

No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
No changes for svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP since the previous build
[GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [viggen] is in [[macys, macys_VM, master, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-rhel7, reynolds-ubuntu16, reynolds-ubuntu18, reynolds-ubuntu20]]
Run condition [Execution node ] preventing perform for step [Execute shell]
[Execution node] check if [viggen] is in [[viggen]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[ESP_bPreBuilt] $ /bin/bash -ex /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T/jenkins2225048135025984670.sh
+ arch -arch arm64 /bin/bash -ex /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/ESP_PreBuilt.sh
+ source /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.6
++ OCCTREF=7.6
++ AFLR_VERSION=11.5.9
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.34.0
++ export PYTHON_VERSION=3.11.6
++ PYTHON_VERSION=3.11.6
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ viggen == \r\e\y\n\o\l\d\s ]]
++ [[ '' == *\.\i\f\o\r\t ]]
++ '[' -f /opt/intel/oneapi/setvars.sh ']'
++ source /opt/intel/oneapi/setvars.sh
++ '[' -f /Users/jenkins/.bashrc ']'
++ export CAPS_OUTLEVEL=0
++ CAPS_OUTLEVEL=0
++ [[ '' == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ ESP_BLOC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//julia
++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.6 != '' ]]
++ [[ '' != '' ]]
++ [[ viggen == *\r\e\y\n\o\l\d\s* ]]
++ [[ viggen == *\m\a\c\y\s* ]]
++ [[ viggen == *\v\i\g\g\e\n* ]]
++ export EMPnumProc=2
++ EMPnumProc=2
++ export OMP_NUM_THREADS=2
++ OMP_NUM_THREADS=2
++ source /Users/jenkins/.bash_profile
++++ /opt/homebrew/bin/brew shellenv
+++ eval 'export HOMEBREW_PREFIX="/opt/homebrew";
export HOMEBREW_CELLAR="/opt/homebrew/Cellar";
export HOMEBREW_REPOSITORY="/opt/homebrew";
export PATH="/opt/homebrew/bin:/opt/homebrew/sbin${PATH+:$PATH}";
export MANPATH="/opt/homebrew/share/man${MANPATH+:$MANPATH}:";
export INFOPATH="/opt/homebrew/share/info:${INFOPATH:-}";'
++++ export HOMEBREW_PREFIX=/opt/homebrew
++++ HOMEBREW_PREFIX=/opt/homebrew
++++ export HOMEBREW_CELLAR=/opt/homebrew/Cellar
++++ HOMEBREW_CELLAR=/opt/homebrew/Cellar
++++ export HOMEBREW_REPOSITORY=/opt/homebrew
++++ HOMEBREW_REPOSITORY=/opt/homebrew
++++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin
++++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin
++++ export MANPATH=/opt/homebrew/share/man:
++++ MANPATH=/opt/homebrew/share/man:
++++ export INFOPATH=/opt/homebrew/share/info:
++++ INFOPATH=/opt/homebrew/share/info:
+++ [[ -r /opt/homebrew/etc/profile.d/bash_completion.sh ]]
+++ . /opt/homebrew/etc/profile.d/bash_completion.sh
++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']'
++++ return
++ [[ viggen == *\m\a\c\y\s* ]]
++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ [[ viggen == \m\a\c\y\s ]]
++ export CASARCH=.
++ CASARCH=.
++ '[' '!' -z '' ']'
+++ ls -d '/Users/jenkins/util/ESP/OpenCASCADE-.?'
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/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib
++ DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//lib:/lib:/opt/intel/oneapi/tbb/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib
++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.9
++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.9
++ [[ viggen == *\m\a\c\y\s* ]]
++ export AFLR_ARCH=MacOSX-arm64
++ AFLR_ARCH=MacOSX-arm64
++ export ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ export PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ export CART3D_ARCH=OSX64_ICC
++ CART3D_ARCH=OSX64_ICC
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.34.0-MacOS
++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.34.0-MacOS
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ [[ viggen == \m\a\c\y\s ]]
++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']'
+++ perl -I/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 -Mlocal::lib=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
++ eval 'PATH="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin${PATH:+:${PATH}}"; export PATH;
PERL5LIB="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5${PERL5LIB:+:${PERL5LIB}}"; export PERL5LIB;
PERL_LOCAL_LIB_ROOT="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl${PERL_LOCAL_LIB_ROOT:+:${PERL_LOCAL_LIB_ROOT}}"; export PERL_LOCAL_LIB_ROOT;
PERL_MB_OPT="--install_base \"/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl\""; export PERL_MB_OPT;
PERL_MM_OPT="INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"; export PERL_MM_OPT;'
+++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
+++ export PATH
+++ PERL5LIB=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5
+++ export PERL5LIB
+++ PERL_LOCAL_LIB_ROOT=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
+++ export PERL_LOCAL_LIB_ROOT
+++ PERL_MB_OPT='--install_base "/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"'
+++ export PERL_MB_OPT
+++ PERL_MM_OPT=INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
+++ export PERL_MM_OPT
++ export PATH=/Users/jenkins/workspace/ESP_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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/workspace/ESP_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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_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
++ [[ viggen == \m\a\c\y\s* ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ 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-*'
++ [[ viggen == \m\a\c\y\s ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/python3 /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/python3-config /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python-config
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/virtualenv /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/virtualenv
+++ ls /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-cc /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-build
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-build
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-build /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-build
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-c++
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-c++
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-c++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-c++
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-cc
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-cc
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-cc /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-cc
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-build
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-build
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-build /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/intercept-build
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-c++
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-c++
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-c++ /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/intercept-c++
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-cc
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-cc
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11'
++ PYTHONINC='. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation'
++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation'
++ [[ viggen == \m\a\c\y\s ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w'
++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w'
++ export PYTHONUNBUFFERED=true
++ PYTHONUNBUFFERED=true
++ export PYTHONFAULTHANDLER=true
++ PYTHONFAULTHANDLER=true
++ python --version
Python 3.11.6
++ [[ '' == \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=arm64
+ wget --tries=3 https://acdl.mit.edu/ESP/archive/ESPbeta-macos-arm64.tgz
--2024-03-06 20:30:41--  https://acdl.mit.edu/ESP/archive/ESPbeta-macos-arm64.tgz
Resolving acdl.mit.edu (acdl.mit.edu)... 18.18.33.14
Connecting to acdl.mit.edu (acdl.mit.edu)|18.18.33.14|:443... connected.
HTTP request sent, awaiting response... 200 OK
Length: 515690371 (492M) [application/x-gzip]
Saving to: ‘ESPbeta-macos-arm64.tgz’

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  9200K .......... .......... .......... .......... ..........  1% 17.5M 27s
  9250K .......... .......... .......... .......... ..........  1% 22.1M 27s
  9300K .......... .......... .......... .......... ..........  1% 24.6M 27s
  9350K .......... .......... .......... .......... ..........  1% 18.9M 27s
  9400K .......... .......... .......... .......... ..........  1% 22.1M 27s
  9450K .......... .......... .......... .......... ..........  1% 18.1M 27s
  9500K .......... .......... .......... .......... ..........  1% 19.8M 27s
  9550K .......... .......... .......... .......... ..........  1% 29.1M 27s
  9600K .......... .......... .......... .......... ..........  1% 18.7M 27s
  9650K .......... .......... .......... .......... ..........  1% 25.1M 27s
  9700K .......... .......... .......... .......... ..........  1% 13.4M 27s
  9750K .......... .......... .......... .......... ..........  1% 27.1M 27s
  9800K .......... .......... .......... .......... ..........  1% 29.0M 27s
  9850K .......... .......... .......... .......... ..........  1% 19.7M 27s
  9900K .......... .......... .......... .......... ..........  1% 85.7M 27s
  9950K .......... .......... .......... .......... ..........  1% 56.7M 27s
 10000K .......... .......... .......... .......... ..........  1% 40.8M 27s
 10050K .......... .......... .......... .......... ..........  2% 41.2M 27s
 10100K .......... .......... .......... .......... ..........  2% 16.4M 27s
 10150K .......... .......... .......... .......... ..........  2% 88.6M 27s
 10200K .......... .......... .......... .......... ..........  2% 24.6M 26s
 10250K .......... .......... .......... .......... ..........  2% 64.8M 26s
 10300K .......... .......... .......... .......... ..........  2% 20.9M 26s
 10350K .......... .......... .......... .......... ..........  2% 20.9M 26s
 10400K .......... .......... .......... .......... ..........  2% 25.6M 26s
 10450K .......... .......... .......... .......... ..........  2% 16.7M 26s
 10500K .......... .......... .......... .......... ..........  2% 31.7M 26s
 10550K .......... .......... .......... .......... ..........  2% 19.8M 26s
 10600K .......... .......... .......... .......... ..........  2% 17.9M 26s
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 10700K .......... .......... .......... .......... ..........  2% 19.7M 26s
 10750K .......... .......... .......... .......... ..........  2% 27.3M 26s
 10800K .......... .......... .......... .......... ..........  2% 16.2M 26s
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 11500K .......... .......... .......... .......... ..........  2% 28.4M 26s
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 11750K .......... .......... .......... .......... ..........  2% 27.9M 26s
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 12050K .......... .......... .......... .......... ..........  2% 64.9M 26s
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 12150K .......... .......... .......... .......... ..........  2% 33.5M 26s
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 12300K .......... .......... .......... .......... ..........  2% 33.9M 25s
 12350K .......... .......... .......... .......... ..........  2% 75.6M 25s
 12400K .......... .......... .......... .......... ..........  2% 31.7M 25s
 12450K .......... .......... .......... .......... ..........  2% 40.8M 25s
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 12550K .......... .......... .......... .......... ..........  2%  117M 25s
 12600K .......... .......... .......... .......... ..........  2%  103M 25s
 12650K .......... .......... .......... .......... ..........  2% 28.3M 25s
 12700K .......... .......... .......... .......... ..........  2% 30.0M 25s
 12750K .......... .......... .......... .......... ..........  2% 22.1M 25s
 12800K .......... .......... .......... .......... ..........  2% 26.2M 25s
 12850K .......... .......... .......... .......... ..........  2% 19.9M 25s
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 13050K .......... .......... .......... .......... ..........  2% 15.0M 25s
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 13200K .......... .......... .......... .......... ..........  2% 9.28M 25s
 13250K .......... .......... .......... .......... ..........  2% 10.5M 25s
 13300K .......... .......... .......... .......... ..........  2% 9.75M 25s
 13350K .......... .......... .......... .......... ..........  2% 8.41M 25s
 13400K .......... .......... .......... .......... ..........  2% 7.80M 26s
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 13550K .......... .......... .......... .......... ..........  2% 4.00M 27s
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 13800K .......... .......... .......... .......... ..........  2% 21.2M 28s
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 14150K .......... .......... .......... .......... ..........  2% 16.6M 28s
 14200K .......... .......... .......... .......... ..........  2% 15.7M 28s
 14250K .......... .......... .......... .......... ..........  2% 26.9M 28s
 14300K .......... .......... .......... .......... ..........  2% 17.1M 28s
 14350K .......... .......... .......... .......... ..........  2% 16.4M 28s
 14400K .......... .......... .......... .......... ..........  2% 26.6M 28s
 14450K .......... .......... .......... .......... ..........  2% 26.9M 28s
 14500K .......... .......... .......... .......... ..........  2% 61.0M 28s
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 14700K .......... .......... .......... .......... ..........  2% 25.5M 27s
 14750K .......... .......... .......... .......... ..........  2% 24.6M 27s
 14800K .......... .......... .......... .......... ..........  2% 31.4M 27s
 14850K .......... .......... .......... .......... ..........  2% 22.8M 27s
 14900K .......... .......... .......... .......... ..........  2% 67.7M 27s
 14950K .......... .......... .......... .......... ..........  2% 24.6M 27s
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 15050K .......... .......... .......... .......... ..........  2% 27.9M 27s
 15100K .......... .......... .......... .......... ..........  3% 25.4M 27s
 15150K .......... .......... .......... .......... ..........  3% 22.0M 27s
 15200K .......... .......... .......... .......... ..........  3% 54.2M 27s
 15250K .......... .......... .......... .......... ..........  3% 31.1M 27s
 15300K .......... .......... .......... .......... ..........  3% 22.2M 27s
 15350K .......... .......... .......... .......... ..........  3% 23.4M 27s
 15400K .......... .......... .......... .......... ..........  3% 23.2M 27s
 15450K .......... .......... .......... .......... ..........  3% 15.7M 27s
 15500K .......... .......... .......... .......... ..........  3% 17.0M 27s
 15550K .......... .......... .......... .......... ..........  3% 23.4M 27s
 15600K .......... .......... .......... .......... ..........  3% 12.6M 27s
 15650K .......... .......... .......... .......... ..........  3% 15.7M 27s
 15700K .......... .......... .......... .......... ..........  3% 12.1M 27s
 15750K .......... .......... .......... .......... ..........  3% 17.1M 27s
 15800K .......... .......... .......... .......... ..........  3% 15.1M 27s
 15850K .......... .......... .......... .......... ..........  3% 9.02M 27s
 15900K .......... .......... .......... .......... ..........  3% 10.7M 27s
 15950K .......... .......... .......... .......... ..........  3% 7.27M 27s
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 16050K .......... .......... .......... .......... ..........  3% 8.28M 28s
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 16300K .......... .......... .......... .......... ..........  3% 27.0M 28s
 16350K .......... .......... .......... .......... ..........  3% 15.0M 28s
 16400K .......... .......... .......... .......... ..........  3% 18.1M 28s
 16450K .......... .......... .......... .......... ..........  3% 25.3M 28s
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 16550K .......... .......... .......... .......... ..........  3% 24.1M 28s
 16600K .......... .......... .......... .......... ..........  3% 17.5M 28s
 16650K .......... .......... .......... .......... ..........  3% 28.5M 28s
 16700K .......... .......... .......... .......... ..........  3% 25.0M 27s
 16750K .......... .......... .......... .......... ..........  3% 25.3M 27s
 16800K .......... .......... .......... .......... ..........  3% 28.1M 27s
 16850K .......... .......... .......... .......... ..........  3% 15.7M 27s
 16900K .......... .......... .......... .......... ..........  3% 26.6M 27s
 16950K .......... .......... .......... .......... ..........  3% 27.5M 27s
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 17050K .......... .......... .......... .......... ..........  3% 26.5M 27s
 17100K .......... .......... .......... .......... ..........  3% 24.7M 27s
 17150K .......... .......... .......... .......... ..........  3% 20.9M 27s
 17200K .......... .......... .......... .......... ..........  3% 16.2M 27s
 17250K .......... .......... .......... .......... ..........  3% 23.2M 27s
 17300K .......... .......... .......... .......... ..........  3% 26.8M 27s
 17350K .......... .......... .......... .......... ..........  3% 25.8M 27s
 17400K .......... .......... .......... .......... ..........  3% 32.0M 27s
 17450K .......... .......... .......... .......... ..........  3% 17.1M 27s
 17500K .......... .......... .......... .......... ..........  3% 62.8M 27s
 17550K .......... .......... .......... .......... ..........  3% 21.6M 27s
 17600K .......... .......... .......... .......... ..........  3% 15.1M 27s
 17650K .......... .......... .......... .......... ..........  3% 64.4M 27s
 17700K .......... .......... .......... .......... ..........  3% 16.0M 27s
 17750K .......... .......... .......... .......... ..........  3% 26.8M 27s
 17800K .......... .......... .......... .......... ..........  3% 28.9M 27s
 17850K .......... .......... .......... .......... ..........  3% 20.8M 27s
 17900K .......... .......... .......... .......... ..........  3% 22.0M 27s
 17950K .......... .......... .......... .......... ..........  3% 12.6M 27s
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 18050K .......... .......... .......... .......... ..........  3% 15.6M 27s
 18100K .......... .......... .......... .......... ..........  3% 10.5M 27s
 18150K .......... .......... .......... .......... ..........  3% 13.0M 27s
 18200K .......... .......... .......... .......... ..........  3% 8.39M 27s
 18250K .......... .......... .......... .......... ..........  3% 6.13M 27s
 18300K .......... .......... .......... .......... ..........  3% 5.14M 27s
 18350K .......... .......... .......... .......... ..........  3% 4.98M 28s
 18400K .......... .......... .......... .......... ..........  3% 19.0M 28s
 18450K .......... .......... .......... .......... ..........  3% 8.21M 28s
 18500K .......... .......... .......... .......... ..........  3% 87.0M 28s
 18550K .......... .......... .......... .......... ..........  3% 16.6M 28s
 18600K .......... .......... .......... .......... ..........  3% 16.9M 28s
 18650K .......... .......... .......... .......... ..........  3% 17.1M 28s
 18700K .......... .......... .......... .......... ..........  3% 15.6M 28s
 18750K .......... .......... .......... .......... ..........  3% 16.3M 28s
 18800K .......... .......... .......... .......... ..........  3% 18.9M 28s
 18850K .......... .......... .......... .......... ..........  3% 17.1M 28s
 18900K .......... .......... .......... .......... ..........  3% 15.0M 28s
 18950K .......... .......... .......... .......... ..........  3% 6.99M 28s
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 19150K .......... .......... .......... .......... ..........  3% 9.27M 28s
 19200K .......... .......... .......... .......... ..........  3% 7.16M 28s
 19250K .......... .......... .......... .......... ..........  3% 7.83M 28s
 19300K .......... .......... .......... .......... ..........  3% 14.1M 28s
 19350K .......... .......... .......... .......... ..........  3% 21.0M 28s
 19400K .......... .......... .......... .......... ..........  3% 26.5M 28s
 19450K .......... .......... .......... .......... ..........  3% 14.9M 28s
 19500K .......... .......... .......... .......... ..........  3% 60.4M 28s
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 19600K .......... .......... .......... .......... ..........  3% 17.1M 28s
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 19700K .......... .......... .......... .......... ..........  3% 17.4M 28s
 19750K .......... .......... .......... .......... ..........  3% 15.0M 28s
 19800K .......... .......... .......... .......... ..........  3% 16.9M 28s
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 20100K .......... .......... .......... .......... ..........  4% 12.0M 28s
 20150K .......... .......... .......... .......... ..........  4% 14.0M 28s
 20200K .......... .......... .......... .......... ..........  4% 12.5M 28s
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 20300K .......... .......... .......... .......... ..........  4% 21.9M 28s
 20350K .......... .......... .......... .......... ..........  4% 23.6M 28s
 20400K .......... .......... .......... .......... ..........  4% 30.0M 28s
 20450K .......... .......... .......... .......... ..........  4% 19.2M 28s
 20500K .......... .......... .......... .......... ..........  4% 73.8M 28s
 20550K .......... .......... .......... .......... ..........  4% 19.6M 28s
 20600K .......... .......... .......... .......... ..........  4% 18.9M 28s
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 20700K .......... .......... .......... .......... ..........  4% 12.6M 28s
 20750K .......... .......... .......... .......... ..........  4% 17.0M 28s
 20800K .......... .......... .......... .......... ..........  4% 16.4M 28s
 20850K .......... .......... .......... .......... ..........  4% 12.5M 28s
 20900K .......... .......... .......... .......... ..........  4% 21.0M 28s
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 21000K .......... .......... .......... .......... ..........  4% 12.8M 28s
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 21500K .......... .......... .......... .......... ..........  4% 32.8M 28s
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 21700K .......... .......... .......... .......... ..........  4% 19.8M 28s
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 22050K .......... .......... .......... .......... ..........  4% 23.0M 28s
 22100K .......... .......... .......... .......... ..........  4% 18.7M 28s
 22150K .......... .......... .......... .......... ..........  4% 18.9M 28s
 22200K .......... .......... .......... .......... ..........  4% 13.8M 28s
 22250K .......... .......... .......... .......... ..........  4% 21.1M 28s
 22300K .......... .......... .......... .......... ..........  4% 16.5M 28s
 22350K .......... .......... .......... .......... ..........  4% 14.0M 28s
 22400K .......... .......... .......... .......... ..........  4% 18.9M 28s
 22450K .......... .......... .......... .......... ..........  4% 15.3M 28s
 22500K .......... .......... .......... .......... ..........  4% 17.1M 28s
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 22600K .......... .......... .......... .......... ..........  4% 16.6M 28s
 22650K .......... .......... .......... .......... ..........  4% 19.1M 28s
 22700K .......... .......... .......... .......... ..........  4% 14.5M 28s
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 22800K .......... .......... .......... .......... ..........  4% 14.1M 28s
 22850K .......... .......... .......... .......... ..........  4% 18.4M 28s
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 23000K .......... .......... .......... .......... ..........  4% 19.9M 28s
 23050K .......... .......... .......... .......... ..........  4% 23.8M 28s
 23100K .......... .......... .......... .......... ..........  4% 15.6M 28s
 23150K .......... .......... .......... .......... ..........  4% 20.7M 28s
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 37050K .......... .......... .......... .......... ..........  7% 16.6M 28s
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 50650K .......... .......... .......... .......... .......... 10% 12.5M 31s
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 50850K .......... .......... .......... .......... .......... 10% 9.00M 31s
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 50950K .......... .......... .......... .......... .......... 10% 7.69M 31s
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 51100K .......... .......... .......... .......... .......... 10% 6.63M 31s
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 80200K .......... .......... .......... .......... .......... 15% 35.1M 32s
 80250K .......... .......... .......... .......... .......... 15% 23.4M 32s
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 82050K .......... .......... .......... .......... .......... 16% 16.4M 32s
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 82150K .......... .......... .......... .......... .......... 16% 17.1M 32s
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 83100K .......... .......... .......... .......... .......... 16% 12.9M 32s
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 87250K .......... .......... .......... .......... .......... 17% 94.3M 32s
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 89100K .......... .......... .......... .......... .......... 17% 19.1M 32s
 89150K .......... .......... .......... .......... .......... 17% 30.3M 32s
 89200K .......... .......... .......... .......... .......... 17% 17.9M 32s
 89250K .......... .......... .......... .......... .......... 17% 27.7M 31s
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 90050K .......... .......... .......... .......... .......... 17% 18.6M 31s
 90100K .......... .......... .......... .......... .......... 17% 13.7M 31s
 90150K .......... .......... .......... .......... .......... 17% 35.9M 31s
 90200K .......... .......... .......... .......... .......... 17% 13.9M 31s
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 90700K .......... .......... .......... .......... .......... 18% 69.2M 31s
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 91100K .......... .......... .......... .......... .......... 18% 19.8M 31s
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 91200K .......... .......... .......... .......... .......... 18% 12.8M 31s
 91250K .......... .......... .......... .......... .......... 18% 21.1M 31s
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 91600K .......... .......... .......... .......... .......... 18% 6.66M 31s
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 91800K .......... .......... .......... .......... .......... 18% 30.5M 31s
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 91900K .......... .......... .......... .......... .......... 18% 19.0M 31s
 91950K .......... .......... .......... .......... .......... 18% 23.5M 31s
 92000K .......... .......... .......... .......... .......... 18% 15.7M 31s
 92050K .......... .......... .......... .......... .......... 18% 11.5M 31s
 92100K .......... .......... .......... .......... .......... 18% 15.0M 31s
 92150K .......... .......... .......... .......... .......... 18% 14.5M 31s
 92200K .......... .......... .......... .......... .......... 18% 9.18M 31s
 92250K .......... .......... .......... .......... .......... 18% 15.7M 31s
 92300K .......... .......... .......... .......... .......... 18% 15.6M 31s
 92350K .......... .......... .......... .......... .......... 18% 11.3M 31s
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 92450K .......... .......... .......... .......... .......... 18% 10.8M 31s
 92500K .......... .......... .......... .......... .......... 18% 11.1M 31s
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 92600K .......... .......... .......... .......... .......... 18% 10.5M 31s
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 92700K .......... .......... .......... .......... .......... 18% 9.24M 31s
 92750K .......... .......... .......... .......... .......... 18% 10.3M 31s
 92800K .......... .......... .......... .......... .......... 18% 13.7M 31s
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 92900K .......... .......... .......... .......... .......... 18% 27.1M 31s
 92950K .......... .......... .......... .......... .......... 18% 14.9M 31s
 93000K .......... .......... .......... .......... .......... 18% 21.2M 31s
 93050K .......... .......... .......... .......... .......... 18% 10.4M 31s
 93100K .......... .......... .......... .......... .......... 18% 6.63M 31s
 93150K .......... .......... .......... .......... .......... 18% 8.97M 31s
 93200K .......... .......... .......... .......... .......... 18% 8.37M 31s
 93250K .......... .......... .......... .......... .......... 18% 6.03M 31s
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 93450K .......... .......... .......... .......... .......... 18% 6.04M 31s
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 93850K .......... .......... .......... .......... .......... 18% 4.07M 31s
 93900K .......... .......... .......... .......... .......... 18% 5.21M 31s
 93950K .......... .......... .......... .......... .......... 18% 16.1M 31s
 94000K .......... .......... .......... .......... .......... 18% 18.4M 31s
 94050K .......... .......... .......... .......... .......... 18% 71.7M 31s
 94100K .......... .......... .......... .......... .......... 18% 15.9M 31s
 94150K .......... .......... .......... .......... .......... 18% 19.7M 31s
 94200K .......... .......... .......... .......... .......... 18% 62.8M 31s
 94250K .......... .......... .......... .......... .......... 18% 61.5M 31s
 94300K .......... .......... .......... .......... .......... 18% 34.0M 31s
 94350K .......... .......... .......... .......... .......... 18% 18.7M 31s
 94400K .......... .......... .......... .......... .......... 18% 17.1M 31s
 94450K .......... .......... .......... .......... .......... 18% 28.8M 31s
 94500K .......... .......... .......... .......... .......... 18% 18.7M 31s
 94550K .......... .......... .......... .......... .......... 18% 20.8M 31s
 94600K .......... .......... .......... .......... .......... 18% 17.0M 31s
 94650K .......... .......... .......... .......... .......... 18% 22.3M 31s
 94700K .......... .......... .......... .......... .......... 18% 16.4M 31s
 94750K .......... .......... .......... .......... .......... 18% 16.3M 31s
 94800K .......... .......... .......... .......... .......... 18% 21.5M 31s
 94850K .......... .......... .......... .......... .......... 18% 12.6M 31s
 94900K .......... .......... .......... .......... .......... 18% 14.0M 31s
 94950K .......... .......... .......... .......... .......... 18% 9.49M 31s
 95000K .......... .......... .......... .......... .......... 18% 8.80M 31s
 95050K .......... .......... .......... .......... .......... 18% 9.75M 31s
 95100K .......... .......... .......... .......... .......... 18% 14.0M 31s
 95150K .......... .......... .......... .......... .......... 18% 14.8M 31s
 95200K .......... .......... .......... .......... .......... 18% 9.29M 31s
 95250K .......... .......... .......... .......... .......... 18% 9.60M 31s
 95300K .......... .......... .......... .......... .......... 18% 9.09M 31s
 95350K .......... .......... .......... .......... .......... 18% 6.79M 31s
 95400K .......... .......... .......... .......... .......... 18% 10.6M 31s
 95450K .......... .......... .......... .......... .......... 18% 6.19M 31s
 95500K .......... .......... .......... .......... .......... 18% 13.1M 31s
 95550K .......... .......... .......... .......... .......... 18% 8.55M 31s
 95600K .......... .......... .......... .......... .......... 18% 9.00M 31s
 95650K .......... .......... .......... .......... .......... 19% 10.5M 31s
 95700K .......... .......... .......... .......... .......... 19% 8.24M 31s
 95750K .......... .......... .......... .......... .......... 19% 7.67M 31s
 95800K .......... .......... .......... .......... .......... 19% 11.1M 31s
 95850K .......... .......... .......... .......... .......... 19% 8.43M 31s
 95900K .......... .......... .......... .......... .......... 19% 9.91M 31s
 95950K .......... .......... .......... .......... .......... 19% 12.6M 31s
 96000K .......... .......... .......... .......... .......... 19% 15.0M 31s
 96050K .......... .......... .......... .......... .......... 19% 12.1M 31s
 96100K .......... .......... .......... .......... .......... 19% 7.87M 31s
 96150K .......... .......... .......... .......... .......... 19% 7.23M 31s
 96200K .......... .......... .......... .......... .......... 19% 5.99M 31s
 96250K .......... .......... .......... .......... .......... 19% 6.78M 31s
 96300K .......... .......... .......... .......... .......... 19% 6.11M 31s
 96350K .......... .......... .......... .......... .......... 19% 7.76M 31s
 96400K .......... .......... .......... .......... .......... 19% 28.4M 31s
 96450K .......... .......... .......... .......... .......... 19% 20.4M 31s
 96500K .......... .......... .......... .......... .......... 19% 18.7M 31s
 96550K .......... .......... .......... .......... .......... 19% 37.4M 31s
 96600K .......... .......... .......... .......... .......... 19% 12.9M 31s
 96650K .......... .......... .......... .......... .......... 19% 11.1M 31s
 96700K .......... .......... .......... .......... .......... 19% 11.7M 31s
 96750K .......... .......... .......... .......... .......... 19% 12.6M 31s
 96800K .......... .......... .......... .......... .......... 19% 11.4M 31s
 96850K .......... .......... .......... .......... .......... 19% 10.7M 31s
 96900K .......... .......... .......... .......... .......... 19% 11.6M 31s
 96950K .......... .......... .......... .......... .......... 19% 9.39M 31s
 97000K .......... .......... .......... .......... .......... 19% 9.29M 31s
 97050K .......... .......... .......... .......... .......... 19% 12.7M 31s
 97100K .......... .......... .......... .......... .......... 19% 16.0M 31s
 97150K .......... .......... .......... .......... .......... 19% 31.9M 31s
 97200K .......... .......... .......... .......... .......... 19% 28.8M 31s
 97250K .......... .......... .......... .......... .......... 19% 27.5M 31s
 97300K .......... .......... .......... .......... .......... 19% 30.8M 31s
 97350K .......... .......... .......... .......... .......... 19% 27.0M 31s
 97400K .......... .......... .......... .......... .......... 19% 27.9M 31s
 97450K .......... .......... .......... .......... .......... 19% 26.5M 31s
 97500K .......... .......... .......... .......... .......... 19% 20.9M 31s
 97550K .......... .......... .......... .......... .......... 19% 78.9M 31s
 97600K .......... .......... .......... .......... .......... 19% 29.5M 31s
 97650K .......... .......... .......... .......... .......... 19% 17.0M 31s
 97700K .......... .......... .......... .......... .......... 19% 14.4M 31s
 97750K .......... .......... .......... .......... .......... 19% 12.5M 31s
 97800K .......... .......... .......... .......... .......... 19% 18.9M 31s
 97850K .......... .......... .......... .......... .......... 19% 15.9M 31s
 97900K .......... .......... .......... .......... .......... 19% 15.5M 31s
 97950K .......... .......... .......... .......... .......... 19% 9.83M 31s
 98000K .......... .......... .......... .......... .......... 19% 12.1M 31s
 98050K .......... .......... .......... .......... .......... 19% 15.4M 31s
 98100K .......... .......... .......... .......... .......... 19% 10.9M 31s
 98150K .......... .......... .......... .......... .......... 19% 12.0M 31s
 98200K .......... .......... .......... .......... .......... 19% 9.83M 31s
 98250K .......... .......... .......... .......... .......... 19% 10.4M 31s
 98300K .......... .......... .......... .......... .......... 19% 8.47M 31s
 98350K .......... .......... .......... .......... .......... 19% 7.72M 31s
 98400K .......... .......... .......... .......... .......... 19% 6.65M 31s
 98450K .......... .......... .......... .......... .......... 19% 6.00M 31s
 98500K .......... .......... .......... .......... .......... 19% 6.13M 31s
 98550K .......... .......... .......... .......... .......... 19% 6.35M 31s
 98600K .......... .......... .......... .......... .......... 19% 6.60M 31s
 98650K .......... .......... .......... .......... .......... 19% 25.3M 31s
 98700K .......... .......... .......... .......... .......... 19% 18.9M 31s
 98750K .......... .......... .......... .......... .......... 19% 26.8M 31s
 98800K .......... .......... .......... .......... .......... 19% 20.9M 31s
 98850K .......... .......... .......... .......... .......... 19% 23.4M 31s
 98900K .......... .......... .......... .......... .......... 19% 17.8M 31s
 98950K .......... .......... .......... .......... .......... 19% 15.5M 31s
 99000K .......... .......... .......... .......... .......... 19% 15.6M 31s
 99050K .......... .......... .......... .......... .......... 19% 15.1M 31s
 99100K .......... .......... .......... .......... .......... 19% 13.3M 31s
 99150K .......... .......... .......... .......... .......... 19% 12.9M 31s
 99200K .......... .......... .......... .......... .......... 19% 14.0M 31s
 99250K .......... .......... .......... .......... .......... 19% 13.7M 31s
 99300K .......... .......... .......... .......... .......... 19% 14.5M 31s
 99350K .......... .......... .......... .......... .......... 19% 15.1M 31s
 99400K .......... .......... .......... .......... .......... 19% 15.0M 31s
 99450K .......... .......... .......... .......... .......... 19% 13.4M 31s
 99500K .......... .......... .......... .......... .......... 19% 15.0M 31s
 99550K .......... .......... .......... .......... .......... 19% 13.9M 31s
 99600K .......... .......... .......... .......... .......... 19% 12.5M 31s
 99650K .......... .......... .......... .......... .......... 19% 13.9M 31s
 99700K .......... .......... .......... .......... .......... 19% 15.1M 31s
 99750K .......... .......... .......... .......... .......... 19% 13.9M 31s
 99800K .......... .......... .......... .......... .......... 19% 15.9M 31s
 99850K .......... .......... .......... .......... .......... 19% 7.78M 31s
 99900K .......... .......... .......... .......... .......... 19% 9.44M 31s
 99950K .......... .......... .......... .......... .......... 19% 5.64M 31s
100000K .......... .......... .......... .......... .......... 19% 6.43M 31s
100050K .......... .......... .......... .......... .......... 19% 7.59M 31s
100100K .......... .......... .......... .......... .......... 19% 5.52M 31s
100150K .......... .......... .......... .......... .......... 19% 10.0M 31s
100200K .......... .......... .......... .......... .......... 19% 9.86M 31s
100250K .......... .......... .......... .......... .......... 19% 9.22M 31s
100300K .......... .......... .......... .......... .......... 19% 10.1M 31s
100350K .......... .......... .......... .......... .......... 19% 9.44M 31s
100400K .......... .......... .......... .......... .......... 19% 12.1M 31s
100450K .......... .......... .......... .......... .......... 19% 9.44M 31s
100500K .......... .......... .......... .......... .......... 19% 11.8M 31s
100550K .......... .......... .......... .......... .......... 19% 12.9M 31s
100600K .......... .......... .......... .......... .......... 19% 11.1M 31s
100650K .......... .......... .......... .......... .......... 19% 10.8M 31s
100700K .......... .......... .......... .......... .......... 20% 20.9M 31s
100750K .......... .......... .......... .......... .......... 20% 40.9M 31s
100800K .......... .......... .......... .......... .......... 20% 20.2M 31s
100850K .......... .......... .......... .......... .......... 20% 25.9M 31s
100900K .......... .......... .......... .......... .......... 20% 55.4M 31s
100950K .......... .......... .......... .......... .......... 20% 20.4M 31s
101000K .......... .......... .......... .......... .......... 20% 19.0M 31s
101050K .......... .......... .......... .......... .......... 20% 19.8M 31s
101100K .......... .......... .......... .......... .......... 20% 19.9M 31s
101150K .......... .......... .......... .......... .......... 20% 18.1M 31s
101200K .......... .......... .......... .......... .......... 20% 14.2M 31s
101250K .......... .......... .......... .......... .......... 20% 13.4M 31s
101300K .......... .......... .......... .......... .......... 20% 11.1M 31s
101350K .......... .......... .......... .......... .......... 20% 11.4M 31s
101400K .......... .......... .......... .......... .......... 20% 11.4M 31s
101450K .......... .......... .......... .......... .......... 20% 11.4M 31s
101500K .......... .......... .......... .......... .......... 20% 11.4M 31s
101550K .......... .......... .......... .......... .......... 20% 10.2M 31s
101600K .......... .......... .......... .......... .......... 20% 8.70M 31s
101650K .......... .......... .......... .......... .......... 20% 9.56M 31s
101700K .......... .......... .......... .......... .......... 20% 6.59M 31s
101750K .......... .......... .......... .......... .......... 20% 10.2M 31s
101800K .......... .......... .......... .......... .......... 20% 7.25M 31s
101850K .......... .......... .......... .......... .......... 20% 6.95M 31s
101900K .......... .......... .......... .......... .......... 20% 6.85M 31s
101950K .......... .......... .......... .......... .......... 20% 7.81M 31s
102000K .......... .......... .......... .......... .......... 20% 8.64M 31s
102050K .......... .......... .......... .......... .......... 20% 6.21M 31s
102100K .......... .......... .......... .......... .......... 20% 5.29M 31s
102150K .......... .......... .......... .......... .......... 20% 4.91M 31s
102200K .......... .......... .......... .......... .......... 20% 8.37M 31s
102250K .......... .......... .......... .......... .......... 20% 7.80M 31s
102300K .......... .......... .......... .......... .......... 20% 8.04M 31s
102350K .......... .......... .......... .......... .......... 20% 7.69M 31s
102400K .......... .......... .......... .......... .......... 20% 8.79M 31s
102450K .......... .......... .......... .......... .......... 20% 8.58M 31s
102500K .......... .......... .......... .......... .......... 20% 7.38M 31s
102550K .......... .......... .......... .......... .......... 20% 7.43M 31s
102600K .......... .......... .......... .......... .......... 20% 5.75M 31s
102650K .......... .......... .......... .......... .......... 20% 5.51M 31s
102700K .......... .......... .......... .......... .......... 20% 5.62M 31s
102750K .......... .......... .......... .......... .......... 20% 15.1M 31s
102800K .......... .......... .......... .......... .......... 20% 22.4M 31s
102850K .......... .......... .......... .......... .......... 20% 15.4M 31s
102900K .......... .......... .......... .......... .......... 20% 17.1M 31s
102950K .......... .......... .......... .......... .......... 20% 15.1M 31s
103000K .......... .......... .......... .......... .......... 20% 14.0M 31s
103050K .......... .......... .......... .......... .......... 20% 20.9M 31s
103100K .......... .......... .......... .......... .......... 20% 12.4M 31s
103150K .......... .......... .......... .......... .......... 20% 15.0M 31s
103200K .......... .......... .......... .......... .......... 20% 11.0M 31s
103250K .......... .......... .......... .......... .......... 20% 11.8M 31s
103300K .......... .......... .......... .......... .......... 20% 6.88M 31s
103350K .......... .......... .......... .......... .......... 20% 6.40M 31s
103400K .......... .......... .......... .......... .......... 20% 6.88M 31s
103450K .......... .......... .......... .......... .......... 20% 4.73M 31s
103500K .......... .......... .......... .......... .......... 20% 6.85M 31s
103550K .......... .......... .......... .......... .......... 20% 5.74M 31s
103600K .......... .......... .......... .......... .......... 20% 3.74M 31s
103650K .......... .......... .......... .......... .......... 20% 6.84M 31s
103700K .......... .......... .......... .......... .......... 20% 10.4M 31s
103750K .......... .......... .......... .......... .......... 20% 26.2M 31s
103800K .......... .......... .......... .......... .......... 20% 26.9M 31s
103850K .......... .......... .......... .......... .......... 20% 12.9M 31s
103900K .......... .......... .......... .......... .......... 20% 14.4M 31s
103950K .......... .......... .......... .......... .......... 20% 8.18M 31s
104000K .......... .......... .......... .......... .......... 20% 7.90M 31s
104050K .......... .......... .......... .......... .......... 20% 10.2M 31s
104100K .......... .......... .......... .......... .......... 20% 7.00M 31s
104150K .......... .......... .......... .......... .......... 20% 6.74M 31s
104200K .......... .......... .......... .......... .......... 20% 6.02M 31s
104250K .......... .......... .......... .......... .......... 20% 5.92M 31s
104300K .......... .......... .......... .......... .......... 20% 6.65M 31s
104350K .......... .......... .......... .......... .......... 20% 6.53M 31s
104400K .......... .......... .......... .......... .......... 20% 6.99M 31s
104450K .......... .......... .......... .......... .......... 20% 5.16M 31s
104500K .......... .......... .......... .......... .......... 20% 5.73M 31s
104550K .......... .......... .......... .......... .......... 20% 5.05M 31s
104600K .......... .......... .......... .......... .......... 20% 7.42M 31s
104650K .......... .......... .......... .......... .......... 20% 9.26M 31s
104700K .......... .......... .......... .......... .......... 20% 6.34M 31s
104750K .......... .......... .......... .......... .......... 20% 7.62M 31s
104800K .......... .......... .......... .......... .......... 20% 8.61M 31s
104850K .......... .......... .......... .......... .......... 20% 12.1M 31s
104900K .......... .......... .......... .......... .......... 20% 26.8M 31s
104950K .......... .......... .......... .......... .......... 20% 20.5M 31s
105000K .......... .......... .......... .......... .......... 20% 18.1M 31s
105050K .......... .......... .......... .......... .......... 20% 14.5M 31s
105100K .......... .......... .......... .......... .......... 20% 8.36M 31s
105150K .......... .......... .......... .......... .......... 20% 12.2M 31s
105200K .......... .......... .......... .......... .......... 20% 9.40M 31s
105250K .......... .......... .......... .......... .......... 20% 12.5M 31s
105300K .......... .......... .......... .......... .......... 20% 10.7M 31s
105350K .......... .......... .......... .......... .......... 20% 9.41M 31s
105400K .......... .......... .......... .......... .......... 20% 11.3M 31s
105450K .......... .......... .......... .......... .......... 20% 8.13M 31s
105500K .......... .......... .......... .......... .......... 20% 7.64M 31s
105550K .......... .......... .......... .......... .......... 20% 7.06M 31s
105600K .......... .......... .......... .......... .......... 20% 6.12M 31s
105650K .......... .......... .......... .......... .......... 20% 6.84M 31s
105700K .......... .......... .......... .......... .......... 20% 6.40M 31s
105750K .......... .......... .......... .......... .......... 21% 5.74M 31s
105800K .......... .......... .......... .......... .......... 21% 11.1M 31s
105850K .......... .......... .......... .......... .......... 21% 9.93M 31s
105900K .......... .......... .......... .......... .......... 21% 9.48M 31s
105950K .......... .......... .......... .......... .......... 21% 8.96M 31s
106000K .......... .......... .......... .......... .......... 21% 10.2M 31s
106050K .......... .......... .......... .......... .......... 21% 9.71M 31s
106100K .......... .......... .......... .......... .......... 21% 10.1M 31s
106150K .......... .......... .......... .......... .......... 21% 10.4M 31s
106200K .......... .......... .......... .......... .......... 21% 11.4M 31s
106250K .......... .......... .......... .......... .......... 21% 25.3M 31s
106300K .......... .......... .......... .......... .......... 21% 31.2M 31s
106350K .......... .......... .......... .......... .......... 21% 20.1M 31s
106400K .......... .......... .......... .......... .......... 21% 48.9M 31s
106450K .......... .......... .......... .......... .......... 21% 10.4M 31s
106500K .......... .......... .......... .......... .......... 21% 83.0M 31s
106550K .......... .......... .......... .......... .......... 21% 15.6M 31s
106600K .......... .......... .......... .......... .......... 21% 15.0M 31s
106650K .......... .......... .......... .......... .......... 21% 17.7M 31s
106700K .......... .......... .......... .......... .......... 21% 13.4M 31s
106750K .......... .......... .......... .......... .......... 21% 17.3M 31s
106800K .......... .......... .......... .......... .......... 21% 9.94M 31s
106850K .......... .......... .......... .......... .......... 21% 16.4M 31s
106900K .......... .......... .......... .......... .......... 21% 15.1M 31s
106950K .......... .......... .......... .......... .......... 21% 11.8M 31s
107000K .......... .......... .......... .......... .......... 21% 16.5M 31s
107050K .......... .......... .......... .......... .......... 21% 11.9M 31s
107100K .......... .......... .......... .......... .......... 21% 9.91M 31s
107150K .......... .......... .......... .......... .......... 21% 13.5M 31s
107200K .......... .......... .......... .......... .......... 21% 9.23M 31s
107250K .......... .......... .......... .......... .......... 21% 10.9M 31s
107300K .......... .......... .......... .......... .......... 21% 7.83M 31s
107350K .......... .......... .......... .......... .......... 21% 6.86M 31s
107400K .......... .......... .......... .......... .......... 21% 7.13M 31s
107450K .......... .......... .......... .......... .......... 21% 8.07M 31s
107500K .......... .......... .......... .......... .......... 21% 7.33M 31s
107550K .......... .......... .......... .......... .......... 21% 6.22M 31s
107600K .......... .......... .......... .......... .......... 21% 5.41M 31s
107650K .......... .......... .......... .......... .......... 21% 6.57M 31s
107700K .......... .......... .......... .......... .......... 21% 3.89M 31s
107750K .......... .......... .......... .......... .......... 21% 5.55M 31s
107800K .......... .......... .......... .......... .......... 21% 5.74M 31s
107850K .......... .......... .......... .......... .......... 21% 6.27M 31s
107900K .......... .......... .......... .......... .......... 21% 8.05M 31s
107950K .......... .......... .......... .......... .......... 21% 6.82M 31s
108000K .......... .......... .......... .......... .......... 21% 7.16M 31s
108050K .......... .......... .......... .......... .......... 21% 8.84M 31s
108100K .......... .......... .......... .......... .......... 21% 7.60M 31s
108150K .......... .......... .......... .......... .......... 21% 28.6M 31s
108200K .......... .......... .......... .......... .......... 21% 18.3M 31s
108250K .......... .......... .......... .......... .......... 21% 20.2M 31s
108300K .......... .......... .......... .......... .......... 21% 10.3M 31s
108350K .......... .......... .......... .......... .......... 21% 7.87M 31s
108400K .......... .......... .......... .......... .......... 21% 9.14M 31s
108450K .......... .......... .......... .......... .......... 21% 7.88M 31s
108500K .......... .......... .......... .......... .......... 21% 7.70M 31s
108550K .......... .......... .......... .......... .......... 21% 9.45M 31s
108600K .......... .......... .......... .......... .......... 21% 6.73M 31s
108650K .......... .......... .......... .......... .......... 21% 7.75M 31s
108700K .......... .......... .......... .......... .......... 21% 6.91M 31s
108750K .......... .......... .......... .......... .......... 21% 8.43M 31s
108800K .......... .......... .......... .......... .......... 21% 10.3M 31s
108850K .......... .......... .......... .......... .......... 21% 14.0M 31s
108900K .......... .......... .......... .......... .......... 21% 31.6M 31s
108950K .......... .......... .......... .......... .......... 21% 19.1M 31s
109000K .......... .......... .......... .......... .......... 21% 17.1M 31s
109050K .......... .......... .......... .......... .......... 21% 10.2M 31s
109100K .......... .......... .......... .......... .......... 21% 9.44M 31s
109150K .......... .......... .......... .......... .......... 21% 11.7M 31s
109200K .......... .......... .......... .......... .......... 21% 9.70M 31s
109250K .......... .......... .......... .......... .......... 21% 14.0M 31s
109300K .......... .......... .......... .......... .......... 21% 10.3M 31s
109350K .......... .......... .......... .......... .......... 21% 6.42M 31s
109400K .......... .......... .......... .......... .......... 21% 17.9M 31s
109450K .......... .......... .......... .......... .......... 21% 12.6M 31s
109500K .......... .......... .......... .......... .......... 21% 16.3M 31s
109550K .......... .......... .......... .......... .......... 21% 15.2M 31s
109600K .......... .......... .......... .......... .......... 21% 11.7M 31s
109650K .......... .......... .......... .......... .......... 21% 15.0M 31s
109700K .......... .......... .......... .......... .......... 21% 12.6M 31s
109750K .......... .......... .......... .......... .......... 21% 18.3M 31s
109800K .......... .......... .......... .......... .......... 21% 12.9M 31s
109850K .......... .......... .......... .......... .......... 21% 13.7M 31s
109900K .......... .......... .......... .......... .......... 21% 12.2M 31s
109950K .......... .......... .......... .......... .......... 21% 8.04M 31s
110000K .......... .......... .......... .......... .......... 21% 15.5M 31s
110050K .......... .......... .......... .......... .......... 21% 9.69M 31s
110100K .......... .......... .......... .......... .......... 21% 6.72M 31s
110150K .......... .......... .......... .......... .......... 21% 6.81M 31s
110200K .......... .......... .......... .......... .......... 21% 4.65M 31s
110250K .......... .......... .......... .......... .......... 21% 5.73M 31s
110300K .......... .......... .......... .......... .......... 21% 12.9M 31s
110350K .......... .......... .......... .......... .......... 21% 25.1M 31s
110400K .......... .......... .......... .......... .......... 21% 20.0M 31s
110450K .......... .......... .......... .......... .......... 21% 17.1M 31s
110500K .......... .......... .......... .......... .......... 21% 26.6M 31s
110550K .......... .......... .......... .......... .......... 21% 13.5M 31s
110600K .......... .......... .......... .......... .......... 21% 7.99M 31s
110650K .......... .......... .......... .......... .......... 21% 6.19M 31s
110700K .......... .......... .......... .......... .......... 21% 5.72M 31s
110750K .......... .......... .......... .......... .......... 22% 6.80M 31s
110800K .......... .......... .......... .......... .......... 22% 6.64M 31s
110850K .......... .......... .......... .......... .......... 22% 5.34M 31s
110900K .......... .......... .......... .......... .......... 22% 9.48M 31s
110950K .......... .......... .......... .......... .......... 22% 6.34M 31s
111000K .......... .......... .......... .......... .......... 22% 12.2M 31s
111050K .......... .......... .......... .......... .......... 22% 7.26M 31s
111100K .......... .......... .......... .......... .......... 22% 6.30M 31s
111150K .......... .......... .......... .......... .......... 22% 6.90M 31s
111200K .......... .......... .......... .......... .......... 22% 5.37M 31s
111250K .......... .......... .......... .......... .......... 22% 7.62M 31s
111300K .......... .......... .......... .......... .......... 22% 12.7M 31s
111350K .......... .......... .......... .......... .......... 22% 31.3M 31s
111400K .......... .......... .......... .......... .......... 22% 14.8M 31s
111450K .......... .......... .......... .......... .......... 22% 13.8M 31s
111500K .......... .......... .......... .......... .......... 22% 11.4M 31s
111550K .......... .......... .......... .......... .......... 22% 13.0M 31s
111600K .......... .......... .......... .......... .......... 22% 8.03M 31s
111650K .......... .......... .......... .......... .......... 22% 12.9M 31s
111700K .......... .......... .......... .......... .......... 22% 9.71M 31s
111750K .......... .......... .......... .......... .......... 22% 11.2M 31s
111800K .......... .......... .......... .......... .......... 22% 10.6M 31s
111850K .......... .......... .......... .......... .......... 22% 10.1M 31s
111900K .......... .......... .......... .......... .......... 22% 10.0M 31s
111950K .......... .......... .......... .......... .......... 22% 10.5M 31s
112000K .......... .......... .......... .......... .......... 22% 24.3M 31s
112050K .......... .......... .......... .......... .......... 22% 27.5M 31s
112100K .......... .......... .......... .......... .......... 22% 28.7M 31s
112150K .......... .......... .......... .......... .......... 22% 37.6M 31s
112200K .......... .......... .......... .......... .......... 22% 27.2M 31s
112250K .......... .......... .......... .......... .......... 22% 72.7M 31s
112300K .......... .......... .......... .......... .......... 22% 33.9M 31s
112350K .......... .......... .......... .......... .......... 22% 17.0M 31s
112400K .......... .......... .......... .......... .......... 22% 24.9M 31s
112450K .......... .......... .......... .......... .......... 22% 17.8M 31s
112500K .......... .......... .......... .......... .......... 22% 13.1M 31s
112550K .......... .......... .......... .......... .......... 22% 11.2M 31s
112600K .......... .......... .......... .......... .......... 22% 9.91M 31s
112650K .......... .......... .......... .......... .......... 22% 10.3M 31s
112700K .......... .......... .......... .......... .......... 22% 7.46M 31s
112750K .......... .......... .......... .......... .......... 22% 10.5M 31s
112800K .......... .......... .......... .......... .......... 22% 9.29M 31s
112850K .......... .......... .......... .......... .......... 22% 7.97M 31s
112900K .......... .......... .......... .......... .......... 22% 24.8M 31s
112950K .......... .......... .......... .......... .......... 22% 10.7M 31s
113000K .......... .......... .......... .......... .......... 22% 14.5M 31s
113050K .......... .......... .......... .......... .......... 22% 14.4M 31s
113100K .......... .......... .......... .......... .......... 22% 9.01M 31s
113150K .......... .......... .......... .......... .......... 22% 12.7M 31s
113200K .......... .......... .......... .......... .......... 22% 8.91M 31s
113250K .......... .......... .......... .......... .......... 22% 14.4M 31s
113300K .......... .......... .......... .......... .......... 22% 9.13M 31s
113350K .......... .......... .......... .......... .......... 22% 6.84M 31s
113400K .......... .......... .......... .......... .......... 22% 11.3M 31s
113450K .......... .......... .......... .......... .......... 22% 8.75M 31s
113500K .......... .......... .......... .......... .......... 22% 9.36M 31s
113550K .......... .......... .......... .......... .......... 22% 6.40M 31s
113600K .......... .......... .......... .......... .......... 22% 8.03M 31s
113650K .......... .......... .......... .......... .......... 22% 7.32M 31s
113700K .......... .......... .......... .......... .......... 22% 7.31M 31s
113750K .......... .......... .......... .......... .......... 22% 6.66M 31s
113800K .......... .......... .......... .......... .......... 22% 7.65M 31s
113850K .......... .......... .......... .......... .......... 22% 9.35M 31s
113900K .......... .......... .......... .......... .......... 22% 31.8M 31s
113950K .......... .......... .......... .......... .......... 22% 17.4M 31s
114000K .......... .......... .......... .......... .......... 22% 19.7M 31s
114050K .......... .......... .......... .......... .......... 22% 34.0M 31s
114100K .......... .......... .......... .......... .......... 22% 23.6M 31s
114150K .......... .......... .......... .......... .......... 22% 22.7M 31s
114200K .......... .......... .......... .......... .......... 22% 16.5M 31s
114250K .......... .......... .......... .......... .......... 22% 22.1M 31s
114300K .......... .......... .......... .......... .......... 22% 23.3M 31s
114350K .......... .......... .......... .......... .......... 22% 20.2M 31s
114400K .......... .......... .......... .......... .......... 22% 22.0M 31s
114450K .......... .......... .......... .......... .......... 22% 15.7M 31s
114500K .......... .......... .......... .......... .......... 22% 19.8M 31s
114550K .......... .......... .......... .......... .......... 22% 17.9M 31s
114600K .......... .......... .......... .......... .......... 22% 16.5M 31s
114650K .......... .......... .......... .......... .......... 22% 11.0M 31s
114700K .......... .......... .......... .......... .......... 22% 30.2M 31s
114750K .......... .......... .......... .......... .......... 22% 12.3M 31s
114800K .......... .......... .......... .......... .......... 22% 20.9M 31s
114850K .......... .......... .......... .......... .......... 22% 12.1M 31s
114900K .......... .......... .......... .......... .......... 22% 15.0M 31s
114950K .......... .......... .......... .......... .......... 22% 8.93M 31s
115000K .......... .......... .......... .......... .......... 22% 8.76M 31s
115050K .......... .......... .......... .......... .......... 22% 7.29M 31s
115100K .......... .......... .......... .......... .......... 22% 8.19M 31s
115150K .......... .......... .......... .......... .......... 22% 9.43M 31s
115200K .......... .......... .......... .......... .......... 22% 9.01M 31s
115250K .......... .......... .......... .......... .......... 22% 7.56M 31s
115300K .......... .......... .......... .......... .......... 22% 8.77M 31s
115350K .......... .......... .......... .......... .......... 22% 9.97M 31s
115400K .......... .......... .......... .......... .......... 22% 8.17M 31s
115450K .......... .......... .......... .......... .......... 22% 9.92M 31s
115500K .......... .......... .......... .......... .......... 22% 10.2M 31s
115550K .......... .......... .......... .......... .......... 22% 12.2M 31s
115600K .......... .......... .......... .......... .......... 22% 8.63M 31s
115650K .......... .......... .......... .......... .......... 22% 11.4M 31s
115700K .......... .......... .......... .......... .......... 22% 8.61M 31s
115750K .......... .......... .......... .......... .......... 22% 11.6M 31s
115800K .......... .......... .......... .......... .......... 23% 10.1M 31s
115850K .......... .......... .......... .......... .......... 23% 4.53M 31s
115900K .......... .......... .......... .......... .......... 23% 7.85M 31s
115950K .......... .......... .......... .......... .......... 23% 9.33M 31s
116000K .......... .......... .......... .......... .......... 23% 15.6M 31s
116050K .......... .......... .......... .......... .......... 23% 11.7M 31s
116100K .......... .......... .......... .......... .......... 23% 9.85M 31s
116150K .......... .......... .......... .......... .......... 23% 14.5M 31s
116200K .......... .......... .......... .......... .......... 23% 7.85M 31s
116250K .......... .......... .......... .......... .......... 23% 12.9M 31s
116300K .......... .......... .......... .......... .......... 23% 7.88M 31s
116350K .......... .......... .......... .......... .......... 23% 6.74M 31s
116400K .......... .......... .......... .......... .......... 23% 12.9M 31s
116450K .......... .......... .......... .......... .......... 23% 12.4M 31s
116500K .......... .......... .......... .......... .......... 23% 11.1M 31s
116550K .......... .......... .......... .......... .......... 23% 11.8M 31s
116600K .......... .......... .......... .......... .......... 23% 9.64M 31s
116650K .......... .......... .......... .......... .......... 23% 9.43M 31s
116700K .......... .......... .......... .......... .......... 23% 9.16M 31s
116750K .......... .......... .......... .......... .......... 23% 19.0M 31s
116800K .......... .......... .......... .......... .......... 23% 7.82M 31s
116850K .......... .......... .......... .......... .......... 23% 10.2M 31s
116900K .......... .......... .......... .......... .......... 23% 10.4M 31s
116950K .......... .......... .......... .......... .......... 23% 9.94M 31s
117000K .......... .......... .......... .......... .......... 23% 9.04M 31s
117050K .......... .......... .......... .......... .......... 23% 8.79M 31s
117100K .......... .......... .......... .......... .......... 23% 7.05M 31s
117150K .......... .......... .......... .......... .......... 23% 8.39M 31s
117200K .......... .......... .......... .......... .......... 23% 23.6M 31s
117250K .......... .......... .......... .......... .......... 23% 18.6M 31s
117300K .......... .......... .......... .......... .......... 23% 14.4M 31s
117350K .......... .......... .......... .......... .......... 23% 9.89M 31s
117400K .......... .......... .......... .......... .......... 23% 6.98M 31s
117450K .......... .......... .......... .......... .......... 23% 6.86M 31s
117500K .......... .......... .......... .......... .......... 23% 9.41M 31s
117550K .......... .......... .......... .......... .......... 23% 11.1M 31s
117600K .......... .......... .......... .......... .......... 23% 7.27M 31s
117650K .......... .......... .......... .......... .......... 23% 10.1M 31s
117700K .......... .......... .......... .......... .......... 23% 7.53M 31s
117750K .......... .......... .......... .......... .......... 23% 9.99M 31s
117800K .......... .......... .......... .......... .......... 23% 28.7M 31s
117850K .......... .......... .......... .......... .......... 23% 19.3M 31s
117900K .......... .......... .......... .......... .......... 23% 14.4M 31s
117950K .......... .......... .......... .......... .......... 23% 20.4M 31s
118000K .......... .......... .......... .......... .......... 23% 9.02M 31s
118050K .......... .......... .......... .......... .......... 23% 6.78M 31s
118100K .......... .......... .......... .......... .......... 23% 5.38M 31s
118150K .......... .......... .......... .......... .......... 23% 5.66M 31s
118200K .......... .......... .......... .......... .......... 23% 4.85M 31s
118250K .......... .......... .......... .......... .......... 23% 5.76M 31s
118300K .......... .......... .......... .......... .......... 23% 5.26M 31s
118350K .......... .......... .......... .......... .......... 23% 7.14M 31s
118400K .......... .......... .......... .......... .......... 23% 12.2M 31s
118450K .......... .......... .......... .......... .......... 23% 6.07M 31s
118500K .......... .......... .......... .......... .......... 23% 9.93M 31s
118550K .......... .......... .......... .......... .......... 23% 7.57M 31s
118600K .......... .......... .......... .......... .......... 23% 6.47M 31s
118650K .......... .......... .......... .......... .......... 23% 6.81M 31s
118700K .......... .......... .......... .......... .......... 23% 5.90M 31s
118750K .......... .......... .......... .......... .......... 23% 9.97M 31s
118800K .......... .......... .......... .......... .......... 23% 15.2M 31s
118850K .......... .......... .......... .......... .......... 23% 7.66M 31s
118900K .......... .......... .......... .......... .......... 23% 10.8M 31s
118950K .......... .......... .......... .......... .......... 23% 4.98M 31s
119000K .......... .......... .......... .......... .......... 23% 11.8M 31s
119050K .......... .......... .......... .......... .......... 23% 8.99M 31s
119100K .......... .......... .......... .......... .......... 23% 5.80M 31s
119150K .......... .......... .......... .......... .......... 23% 9.93M 31s
119200K .......... .......... .......... .......... .......... 23% 5.99M 31s
119250K .......... .......... .......... .......... .......... 23% 5.27M 31s
119300K .......... .......... .......... .......... .......... 23% 6.85M 31s
119350K .......... .......... .......... .......... .......... 23% 5.00M 31s
119400K .......... .......... .......... .......... .......... 23% 6.13M 31s
119450K .......... .......... .......... .......... .......... 23% 6.70M 31s
119500K .......... .......... .......... .......... .......... 23% 9.09M 31s
119550K .......... .......... .......... .......... .......... 23% 8.63M 31s
119600K .......... .......... .......... .......... .......... 23% 8.57M 31s
119650K .......... .......... .......... .......... .......... 23% 9.30M 31s
119700K .......... .......... .......... .......... .......... 23% 8.59M 31s
119750K .......... .......... .......... .......... .......... 23% 10.8M 31s
119800K .......... .......... .......... .......... .......... 23% 10.3M 31s
119850K .......... .......... .......... .......... .......... 23% 16.4M 31s
119900K .......... .......... .......... .......... .......... 23% 19.7M 31s
119950K .......... .......... .......... .......... .......... 23% 23.4M 31s
120000K .......... .......... .......... .......... .......... 23% 24.2M 31s
120050K .......... .......... .......... .......... .......... 23% 20.4M 31s
120100K .......... .......... .......... .......... .......... 23% 20.9M 31s
120150K .......... .......... .......... .......... .......... 23% 14.7M 31s
120200K .......... .......... .......... .......... .......... 23% 17.3M 31s
120250K .......... .......... .......... .......... .......... 23% 20.0M 31s
120300K .......... .......... .......... .......... .......... 23% 14.2M 31s
120350K .......... .......... .......... .......... .......... 23% 11.0M 31s
120400K .......... .......... .......... .......... .......... 23% 8.59M 31s
120450K .......... .......... .......... .......... .......... 23% 7.34M 31s
120500K .......... .......... .......... .......... .......... 23% 9.43M 31s
120550K .......... .......... .......... .......... .......... 23% 7.75M 31s
120600K .......... .......... .......... .......... .......... 23% 7.00M 31s
120650K .......... .......... .......... .......... .......... 23% 8.75M 31s
120700K .......... .......... .......... .......... .......... 23% 6.18M 31s
120750K .......... .......... .......... .......... .......... 23% 7.12M 31s
120800K .......... .......... .......... .......... .......... 23% 8.40M 31s
120850K .......... .......... .......... .......... .......... 24% 15.6M 31s
120900K .......... .......... .......... .......... .......... 24% 9.15M 31s
120950K .......... .......... .......... .......... .......... 24% 9.36M 31s
121000K .......... .......... .......... .......... .......... 24% 8.99M 31s
121050K .......... .......... .......... .......... .......... 24% 8.40M 31s
121100K .......... .......... .......... .......... .......... 24% 5.80M 31s
121150K .......... .......... .......... .......... .......... 24% 2.87M 31s
121200K .......... .......... .......... .......... .......... 24% 2.15M 31s
121250K .......... .......... .......... .......... .......... 24% 3.04M 31s
121300K .......... .......... .......... .......... .......... 24% 3.97M 31s
121350K .......... .......... .......... .......... .......... 24% 16.6M 31s
121400K .......... .......... .......... .......... .......... 24% 22.9M 31s
121450K .......... .......... .......... .......... .......... 24% 56.9M 31s
121500K .......... .......... .......... .......... .......... 24% 46.0M 31s
121550K .......... .......... .......... .......... .......... 24% 19.9M 31s
121600K .......... .......... .......... .......... .......... 24% 13.7M 31s
121650K .......... .......... .......... .......... .......... 24% 14.4M 31s
121700K .......... .......... .......... .......... .......... 24% 13.6M 31s
121750K .......... .......... .......... .......... .......... 24% 9.73M 31s
121800K .......... .......... .......... .......... .......... 24% 12.7M 31s
121850K .......... .......... .......... .......... .......... 24% 8.81M 31s
121900K .......... .......... .......... .......... .......... 24% 7.88M 31s
121950K .......... .......... .......... .......... .......... 24% 5.97M 31s
122000K .......... .......... .......... .......... .......... 24% 5.91M 31s
122050K .......... .......... .......... .......... .......... 24% 7.79M 31s
122100K .......... .......... .......... .......... .......... 24% 8.59M 31s
122150K .......... .......... .......... .......... .......... 24% 9.22M 31s
122200K .......... .......... .......... .......... .......... 24% 8.56M 31s
122250K .......... .......... .......... .......... .......... 24% 7.90M 31s
122300K .......... .......... .......... .......... .......... 24% 9.72M 31s
122350K .......... .......... .......... .......... .......... 24% 5.58M 31s
122400K .......... .......... .......... .......... .......... 24% 9.70M 31s
122450K .......... .......... .......... .......... .......... 24% 6.06M 31s
122500K .......... .......... .......... .......... .......... 24% 6.55M 31s
122550K .......... .......... .......... .......... .......... 24% 7.20M 31s
122600K .......... .......... .......... .......... .......... 24% 6.25M 31s
122650K .......... .......... .......... .......... .......... 24% 10.2M 31s
122700K .......... .......... .......... .......... .......... 24% 7.73M 31s
122750K .......... .......... .......... .......... .......... 24% 10.1M 31s
122800K .......... .......... .......... .......... .......... 24% 8.60M 31s
122850K .......... .......... .......... .......... .......... 24% 5.36M 31s
122900K .......... .......... .......... .......... .......... 24% 6.55M 31s
122950K .......... .......... .......... .......... .......... 24% 7.23M 31s
123000K .......... .......... .......... .......... .......... 24% 7.71M 31s
123050K .......... .......... .......... .......... .......... 24% 7.89M 31s
123100K .......... .......... .......... .......... .......... 24% 6.96M 31s
123150K .......... .......... .......... .......... .......... 24% 6.64M 31s
123200K .......... .......... .......... .......... .......... 24% 5.21M 31s
123250K .......... .......... .......... .......... .......... 24% 5.55M 31s
123300K .......... .......... .......... .......... .......... 24% 7.84M 31s
123350K .......... .......... .......... .......... .......... 24% 17.1M 31s
123400K .......... .......... .......... .......... .......... 24% 18.0M 31s
123450K .......... .......... .......... .......... .......... 24% 16.2M 31s
123500K .......... .......... .......... .......... .......... 24% 20.8M 31s
123550K .......... .......... .......... .......... .......... 24% 12.2M 31s
123600K .......... .......... .......... .......... .......... 24% 10.4M 31s
123650K .......... .......... .......... .......... .......... 24% 12.1M 31s
123700K .......... .......... .......... .......... .......... 24% 8.23M 31s
123750K .......... .......... .......... .......... .......... 24% 12.3M 31s
123800K .......... .......... .......... .......... .......... 24% 8.63M 31s
123850K .......... .......... .......... .......... .......... 24% 6.04M 31s
123900K .......... .......... .......... .......... .......... 24% 5.10M 31s
123950K .......... .......... .......... .......... .......... 24% 5.24M 31s
124000K .......... .......... .......... .......... .......... 24% 5.57M 31s
124050K .......... .......... .......... .......... .......... 24% 4.48M 31s
124100K .......... .......... .......... .......... .......... 24% 3.27M 31s
124150K .......... .......... .......... .......... .......... 24% 3.44M 31s
124200K .......... .......... .......... .......... .......... 24% 7.35M 31s
124250K .......... .......... .......... .......... .......... 24% 17.8M 31s
124300K .......... .......... .......... .......... .......... 24% 27.1M 31s
124350K .......... .......... .......... .......... .......... 24% 30.2M 31s
124400K .......... .......... .......... .......... .......... 24% 27.4M 31s
124450K .......... .......... .......... .......... .......... 24% 32.7M 31s
124500K .......... .......... .......... .......... .......... 24% 31.9M 31s
124550K .......... .......... .......... .......... .......... 24% 19.5M 31s
124600K .......... .......... .......... .......... .......... 24% 15.8M 31s
124650K .......... .......... .......... .......... .......... 24% 16.9M 31s
124700K .......... .......... .......... .......... .......... 24% 10.8M 31s
124750K .......... .......... .......... .......... .......... 24% 18.7M 31s
124800K .......... .......... .......... .......... .......... 24% 10.1M 31s
124850K .......... .......... .......... .......... .......... 24% 8.18M 31s
124900K .......... .......... .......... .......... .......... 24% 8.97M 31s
124950K .......... .......... .......... .......... .......... 24% 6.81M 31s
125000K .......... .......... .......... .......... .......... 24% 7.57M 31s
125050K .......... .......... .......... .......... .......... 24% 7.60M 31s
125100K .......... .......... .......... .......... .......... 24% 8.69M 31s
125150K .......... .......... .......... .......... .......... 24% 13.8M 31s
125200K .......... .......... .......... .......... .......... 24% 10.4M 31s
125250K .......... .......... .......... .......... .......... 24% 11.4M 31s
125300K .......... .......... .......... .......... .......... 24% 25.6M 31s
125350K .......... .......... .......... .......... .......... 24% 19.6M 31s
125400K .......... .......... .......... .......... .......... 24% 24.9M 31s
125450K .......... .......... .......... .......... .......... 24% 16.2M 31s
125500K .......... .......... .......... .......... .......... 24% 21.1M 31s
125550K .......... .......... .......... .......... .......... 24% 14.1M 31s
125600K .......... .......... .......... .......... .......... 24% 18.4M 31s
125650K .......... .......... .......... .......... .......... 24% 17.9M 31s
125700K .......... .......... .......... .......... .......... 24% 12.6M 31s
125750K .......... .......... .......... .......... .......... 24% 16.2M 31s
125800K .......... .......... .......... .......... .......... 24% 15.0M 31s
125850K .......... .......... .......... .......... .......... 24% 12.6M 31s
125900K .......... .......... .......... .......... .......... 25% 12.1M 31s
125950K .......... .......... .......... .......... .......... 25% 10.2M 31s
126000K .......... .......... .......... .......... .......... 25% 9.47M 31s
126050K .......... .......... .......... .......... .......... 25% 6.85M 31s
126100K .......... .......... .......... .......... .......... 25% 8.04M 31s
126150K .......... .......... .......... .......... .......... 25% 7.35M 31s
126200K .......... .......... .......... .......... .......... 25% 6.92M 31s
126250K .......... .......... .......... .......... .......... 25% 7.58M 31s
126300K .......... .......... .......... .......... .......... 25% 8.44M 31s
126350K .......... .......... .......... .......... .......... 25% 7.43M 31s
126400K .......... .......... .......... .......... .......... 25% 6.51M 31s
126450K .......... .......... .......... .......... .......... 25% 5.42M 31s
126500K .......... .......... .......... .......... .......... 25% 6.43M 31s
126550K .......... .......... .......... .......... .......... 25% 6.04M 31s
126600K .......... .......... .......... .......... .......... 25% 5.28M 31s
126650K .......... .......... .......... .......... .......... 25% 7.07M 31s
126700K .......... .......... .......... .......... .......... 25% 8.13M 31s
126750K .......... .......... .......... .......... .......... 25% 8.58M 31s
126800K .......... .......... .......... .......... .......... 25% 7.42M 31s
126850K .......... .......... .......... .......... .......... 25% 6.63M 31s
126900K .......... .......... .......... .......... .......... 25% 4.26M 31s
126950K .......... .......... .......... .......... .......... 25% 3.32M 31s
127000K .......... .......... .......... .......... .......... 25% 3.16M 31s
127050K .......... .......... .......... .......... .......... 25% 7.82M 31s
127100K .......... .......... .......... .......... .......... 25% 12.5M 31s
127150K .......... .......... .......... .......... .......... 25% 38.9M 31s
127200K .......... .......... .......... .......... .......... 25% 21.6M 31s
127250K .......... .......... .......... .......... .......... 25% 15.7M 31s
127300K .......... .......... .......... .......... .......... 25% 14.3M 31s
127350K .......... .......... .......... .......... .......... 25% 10.2M 31s
127400K .......... .......... .......... .......... .......... 25% 13.5M 31s
127450K .......... .......... .......... .......... .......... 25% 9.69M 31s
127500K .......... .......... .......... .......... .......... 25% 10.8M 31s
127550K .......... .......... .......... .......... .......... 25% 11.7M 31s
127600K .......... .......... .......... .......... .......... 25% 9.68M 31s
127650K .......... .......... .......... .......... .......... 25% 11.8M 31s
127700K .......... .......... .......... .......... .......... 25% 12.3M 31s
127750K .......... .......... .......... .......... .......... 25% 28.8M 31s
127800K .......... .......... .......... .......... .......... 25% 32.1M 31s
127850K .......... .......... .......... .......... .......... 25% 29.0M 31s
127900K .......... .......... .......... .......... .......... 25% 33.9M 31s
127950K .......... .......... .......... .......... .......... 25% 35.1M 31s
128000K .......... .......... .......... .......... .......... 25% 21.9M 31s
128050K .......... .......... .......... .......... .......... 25% 77.9M 31s
128100K .......... .......... .......... .......... .......... 25% 22.9M 31s
128150K .......... .......... .......... .......... .......... 25% 46.1M 31s
128200K .......... .......... .......... .......... .......... 25% 14.6M 31s
128250K .......... .......... .......... .......... .......... 25% 23.3M 31s
128300K .......... .......... .......... .......... .......... 25% 9.69M 31s
128350K .......... .......... .......... .......... .......... 25% 9.16M 31s
128400K .......... .......... .......... .......... .......... 25% 8.98M 31s
128450K .......... .......... .......... .......... .......... 25% 8.10M 31s
128500K .......... .......... .......... .......... .......... 25% 7.74M 31s
128550K .......... .......... .......... .......... .......... 25% 7.23M 31s
128600K .......... .......... .......... .......... .......... 25% 3.75M 31s
128650K .......... .......... .......... .......... .......... 25% 11.6M 31s
128700K .......... .......... .......... .......... .......... 25% 6.23M 31s
128750K .......... .......... .......... .......... .......... 25% 19.7M 31s
128800K .......... .......... .......... .......... .......... 25% 12.1M 31s
128850K .......... .......... .......... .......... .......... 25% 11.5M 31s
128900K .......... .......... .......... .......... .......... 25% 22.0M 31s
128950K .......... .......... .......... .......... .......... 25% 13.9M 31s
129000K .......... .......... .......... .......... .......... 25% 17.2M 31s
129050K .......... .......... .......... .......... .......... 25% 13.0M 31s
129100K .......... .......... .......... .......... .......... 25% 15.5M 31s
129150K .......... .......... .......... .......... .......... 25% 13.3M 31s
129200K .......... .......... .......... .......... .......... 25% 18.7M 31s
129250K .......... .......... .......... .......... .......... 25% 16.3M 31s
129300K .......... .......... .......... .......... .......... 25% 12.6M 31s
129350K .......... .......... .......... .......... .......... 25% 11.1M 31s
129400K .......... .......... .......... .......... .......... 25% 27.1M 31s
129450K .......... .......... .......... .......... .......... 25% 9.46M 31s
129500K .......... .......... .......... .......... .......... 25% 9.03M 31s
129550K .......... .......... .......... .......... .......... 25% 12.7M 31s
129600K .......... .......... .......... .......... .......... 25% 9.70M 31s
129650K .......... .......... .......... .......... .......... 25% 11.6M 31s
129700K .......... .......... .......... .......... .......... 25% 6.11M 31s
129750K .......... .......... .......... .......... .......... 25% 13.0M 31s
129800K .......... .......... .......... .......... .......... 25% 9.28M 31s
129850K .......... .......... .......... .......... .......... 25% 9.97M 31s
129900K .......... .......... .......... .......... .......... 25% 11.9M 31s
129950K .......... .......... .......... .......... .......... 25% 10.3M 31s
130000K .......... .......... .......... .......... .......... 25% 10.3M 31s
130050K .......... .......... .......... .......... .......... 25% 11.5M 31s
130100K .......... .......... .......... .......... .......... 25% 9.51M 31s
130150K .......... .......... .......... .......... .......... 25% 11.1M 31s
130200K .......... .......... .......... .......... .......... 25% 8.66M 31s
130250K .......... .......... .......... .......... .......... 25% 10.8M 31s
130300K .......... .......... .......... .......... .......... 25% 9.50M 31s
130350K .......... .......... .......... .......... .......... 25% 8.10M 31s
130400K .......... .......... .......... .......... .......... 25% 6.94M 31s
130450K .......... .......... .......... .......... .......... 25% 7.34M 31s
130500K .......... .......... .......... .......... .......... 25% 14.2M 31s
130550K .......... .......... .......... .......... .......... 25% 18.7M 31s
130600K .......... .......... .......... .......... .......... 25% 23.6M 31s
130650K .......... .......... .......... .......... .......... 25% 16.3M 31s
130700K .......... .......... .......... .......... .......... 25% 13.1M 31s
130750K .......... .......... .......... .......... .......... 25% 13.0M 31s
130800K .......... .......... .......... .......... .......... 25% 11.5M 31s
130850K .......... .......... .......... .......... .......... 25% 9.95M 31s
130900K .......... .......... .......... .......... .......... 26% 12.1M 31s
130950K .......... .......... .......... .......... .......... 26% 9.22M 31s
131000K .......... .......... .......... .......... .......... 26% 8.33M 31s
131050K .......... .......... .......... .......... .......... 26% 8.86M 31s
131100K .......... .......... .......... .......... .......... 26% 7.97M 31s
131150K .......... .......... .......... .......... .......... 26% 9.87M 31s
131200K .......... .......... .......... .......... .......... 26% 14.5M 31s
131250K .......... .......... .......... .......... .......... 26% 13.0M 31s
131300K .......... .......... .......... .......... .......... 26% 9.69M 31s
131350K .......... .......... .......... .......... .......... 26% 11.7M 31s
131400K .......... .......... .......... .......... .......... 26% 12.2M 31s
131450K .......... .......... .......... .......... .......... 26% 9.66M 31s
131500K .......... .......... .......... .......... .......... 26% 12.3M 31s
131550K .......... .......... .......... .......... .......... 26% 11.1M 31s
131600K .......... .......... .......... .......... .......... 26% 20.9M 31s
131650K .......... .......... .......... .......... .......... 26% 13.3M 31s
131700K .......... .......... .......... .......... .......... 26% 15.9M 31s
131750K .......... .......... .......... .......... .......... 26% 16.0M 31s
131800K .......... .......... .......... .......... .......... 26% 13.9M 31s
131850K .......... .......... .......... .......... .......... 26% 12.2M 31s
131900K .......... .......... .......... .......... .......... 26% 12.9M 31s
131950K .......... .......... .......... .......... .......... 26% 8.02M 31s
132000K .......... .......... .......... .......... .......... 26% 11.9M 31s
132050K .......... .......... .......... .......... .......... 26% 9.40M 31s
132100K .......... .......... .......... .......... .......... 26% 5.81M 31s
132150K .......... .......... .......... .......... .......... 26% 5.95M 31s
132200K .......... .......... .......... .......... .......... 26% 6.07M 31s
132250K .......... .......... .......... .......... .......... 26% 10.7M 31s
132300K .......... .......... .......... .......... .......... 26% 8.40M 31s
132350K .......... .......... .......... .......... .......... 26% 7.64M 31s
132400K .......... .......... .......... .......... .......... 26% 8.16M 31s
132450K .......... .......... .......... .......... .......... 26% 8.34M 31s
132500K .......... .......... .......... .......... .......... 26% 9.01M 31s
132550K .......... .......... .......... .......... .......... 26% 15.1M 31s
132600K .......... .......... .......... .......... .......... 26% 16.5M 31s
132650K .......... .......... .......... .......... .......... 26% 9.22M 31s
132700K .......... .......... .......... .......... .......... 26% 8.76M 31s
132750K .......... .......... .......... .......... .......... 26% 5.50M 31s
132800K .......... .......... .......... .......... .......... 26% 4.31M 31s
132850K .......... .......... .......... .......... .......... 26% 12.9M 31s
132900K .......... .......... .......... .......... .......... 26% 15.1M 31s
132950K .......... .......... .......... .......... .......... 26% 8.46M 31s
133000K .......... .......... .......... .......... .......... 26% 13.5M 31s
133050K .......... .......... .......... .......... .......... 26% 14.1M 31s
133100K .......... .......... .......... .......... .......... 26% 12.8M 31s
133150K .......... .......... .......... .......... .......... 26% 13.8M 31s
133200K .......... .......... .......... .......... .......... 26% 11.7M 31s
133250K .......... .......... .......... .......... .......... 26% 11.1M 31s
133300K .......... .......... .......... .......... .......... 26% 22.7M 31s
133350K .......... .......... .......... .......... .......... 26% 15.9M 31s
133400K .......... .......... .......... .......... .......... 26% 23.7M 31s
133450K .......... .......... .......... .......... .......... 26% 8.77M 31s
133500K .......... .......... .......... .......... .......... 26% 9.62M 31s
133550K .......... .......... .......... .......... .......... 26% 11.9M 31s
133600K .......... .......... .......... .......... .......... 26% 9.85M 31s
133650K .......... .......... .......... .......... .......... 26% 9.71M 31s
133700K .......... .......... .......... .......... .......... 26% 7.69M 31s
133750K .......... .......... .......... .......... .......... 26% 10.6M 31s
133800K .......... .......... .......... .......... .......... 26% 8.20M 31s
133850K .......... .......... .......... .......... .......... 26% 7.12M 31s
133900K .......... .......... .......... .......... .......... 26% 7.93M 31s
133950K .......... .......... .......... .......... .......... 26% 9.52M 31s
134000K .......... .......... .......... .......... .......... 26% 19.8M 31s
134050K .......... .......... .......... .......... .......... 26% 27.7M 31s
134100K .......... .......... .......... .......... .......... 26% 24.6M 31s
134150K .......... .......... .......... .......... .......... 26% 20.0M 31s
134200K .......... .......... .......... .......... .......... 26% 20.2M 31s
134250K .......... .......... .......... .......... .......... 26% 19.9M 31s
134300K .......... .......... .......... .......... .......... 26% 29.8M 31s
134350K .......... .......... .......... .......... .......... 26% 18.0M 31s
134400K .......... .......... .......... .......... .......... 26% 13.3M 31s
134450K .......... .......... .......... .......... .......... 26% 15.7M 31s
134500K .......... .......... .......... .......... .......... 26% 15.7M 31s
134550K .......... .......... .......... .......... .......... 26% 17.2M 31s
134600K .......... .......... .......... .......... .......... 26% 13.8M 31s
134650K .......... .......... .......... .......... .......... 26% 14.5M 31s
134700K .......... .......... .......... .......... .......... 26% 11.0M 31s
134750K .......... .......... .......... .......... .......... 26% 15.1M 31s
134800K .......... .......... .......... .......... .......... 26% 12.1M 31s
134850K .......... .......... .......... .......... .......... 26% 11.4M 31s
134900K .......... .......... .......... .......... .......... 26% 14.5M 31s
134950K .......... .......... .......... .......... .......... 26% 11.4M 31s
135000K .......... .......... .......... .......... .......... 26% 13.5M 31s
135050K .......... .......... .......... .......... .......... 26% 11.4M 31s
135100K .......... .......... .......... .......... .......... 26% 16.5M 31s
135150K .......... .......... .......... .......... .......... 26% 31.0M 31s
135200K .......... .......... .......... .......... .......... 26% 27.7M 31s
135250K .......... .......... .......... .......... .......... 26% 36.8M 30s
135300K .......... .......... .......... .......... .......... 26% 40.4M 30s
135350K .......... .......... .......... .......... .......... 26% 26.9M 30s
135400K .......... .......... .......... .......... .......... 26% 41.8M 30s
135450K .......... .......... .......... .......... .......... 26% 28.0M 30s
135500K .......... .......... .......... .......... .......... 26% 37.4M 30s
135550K .......... .......... .......... .......... .......... 26% 22.3M 30s
135600K .......... .......... .......... .......... .......... 26% 46.8M 30s
135650K .......... .......... .......... .......... .......... 26% 24.8M 30s
135700K .......... .......... .......... .......... .......... 26% 30.9M 30s
135750K .......... .......... .......... .......... .......... 26% 24.2M 30s
135800K .......... .......... .......... .......... .......... 26% 24.1M 30s
135850K .......... .......... .......... .......... .......... 26% 15.3M 30s
135900K .......... .......... .......... .......... .......... 26% 17.4M 30s
135950K .......... .......... .......... .......... .......... 27% 13.9M 30s
136000K .......... .......... .......... .......... .......... 27% 12.5M 30s
136050K .......... .......... .......... .......... .......... 27% 15.1M 30s
136100K .......... .......... .......... .......... .......... 27% 13.4M 30s
136150K .......... .......... .......... .......... .......... 27% 14.4M 30s
136200K .......... .......... .......... .......... .......... 27% 11.0M 30s
136250K .......... .......... .......... .......... .......... 27% 9.62M 30s
136300K .......... .......... .......... .......... .......... 27% 10.2M 30s
136350K .......... .......... .......... .......... .......... 27% 8.18M 30s
136400K .......... .......... .......... .......... .......... 27% 9.40M 30s
136450K .......... .......... .......... .......... .......... 27% 8.75M 30s
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149250K .......... .......... .......... .......... .......... 29% 25.1M 29s
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150000K .......... .......... .......... .......... .......... 29% 11.5M 29s
150050K .......... .......... .......... .......... .......... 29% 9.84M 29s
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150200K .......... .......... .......... .......... .......... 29% 9.62M 29s
150250K .......... .......... .......... .......... .......... 29% 9.00M 29s
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150400K .......... .......... .......... .......... .......... 29% 11.7M 29s
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150500K .......... .......... .......... .......... .......... 29% 7.85M 29s
150550K .......... .......... .......... .......... .......... 29% 8.82M 29s
150600K .......... .......... .......... .......... .......... 29% 8.25M 29s
150650K .......... .......... .......... .......... .......... 29% 8.14M 29s
150700K .......... .......... .......... .......... .......... 29% 7.68M 29s
150750K .......... .......... .......... .......... .......... 29% 8.79M 29s
150800K .......... .......... .......... .......... .......... 29% 12.5M 29s
150850K .......... .......... .......... .......... .......... 29% 16.6M 29s
150900K .......... .......... .......... .......... .......... 29% 28.1M 29s
150950K .......... .......... .......... .......... .......... 29% 17.3M 29s
151000K .......... .......... .......... .......... .......... 29% 29.0M 29s
151050K .......... .......... .......... .......... .......... 30% 28.3M 29s
151100K .......... .......... .......... .......... .......... 30% 23.5M 29s
151150K .......... .......... .......... .......... .......... 30% 21.0M 29s
151200K .......... .......... .......... .......... .......... 30% 17.5M 29s
151250K .......... .......... .......... .......... .......... 30% 27.4M 29s
151300K .......... .......... .......... .......... .......... 30% 18.3M 29s
151350K .......... .......... .......... .......... .......... 30% 19.8M 29s
151400K .......... .......... .......... .......... .......... 30% 31.6M 29s
151450K .......... .......... .......... .......... .......... 30% 17.7M 29s
151500K .......... .......... .......... .......... .......... 30% 18.7M 29s
151550K .......... .......... .......... .......... .......... 30% 20.5M 29s
151600K .......... .......... .......... .......... .......... 30% 18.4M 29s
151650K .......... .......... .......... .......... .......... 30% 9.20M 29s
151700K .......... .......... .......... .......... .......... 30% 12.4M 29s
151750K .......... .......... .......... .......... .......... 30% 18.7M 29s
151800K .......... .......... .......... .......... .......... 30% 15.6M 29s
151850K .......... .......... .......... .......... .......... 30% 11.7M 29s
151900K .......... .......... .......... .......... .......... 30% 17.3M 29s
151950K .......... .......... .......... .......... .......... 30% 13.9M 29s
152000K .......... .......... .......... .......... .......... 30% 13.3M 29s
152050K .......... .......... .......... .......... .......... 30% 13.4M 29s
152100K .......... .......... .......... .......... .......... 30% 8.93M 29s
152150K .......... .......... .......... .......... .......... 30% 12.7M 29s
152200K .......... .......... .......... .......... .......... 30% 7.26M 29s
152250K .......... .......... .......... .......... .......... 30% 12.9M 29s
152300K .......... .......... .......... .......... .......... 30% 8.52M 29s
152350K .......... .......... .......... .......... .......... 30% 7.44M 29s
152400K .......... .......... .......... .......... .......... 30% 8.03M 29s
152450K .......... .......... .......... .......... .......... 30% 7.17M 29s
152500K .......... .......... .......... .......... .......... 30% 7.73M 29s
152550K .......... .......... .......... .......... .......... 30% 10.3M 29s
152600K .......... .......... .......... .......... .......... 30% 27.5M 29s
152650K .......... .......... .......... .......... .......... 30% 19.9M 29s
152700K .......... .......... .......... .......... .......... 30% 14.4M 29s
152750K .......... .......... .......... .......... .......... 30% 9.18M 29s
152800K .......... .......... .......... .......... .......... 30% 10.4M 29s
152850K .......... .......... .......... .......... .......... 30% 10.4M 29s
152900K .......... .......... .......... .......... .......... 30% 13.4M 29s
152950K .......... .......... .......... .......... .......... 30% 11.3M 29s
153000K .......... .......... .......... .......... .......... 30% 8.05M 29s
153050K .......... .......... .......... .......... .......... 30% 7.09M 29s
153100K .......... .......... .......... .......... .......... 30% 8.05M 29s
153150K .......... .......... .......... .......... .......... 30% 9.17M 29s
153200K .......... .......... .......... .......... .......... 30% 8.61M 29s
153250K .......... .......... .......... .......... .......... 30% 8.63M 29s
153300K .......... .......... .......... .......... .......... 30% 6.86M 29s
153350K .......... .......... .......... .......... .......... 30% 3.97M 29s
153400K .......... .......... .......... .......... .......... 30% 3.53M 29s
153450K .......... .......... .......... .......... .......... 30% 3.88M 29s
153500K .......... .......... .......... .......... .......... 30% 18.2M 29s
153550K .......... .......... .......... .......... .......... 30% 28.9M 29s
153600K .......... .......... .......... .......... .......... 30% 54.4M 29s
153650K .......... .......... .......... .......... .......... 30% 33.7M 29s
153700K .......... .......... .......... .......... .......... 30% 19.9M 29s
153750K .......... .......... .......... .......... .......... 30%  139M 29s
153800K .......... .......... .......... .......... .......... 30% 47.9M 29s
153850K .......... .......... .......... .......... .......... 30% 21.1M 29s
153900K .......... .......... .......... .......... .......... 30% 25.8M 29s
153950K .......... .......... .......... .......... .......... 30% 14.7M 29s
154000K .......... .......... .......... .......... .......... 30% 15.2M 29s
154050K .......... .......... .......... .......... .......... 30% 12.8M 29s
154100K .......... .......... .......... .......... .......... 30% 14.2M 29s
154150K .......... .......... .......... .......... .......... 30% 17.1M 29s
154200K .......... .......... .......... .......... .......... 30% 11.0M 29s
154250K .......... .......... .......... .......... .......... 30% 13.8M 29s
154300K .......... .......... .......... .......... .......... 30% 15.1M 29s
154350K .......... .......... .......... .......... .......... 30% 11.7M 29s
154400K .......... .......... .......... .......... .......... 30% 12.7M 29s
154450K .......... .......... .......... .......... .......... 30% 9.53M 29s
154500K .......... .......... .......... .......... .......... 30% 11.1M 29s
154550K .......... .......... .......... .......... .......... 30% 16.0M 29s
154600K .......... .......... .......... .......... .......... 30% 25.8M 29s
154650K .......... .......... .......... .......... .......... 30% 20.2M 29s
154700K .......... .......... .......... .......... .......... 30%  115M 29s
154750K .......... .......... .......... .......... .......... 30% 35.7M 29s
154800K .......... .......... .......... .......... .......... 30% 24.1M 29s
154850K .......... .......... .......... .......... .......... 30% 23.5M 29s
154900K .......... .......... .......... .......... .......... 30% 18.7M 29s
154950K .......... .......... .......... .......... .......... 30% 26.3M 29s
155000K .......... .......... .......... .......... .......... 30% 18.1M 29s
155050K .......... .......... .......... .......... .......... 30% 16.4M 29s
155100K .......... .......... .......... .......... .......... 30% 14.4M 29s
155150K .......... .......... .......... .......... .......... 30% 14.0M 29s
155200K .......... .......... .......... .......... .......... 30% 11.2M 29s
155250K .......... .......... .......... .......... .......... 30% 12.2M 29s
155300K .......... .......... .......... .......... .......... 30% 9.43M 29s
155350K .......... .......... .......... .......... .......... 30% 9.69M 29s
155400K .......... .......... .......... .......... .......... 30% 10.5M 29s
155450K .......... .......... .......... .......... .......... 30% 10.2M 29s
155500K .......... .......... .......... .......... .......... 30% 10.8M 29s
155550K .......... .......... .......... .......... .......... 30% 12.1M 29s
155600K .......... .......... .......... .......... .......... 30% 7.18M 29s
155650K .......... .......... .......... .......... .......... 30% 8.44M 29s
155700K .......... .......... .......... .......... .......... 30% 11.4M 29s
155750K .......... .......... .......... .......... .......... 30% 19.9M 29s
155800K .......... .......... .......... .......... .......... 30% 60.4M 29s
155850K .......... .......... .......... .......... .......... 30% 25.0M 29s
155900K .......... .......... .......... .......... .......... 30% 17.0M 29s
155950K .......... .......... .......... .......... .......... 30% 23.8M 29s
156000K .......... .......... .......... .......... .......... 30% 20.9M 29s
156050K .......... .......... .......... .......... .......... 30% 18.3M 29s
156100K .......... .......... .......... .......... .......... 31% 14.6M 29s
156150K .......... .......... .......... .......... .......... 31% 18.7M 29s
156200K .......... .......... .......... .......... .......... 31% 11.7M 29s
156250K .......... .......... .......... .......... .......... 31% 18.1M 29s
156300K .......... .......... .......... .......... .......... 31% 10.5M 29s
156350K .......... .......... .......... .......... .......... 31% 10.8M 29s
156400K .......... .......... .......... .......... .......... 31% 11.7M 29s
156450K .......... .......... .......... .......... .......... 31% 9.90M 29s
156500K .......... .......... .......... .......... .......... 31% 10.5M 29s
156550K .......... .......... .......... .......... .......... 31% 7.96M 29s
156600K .......... .......... .......... .......... .......... 31% 8.75M 29s
156650K .......... .......... .......... .......... .......... 31% 7.15M 29s
156700K .......... .......... .......... .......... .......... 31% 7.38M 29s
156750K .......... .......... .......... .......... .......... 31% 8.58M 29s
156800K .......... .......... .......... .......... .......... 31% 12.2M 29s
156850K .......... .......... .......... .......... .......... 31% 11.7M 29s
156900K .......... .......... .......... .......... .......... 31% 15.7M 29s
156950K .......... .......... .......... .......... .......... 31% 12.5M 29s
157000K .......... .......... .......... .......... .......... 31% 12.1M 29s
157050K .......... .......... .......... .......... .......... 31% 11.5M 29s
157100K .......... .......... .......... .......... .......... 31% 7.61M 29s
157150K .......... .......... .......... .......... .......... 31% 5.47M 29s
157200K .......... .......... .......... .......... .......... 31% 4.99M 29s
157250K .......... .......... .......... .......... .......... 31% 5.38M 29s
157300K .......... .......... .......... .......... .......... 31% 6.05M 29s
157350K .......... .......... .......... .......... .......... 31% 8.85M 29s
157400K .......... .......... .......... .......... .......... 31% 30.3M 29s
157450K .......... .......... .......... .......... .......... 31% 15.6M 29s
157500K .......... .......... .......... .......... .......... 31% 74.5M 29s
157550K .......... .......... .......... .......... .......... 31% 29.6M 29s
157600K .......... .......... .......... .......... .......... 31% 62.4M 29s
157650K .......... .......... .......... .......... .......... 31% 34.8M 29s
157700K .......... .......... .......... .......... .......... 31% 30.8M 29s
157750K .......... .......... .......... .......... .......... 31% 34.5M 29s
157800K .......... .......... .......... .......... .......... 31% 19.9M 29s
157850K .......... .......... .......... .......... .......... 31% 30.9M 29s
157900K .......... .......... .......... .......... .......... 31% 21.6M 29s
157950K .......... .......... .......... .......... .......... 31% 21.3M 29s
158000K .......... .......... .......... .......... .......... 31% 19.6M 29s
158050K .......... .......... .......... .......... .......... 31% 17.3M 29s
158100K .......... .......... .......... .......... .......... 31% 12.5M 29s
158150K .......... .......... .......... .......... .......... 31% 12.9M 29s
158200K .......... .......... .......... .......... .......... 31% 17.0M 29s
158250K .......... .......... .......... .......... .......... 31% 16.3M 29s
158300K .......... .......... .......... .......... .......... 31% 12.5M 29s
158350K .......... .......... .......... .......... .......... 31% 11.4M 29s
158400K .......... .......... .......... .......... .......... 31% 14.0M 29s
158450K .......... .......... .......... .......... .......... 31% 7.56M 29s
158500K .......... .......... .......... .......... .......... 31% 11.4M 29s
158550K .......... .......... .......... .......... .......... 31% 11.2M 29s
158600K .......... .......... .......... .......... .......... 31% 9.40M 29s
158650K .......... .......... .......... .......... .......... 31% 9.61M 29s
158700K .......... .......... .......... .......... .......... 31% 9.24M 29s
158750K .......... .......... .......... .......... .......... 31% 8.64M 29s
158800K .......... .......... .......... .......... .......... 31% 8.68M 29s
158850K .......... .......... .......... .......... .......... 31% 7.18M 29s
158900K .......... .......... .......... .......... .......... 31% 9.27M 29s
158950K .......... .......... .......... .......... .......... 31% 10.3M 29s
159000K .......... .......... .......... .......... .......... 31% 28.6M 29s
159050K .......... .......... .......... .......... .......... 31% 17.3M 29s
159100K .......... .......... .......... .......... .......... 31% 17.7M 29s
159150K .......... .......... .......... .......... .......... 31% 24.0M 29s
159200K .......... .......... .......... .......... .......... 31% 19.4M 29s
159250K .......... .......... .......... .......... .......... 31% 18.9M 29s
159300K .......... .......... .......... .......... .......... 31% 18.7M 29s
159350K .......... .......... .......... .......... .......... 31% 15.7M 29s
159400K .......... .......... .......... .......... .......... 31% 17.9M 29s
159450K .......... .......... .......... .......... .......... 31% 14.0M 29s
159500K .......... .......... .......... .......... .......... 31% 15.5M 29s
159550K .......... .......... .......... .......... .......... 31% 15.1M 29s
159600K .......... .......... .......... .......... .......... 31% 9.61M 29s
159650K .......... .......... .......... .......... .......... 31% 12.5M 29s
159700K .......... .......... .......... .......... .......... 31% 7.87M 29s
159750K .......... .......... .......... .......... .......... 31% 9.49M 29s
159800K .......... .......... .......... .......... .......... 31% 8.01M 29s
159850K .......... .......... .......... .......... .......... 31% 7.06M 29s
159900K .......... .......... .......... .......... .......... 31% 6.11M 29s
159950K .......... .......... .......... .......... .......... 31% 6.53M 29s
160000K .......... .......... .......... .......... .......... 31% 8.00M 29s
160050K .......... .......... .......... .......... .......... 31% 7.70M 29s
160100K .......... .......... .......... .......... .......... 31% 6.42M 29s
160150K .......... .......... .......... .......... .......... 31% 13.9M 29s
160200K .......... .......... .......... .......... .......... 31% 7.89M 29s
160250K .......... .......... .......... .......... .......... 31% 9.24M 29s
160300K .......... .......... .......... .......... .......... 31% 7.92M 29s
160350K .......... .......... .......... .......... .......... 31% 6.23M 29s
160400K .......... .......... .......... .......... .......... 31% 8.37M 29s
160450K .......... .......... .......... .......... .......... 31% 7.10M 29s
160500K .......... .......... .......... .......... .......... 31% 7.71M 29s
160550K .......... .......... .......... .......... .......... 31% 8.06M 29s
160600K .......... .......... .......... .......... .......... 31% 5.44M 29s
160650K .......... .......... .......... .......... .......... 31% 8.06M 29s
160700K .......... .......... .......... .......... .......... 31% 14.0M 29s
160750K .......... .......... .......... .......... .......... 31% 14.6M 29s
160800K .......... .......... .......... .......... .......... 31% 16.1M 29s
160850K .......... .......... .......... .......... .......... 31% 9.15M 29s
160900K .......... .......... .......... .......... .......... 31% 9.17M 29s
160950K .......... .......... .......... .......... .......... 31% 7.26M 29s
161000K .......... .......... .......... .......... .......... 31% 8.25M 29s
161050K .......... .......... .......... .......... .......... 31% 5.66M 29s
161100K .......... .......... .......... .......... .......... 31% 7.86M 29s
161150K .......... .......... .......... .......... .......... 32% 8.86M 29s
161200K .......... .......... .......... .......... .......... 32% 7.95M 29s
161250K .......... .......... .......... .......... .......... 32% 8.87M 29s
161300K .......... .......... .......... .......... .......... 32% 7.82M 29s
161350K .......... .......... .......... .......... .......... 32% 9.44M 29s
161400K .......... .......... .......... .......... .......... 32% 25.4M 28s
161450K .......... .......... .......... .......... .......... 32% 25.4M 28s
161500K .......... .......... .......... .......... .......... 32% 33.0M 28s
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161600K .......... .......... .......... .......... .......... 32% 27.5M 28s
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161700K .......... .......... .......... .......... .......... 32% 12.0M 28s
161750K .......... .......... .......... .......... .......... 32% 14.0M 28s
161800K .......... .......... .......... .......... .......... 32% 13.0M 28s
161850K .......... .......... .......... .......... .......... 32% 8.76M 28s
161900K .......... .......... .......... .......... .......... 32% 10.8M 28s
161950K .......... .......... .......... .......... .......... 32% 8.57M 28s
162000K .......... .......... .......... .......... .......... 32% 9.49M 28s
162050K .......... .......... .......... .......... .......... 32% 7.47M 28s
162100K .......... .......... .......... .......... .......... 32% 6.69M 28s
162150K .......... .......... .......... .......... .......... 32% 5.14M 28s
162200K .......... .......... .......... .......... .......... 32% 6.06M 28s
162250K .......... .......... .......... .......... .......... 32% 7.75M 28s
162300K .......... .......... .......... .......... .......... 32% 7.75M 28s
162350K .......... .......... .......... .......... .......... 32% 7.04M 28s
162400K .......... .......... .......... .......... .......... 32% 6.56M 28s
162450K .......... .......... .......... .......... .......... 32% 9.73M 28s
162500K .......... .......... .......... .......... .......... 32% 12.6M 28s
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162600K .......... .......... .......... .......... .......... 32% 8.26M 28s
162650K .......... .......... .......... .......... .......... 32% 11.8M 28s
162700K .......... .......... .......... .......... .......... 32% 9.07M 28s
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162800K .......... .......... .......... .......... .......... 32% 7.68M 28s
162850K .......... .......... .......... .......... .......... 32% 6.84M 28s
162900K .......... .......... .......... .......... .......... 32% 9.07M 28s
162950K .......... .......... .......... .......... .......... 32% 6.10M 28s
163000K .......... .......... .......... .......... .......... 32% 8.45M 28s
163050K .......... .......... .......... .......... .......... 32% 7.31M 28s
163100K .......... .......... .......... .......... .......... 32% 7.50M 28s
163150K .......... .......... .......... .......... .......... 32% 12.5M 28s
163200K .......... .......... .......... .......... .......... 32% 9.27M 28s
163250K .......... .......... .......... .......... .......... 32% 8.81M 28s
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163350K .......... .......... .......... .......... .......... 32% 5.28M 28s
163400K .......... .......... .......... .......... .......... 32% 6.03M 28s
163450K .......... .......... .......... .......... .......... 32% 5.89M 28s
163500K .......... .......... .......... .......... .......... 32% 6.92M 28s
163550K .......... .......... .......... .......... .......... 32% 5.30M 28s
163600K .......... .......... .......... .......... .......... 32% 5.23M 28s
163650K .......... .......... .......... .......... .......... 32% 6.41M 28s
163700K .......... .......... .......... .......... .......... 32% 4.82M 28s
163750K .......... .......... .......... .......... .......... 32% 5.33M 28s
163800K .......... .......... .......... .......... .......... 32% 9.81M 28s
163850K .......... .......... .......... .......... .......... 32% 15.1M 28s
163900K .......... .......... .......... .......... .......... 32% 20.8M 28s
163950K .......... .......... .......... .......... .......... 32% 17.8M 28s
164000K .......... .......... .......... .......... .......... 32% 11.7M 28s
164050K .......... .......... .......... .......... .......... 32% 16.3M 28s
164100K .......... .......... .......... .......... .......... 32% 10.5M 28s
164150K .......... .......... .......... .......... .......... 32% 11.8M 28s
164200K .......... .......... .......... .......... .......... 32% 10.8M 28s
164250K .......... .......... .......... .......... .......... 32% 13.0M 28s
164300K .......... .......... .......... .......... .......... 32% 12.4M 28s
164350K .......... .......... .......... .......... .......... 32% 11.8M 28s
164400K .......... .......... .......... .......... .......... 32% 9.03M 28s
164450K .......... .......... .......... .......... .......... 32% 8.07M 28s
164500K .......... .......... .......... .......... .......... 32% 8.06M 28s
164550K .......... .......... .......... .......... .......... 32% 7.54M 28s
164600K .......... .......... .......... .......... .......... 32% 10.2M 28s
164650K .......... .......... .......... .......... .......... 32% 9.65M 28s
164700K .......... .......... .......... .......... .......... 32% 9.42M 28s
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177250K .......... .......... .......... .......... .......... 35% 11.0M 27s
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177650K .......... .......... .......... .......... .......... 35% 41.6M 27s
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177850K .......... .......... .......... .......... .......... 35% 14.5M 27s
177900K .......... .......... .......... .......... .......... 35% 19.8M 27s
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178000K .......... .......... .......... .......... .......... 35% 15.7M 27s
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178250K .......... .......... .......... .......... .......... 35% 17.2M 27s
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178350K .......... .......... .......... .......... .......... 35% 61.9M 27s
178400K .......... .......... .......... .......... .......... 35% 24.1M 27s
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178750K .......... .......... .......... .......... .......... 35% 11.9M 27s
178800K .......... .......... .......... .......... .......... 35% 8.31M 27s
178850K .......... .......... .......... .......... .......... 35% 10.0M 27s
178900K .......... .......... .......... .......... .......... 35% 15.6M 27s
178950K .......... .......... .......... .......... .......... 35% 11.0M 27s
179000K .......... .......... .......... .......... .......... 35% 10.2M 27s
179050K .......... .......... .......... .......... .......... 35% 9.41M 27s
179100K .......... .......... .......... .......... .......... 35% 8.58M 27s
179150K .......... .......... .......... .......... .......... 35% 9.19M 27s
179200K .......... .......... .......... .......... .......... 35% 7.03M 27s
179250K .......... .......... .......... .......... .......... 35% 8.60M 27s
179300K .......... .......... .......... .......... .......... 35% 8.57M 27s
179350K .......... .......... .......... .......... .......... 35% 8.10M 27s
179400K .......... .......... .......... .......... .......... 35% 15.9M 27s
179450K .......... .......... .......... .......... .......... 35% 16.4M 27s
179500K .......... .......... .......... .......... .......... 35% 27.5M 27s
179550K .......... .......... .......... .......... .......... 35% 22.4M 27s
179600K .......... .......... .......... .......... .......... 35% 22.9M 27s
179650K .......... .......... .......... .......... .......... 35% 24.3M 27s
179700K .......... .......... .......... .......... .......... 35% 17.9M 27s
179750K .......... .......... .......... .......... .......... 35% 19.8M 27s
179800K .......... .......... .......... .......... .......... 35% 17.8M 27s
179850K .......... .......... .......... .......... .......... 35% 17.3M 27s
179900K .......... .......... .......... .......... .......... 35% 16.3M 27s
179950K .......... .......... .......... .......... .......... 35% 9.24M 27s
180000K .......... .......... .......... .......... .......... 35% 15.7M 27s
180050K .......... .......... .......... .......... .......... 35% 17.9M 27s
180100K .......... .......... .......... .......... .......... 35% 17.3M 27s
180150K .......... .......... .......... .......... .......... 35% 16.5M 27s
180200K .......... .......... .......... .......... .......... 35% 16.0M 27s
180250K .......... .......... .......... .......... .......... 35% 26.6M 27s
180300K .......... .......... .......... .......... .......... 35% 29.3M 27s
180350K .......... .......... .......... .......... .......... 35% 23.1M 27s
180400K .......... .......... .......... .......... .......... 35% 28.6M 27s
180450K .......... .......... .......... .......... .......... 35% 15.6M 27s
180500K .......... .......... .......... .......... .......... 35% 20.8M 27s
180550K .......... .......... .......... .......... .......... 35% 14.3M 27s
180600K .......... .......... .......... .......... .......... 35% 10.6M 27s
180650K .......... .......... .......... .......... .......... 35% 11.1M 27s
180700K .......... .......... .......... .......... .......... 35% 8.33M 27s
180750K .......... .......... .......... .......... .......... 35% 8.73M 27s
180800K .......... .......... .......... .......... .......... 35% 10.5M 27s
180850K .......... .......... .......... .......... .......... 35% 6.87M 27s
180900K .......... .......... .......... .......... .......... 35% 9.08M 27s
180950K .......... .......... .......... .......... .......... 35% 7.71M 27s
181000K .......... .......... .......... .......... .......... 35% 16.9M 27s
181050K .......... .......... .......... .......... .......... 35% 30.4M 27s
181100K .......... .......... .......... .......... .......... 35% 14.6M 27s
181150K .......... .......... .......... .......... .......... 35% 16.7M 27s
181200K .......... .......... .......... .......... .......... 35% 19.0M 27s
181250K .......... .......... .......... .......... .......... 36% 20.4M 27s
181300K .......... .......... .......... .......... .......... 36% 15.8M 27s
181350K .......... .......... .......... .......... .......... 36% 15.5M 27s
181400K .......... .......... .......... .......... .......... 36% 10.1M 27s
181450K .......... .......... .......... .......... .......... 36% 10.5M 27s
181500K .......... .......... .......... .......... .......... 36% 14.1M 27s
181550K .......... .......... .......... .......... .......... 36% 11.4M 27s
181600K .......... .......... .......... .......... .......... 36% 9.88M 27s
181650K .......... .......... .......... .......... .......... 36% 11.0M 27s
181700K .......... .......... .......... .......... .......... 36% 9.64M 27s
181750K .......... .......... .......... .......... .......... 36% 10.5M 27s
181800K .......... .......... .......... .......... .......... 36% 11.1M 27s
181850K .......... .......... .......... .......... .......... 36% 8.29M 27s
181900K .......... .......... .......... .......... .......... 36% 10.6M 27s
181950K .......... .......... .......... .......... .......... 36% 8.16M 27s
182000K .......... .......... .......... .......... .......... 36% 17.2M 27s
182050K .......... .......... .......... .......... .......... 36% 13.6M 27s
182100K .......... .......... .......... .......... .......... 36% 40.6M 27s
182150K .......... .......... .......... .......... .......... 36% 21.2M 27s
182200K .......... .......... .......... .......... .......... 36% 18.0M 27s
182250K .......... .......... .......... .......... .......... 36% 14.7M 27s
182300K .......... .......... .......... .......... .......... 36% 21.1M 27s
182350K .......... .......... .......... .......... .......... 36% 12.9M 27s
182400K .......... .......... .......... .......... .......... 36% 13.2M 27s
182450K .......... .......... .......... .......... .......... 36% 10.5M 27s
182500K .......... .......... .......... .......... .......... 36% 18.6M 27s
182550K .......... .......... .......... .......... .......... 36% 12.1M 27s
182600K .......... .......... .......... .......... .......... 36% 12.1M 27s
182650K .......... .......... .......... .......... .......... 36% 11.1M 27s
182700K .......... .......... .......... .......... .......... 36% 12.4M 27s
182750K .......... .......... .......... .......... .......... 36% 11.1M 27s
182800K .......... .......... .......... .......... .......... 36% 10.1M 27s
182850K .......... .......... .......... .......... .......... 36% 11.4M 27s
182900K .......... .......... .......... .......... .......... 36% 12.1M 27s
182950K .......... .......... .......... .......... .......... 36% 10.3M 27s
183000K .......... .......... .......... .......... .......... 36% 11.4M 27s
183050K .......... .......... .......... .......... .......... 36% 10.5M 27s
183100K .......... .......... .......... .......... .......... 36% 9.38M 27s
183150K .......... .......... .......... .......... .......... 36% 9.89M 27s
183200K .......... .......... .......... .......... .......... 36% 7.58M 27s
183250K .......... .......... .......... .......... .......... 36% 8.61M 27s
183300K .......... .......... .......... .......... .......... 36% 31.9M 27s
183350K .......... .......... .......... .......... .......... 36% 16.2M 27s
183400K .......... .......... .......... .......... .......... 36% 13.4M 27s
183450K .......... .......... .......... .......... .......... 36% 10.8M 27s
183500K .......... .......... .......... .......... .......... 36% 12.8M 27s
183550K .......... .......... .......... .......... .......... 36% 11.5M 27s
183600K .......... .......... .......... .......... .......... 36% 10.0M 27s
183650K .......... .......... .......... .......... .......... 36% 9.94M 27s
183700K .......... .......... .......... .......... .......... 36% 13.2M 27s
183750K .......... .......... .......... .......... .......... 36% 14.1M 27s
183800K .......... .......... .......... .......... .......... 36% 15.5M 27s
183850K .......... .......... .......... .......... .......... 36% 77.4M 27s
183900K .......... .......... .......... .......... .......... 36% 27.3M 27s
183950K .......... .......... .......... .......... .......... 36% 30.0M 27s
184000K .......... .......... .......... .......... .......... 36% 21.3M 27s
184050K .......... .......... .......... .......... .......... 36% 18.4M 27s
184100K .......... .......... .......... .......... .......... 36% 15.5M 27s
184150K .......... .......... .......... .......... .......... 36% 14.5M 27s
184200K .......... .......... .......... .......... .......... 36% 11.1M 27s
184250K .......... .......... .......... .......... .......... 36% 14.5M 27s
184300K .......... .......... .......... .......... .......... 36% 12.5M 27s
184350K .......... .......... .......... .......... .......... 36% 7.29M 27s
184400K .......... .......... .......... .......... .......... 36% 8.71M 27s
184450K .......... .......... .......... .......... .......... 36% 6.98M 27s
184500K .......... .......... .......... .......... .......... 36% 6.93M 27s
184550K .......... .......... .......... .......... .......... 36% 8.11M 27s
184600K .......... .......... .......... .......... .......... 36% 5.58M 27s
184650K .......... .......... .......... .......... .......... 36% 8.42M 27s
184700K .......... .......... .......... .......... .......... 36% 18.7M 27s
184750K .......... .......... .......... .......... .......... 36% 26.7M 27s
184800K .......... .......... .......... .......... .......... 36% 15.2M 27s
184850K .......... .......... .......... .......... .......... 36% 12.5M 27s
184900K .......... .......... .......... .......... .......... 36% 14.9M 27s
184950K .......... .......... .......... .......... .......... 36% 13.3M 27s
185000K .......... .......... .......... .......... .......... 36% 12.9M 27s
185050K .......... .......... .......... .......... .......... 36% 16.4M 27s
185100K .......... .......... .......... .......... .......... 36% 13.9M 27s
185150K .......... .......... .......... .......... .......... 36% 13.0M 27s
185200K .......... .......... .......... .......... .......... 36% 9.89M 27s
185250K .......... .......... .......... .......... .......... 36% 11.7M 27s
185300K .......... .......... .......... .......... .......... 36% 16.3M 27s
185350K .......... .......... .......... .......... .......... 36% 11.1M 27s
185400K .......... .......... .......... .......... .......... 36% 12.9M 27s
185450K .......... .......... .......... .......... .......... 36% 11.4M 27s
185500K .......... .......... .......... .......... .......... 36% 8.01M 27s
185550K .......... .......... .......... .......... .......... 36% 6.40M 27s
185600K .......... .......... .......... .......... .......... 36% 5.34M 27s
185650K .......... .......... .......... .......... .......... 36% 6.51M 27s
185700K .......... .......... .......... .......... .......... 36% 6.02M 27s
185750K .......... .......... .......... .......... .......... 36% 18.2M 27s
185800K .......... .......... .......... .......... .......... 36% 29.0M 27s
185850K .......... .......... .......... .......... .......... 36% 17.2M 27s
185900K .......... .......... .......... .......... .......... 36% 31.2M 27s
185950K .......... .......... .......... .......... .......... 36% 17.0M 27s
186000K .......... .......... .......... .......... .......... 36% 64.1M 27s
186050K .......... .......... .......... .......... .......... 36% 17.7M 27s
186100K .......... .......... .......... .......... .......... 36% 18.7M 27s
186150K .......... .......... .......... .......... .......... 36% 24.9M 26s
186200K .......... .......... .......... .......... .......... 36% 13.3M 26s
186250K .......... .......... .......... .......... .......... 36% 15.8M 26s
186300K .......... .......... .......... .......... .......... 37% 17.0M 26s
186350K .......... .......... .......... .......... .......... 37% 11.8M 26s
186400K .......... .......... .......... .......... .......... 37% 16.3M 26s
186450K .......... .......... .......... .......... .......... 37% 13.9M 26s
186500K .......... .......... .......... .......... .......... 37% 13.4M 26s
186550K .......... .......... .......... .......... .......... 37% 12.6M 26s
186600K .......... .......... .......... .......... .......... 37% 13.0M 26s
186650K .......... .......... .......... .......... .......... 37% 16.4M 26s
186700K .......... .......... .......... .......... .......... 37% 9.39M 26s
186750K .......... .......... .......... .......... .......... 37% 11.1M 26s
186800K .......... .......... .......... .......... .......... 37% 10.9M 26s
186850K .......... .......... .......... .......... .......... 37% 9.87M 26s
186900K .......... .......... .......... .......... .......... 37% 13.4M 26s
186950K .......... .......... .......... .......... .......... 37% 7.56M 26s
187000K .......... .......... .......... .......... .......... 37% 9.48M 26s
187050K .......... .......... .......... .......... .......... 37% 14.1M 26s
187100K .......... .......... .......... .......... .......... 37% 8.89M 26s
187150K .......... .......... .......... .......... .......... 37% 12.1M 26s
187200K .......... .......... .......... .......... .......... 37% 9.17M 26s
187250K .......... .......... .......... .......... .......... 37% 10.2M 26s
187300K .......... .......... .......... .......... .......... 37% 8.24M 26s
187350K .......... .......... .......... .......... .......... 37% 10.0M 26s
187400K .......... .......... .......... .......... .......... 37% 7.78M 26s
187450K .......... .......... .......... .......... .......... 37% 9.34M 26s
187500K .......... .......... .......... .......... .......... 37% 8.07M 26s
187550K .......... .......... .......... .......... .......... 37% 6.87M 26s
187600K .......... .......... .......... .......... .......... 37% 5.69M 26s
187650K .......... .......... .......... .......... .......... 37% 6.65M 26s
187700K .......... .......... .......... .......... .......... 37% 5.64M 26s
187750K .......... .......... .......... .......... .......... 37% 6.89M 26s
187800K .......... .......... .......... .......... .......... 37% 17.6M 26s
187850K .......... .......... .......... .......... .......... 37% 17.2M 26s
187900K .......... .......... .......... .......... .......... 37% 19.5M 26s
187950K .......... .......... .......... .......... .......... 37% 29.6M 26s
188000K .......... .......... .......... .......... .......... 37% 17.4M 26s
188050K .......... .......... .......... .......... .......... 37% 33.5M 26s
188100K .......... .......... .......... .......... .......... 37% 22.1M 26s
188150K .......... .......... .......... .......... .......... 37% 31.6M 26s
188200K .......... .......... .......... .......... .......... 37% 22.0M 26s
188250K .......... .......... .......... .......... .......... 37% 29.2M 26s
188300K .......... .......... .......... .......... .......... 37% 31.4M 26s
188350K .......... .......... .......... .......... .......... 37% 21.2M 26s
188400K .......... .......... .......... .......... .......... 37% 9.42M 26s
188450K .......... .......... .......... .......... .......... 37% 26.3M 26s
188500K .......... .......... .......... .......... .......... 37% 18.1M 26s
188550K .......... .......... .......... .......... .......... 37% 23.4M 26s
188600K .......... .......... .......... .......... .......... 37% 27.5M 26s
188650K .......... .......... .......... .......... .......... 37% 18.9M 26s
188700K .......... .......... .......... .......... .......... 37% 13.1M 26s
188750K .......... .......... .......... .......... .......... 37% 16.3M 26s
188800K .......... .......... .......... .......... .......... 37% 12.5M 26s
188850K .......... .......... .......... .......... .......... 37% 7.59M 26s
188900K .......... .......... .......... .......... .......... 37% 8.76M 26s
188950K .......... .......... .......... .......... .......... 37% 7.59M 26s
189000K .......... .......... .......... .......... .......... 37% 6.77M 26s
189050K .......... .......... .......... .......... .......... 37% 9.89M 26s
189100K .......... .......... .......... .......... .......... 37% 9.23M 26s
189150K .......... .......... .......... .......... .......... 37% 9.04M 26s
189200K .......... .......... .......... .......... .......... 37% 8.17M 26s
189250K .......... .......... .......... .......... .......... 37% 12.7M 26s
189300K .......... .......... .......... .......... .......... 37% 11.8M 26s
189350K .......... .......... .......... .......... .......... 37% 9.96M 26s
189400K .......... .......... .......... .......... .......... 37% 12.5M 26s
189450K .......... .......... .......... .......... .......... 37% 10.1M 26s
189500K .......... .......... .......... .......... .......... 37% 12.3M 26s
189550K .......... .......... .......... .......... .......... 37% 11.9M 26s
189600K .......... .......... .......... .......... .......... 37% 9.73M 26s
189650K .......... .......... .......... .......... .......... 37% 10.9M 26s
189700K .......... .......... .......... .......... .......... 37% 6.23M 26s
189750K .......... .......... .......... .......... .......... 37% 9.03M 26s
189800K .......... .......... .......... .......... .......... 37% 7.80M 26s
189850K .......... .......... .......... .......... .......... 37% 5.96M 26s
189900K .......... .......... .......... .......... .......... 37% 9.22M 26s
189950K .......... .......... .......... .......... .......... 37% 8.39M 26s
190000K .......... .......... .......... .......... .......... 37% 10.1M 26s
190050K .......... .......... .......... .......... .......... 37% 6.77M 26s
190100K .......... .......... .......... .......... .......... 37% 6.78M 26s
190150K .......... .......... .......... .......... .......... 37% 6.02M 26s
190200K .......... .......... .......... .......... .......... 37% 4.65M 26s
190250K .......... .......... .......... .......... .......... 37% 5.98M 26s
190300K .......... .......... .......... .......... .......... 37% 5.81M 26s
190350K .......... .......... .......... .......... .......... 37% 11.9M 26s
190400K .......... .......... .......... .......... .......... 37% 12.1M 26s
190450K .......... .......... .......... .......... .......... 37% 9.92M 26s
190500K .......... .......... .......... .......... .......... 37% 11.8M 26s
190550K .......... .......... .......... .......... .......... 37% 10.5M 26s
190600K .......... .......... .......... .......... .......... 37% 9.72M 26s
190650K .......... .......... .......... .......... .......... 37% 6.53M 26s
190700K .......... .......... .......... .......... .......... 37% 7.39M 26s
190750K .......... .......... .......... .......... .......... 37% 7.57M 26s
190800K .......... .......... .......... .......... .......... 37% 7.64M 26s
190850K .......... .......... .......... .......... .......... 37% 5.86M 26s
190900K .......... .......... .......... .......... .......... 37% 9.21M 26s
190950K .......... .......... .......... .......... .......... 37% 7.00M 26s
191000K .......... .......... .......... .......... .......... 37% 7.41M 26s
191050K .......... .......... .......... .......... .......... 37% 7.93M 26s
191100K .......... .......... .......... .......... .......... 37% 6.89M 26s
191150K .......... .......... .......... .......... .......... 37% 13.5M 26s
191200K .......... .......... .......... .......... .......... 37% 25.0M 26s
191250K .......... .......... .......... .......... .......... 37% 18.9M 26s
191300K .......... .......... .......... .......... .......... 37% 39.0M 26s
191350K .......... .......... .......... .......... .......... 38% 17.4M 26s
191400K .......... .......... .......... .......... .......... 38% 18.0M 26s
191450K .......... .......... .......... .......... .......... 38% 14.0M 26s
191500K .......... .......... .......... .......... .......... 38% 19.6M 26s
191550K .......... .......... .......... .......... .......... 38% 13.4M 26s
191600K .......... .......... .......... .......... .......... 38% 11.5M 26s
191650K .......... .......... .......... .......... .......... 38% 13.5M 26s
191700K .......... .......... .......... .......... .......... 38% 9.94M 26s
191750K .......... .......... .......... .......... .......... 38% 9.64M 26s
191800K .......... .......... .......... .......... .......... 38% 10.2M 26s
191850K .......... .......... .......... .......... .......... 38% 8.87M 26s
191900K .......... .......... .......... .......... .......... 38% 7.45M 26s
191950K .......... .......... .......... .......... .......... 38% 4.79M 26s
192000K .......... .......... .......... .......... .......... 38% 5.96M 26s
192050K .......... .......... .......... .......... .......... 38% 14.7M 26s
192100K .......... .......... .......... .......... .......... 38% 18.0M 26s
192150K .......... .......... .......... .......... .......... 38% 16.1M 26s
192200K .......... .......... .......... .......... .......... 38% 12.1M 26s
192250K .......... .......... .......... .......... .......... 38% 19.6M 26s
192300K .......... .......... .......... .......... .......... 38% 14.1M 26s
192350K .......... .......... .......... .......... .......... 38% 16.2M 26s
192400K .......... .......... .......... .......... .......... 38% 11.5M 26s
192450K .......... .......... .......... .......... .......... 38% 14.9M 26s
192500K .......... .......... .......... .......... .......... 38% 14.9M 26s
192550K .......... .......... .......... .......... .......... 38% 12.6M 26s
192600K .......... .......... .......... .......... .......... 38% 11.4M 26s
192650K .......... .......... .......... .......... .......... 38%  224K 26s
192700K .......... .......... .......... .......... .......... 38% 4.21M 26s
192750K .......... .......... .......... .......... .......... 38% 7.28M 26s
192800K .......... .......... .......... .......... .......... 38% 8.49M 26s
192850K .......... .......... .......... .......... .......... 38% 10.0M 26s
192900K .......... .......... .......... .......... .......... 38% 11.4M 26s
192950K .......... .......... .......... .......... .......... 38% 3.97M 26s
193000K .......... .......... .......... .......... .......... 38%  925K 26s
193050K .......... .......... .......... .......... .......... 38% 4.32M 26s
193100K .......... .......... .......... .......... .......... 38% 12.0M 26s
193150K .......... .......... .......... .......... .......... 38% 21.8M 26s
193200K .......... .......... .......... .......... .......... 38% 14.9M 26s
193250K .......... .......... .......... .......... .......... 38% 7.23M 26s
193300K .......... .......... .......... .......... .......... 38% 7.49M 26s
193350K .......... .......... .......... .......... .......... 38% 5.72M 26s
193400K .......... .......... .......... .......... .......... 38% 9.51M 26s
193450K .......... .......... .......... .......... .......... 38% 5.83M 26s
193500K .......... .......... .......... .......... .......... 38% 2.00M 27s
193550K .......... .......... .......... .......... .......... 38%  941K 27s
193600K .......... .......... .......... .......... .......... 38% 2.56M 27s
193650K .......... .......... .......... .......... .......... 38% 2.49M 27s
193700K .......... .......... .......... .......... .......... 38% 2.69M 27s
193750K .......... .......... .......... .......... .......... 38% 2.88M 27s
193800K .......... .......... .......... .......... .......... 38% 2.18M 27s
193850K .......... .......... .......... .......... .......... 38% 12.5M 27s
193900K .......... .......... .......... .......... .......... 38% 17.7M 27s
193950K .......... .......... .......... .......... .......... 38% 30.2M 27s
194000K .......... .......... .......... .......... .......... 38% 27.2M 27s
194050K .......... .......... .......... .......... .......... 38% 27.8M 27s
194100K .......... .......... .......... .......... .......... 38% 26.5M 27s
194150K .......... .......... .......... .......... .......... 38% 19.3M 27s
194200K .......... .......... .......... .......... .......... 38% 22.8M 27s
194250K .......... .......... .......... .......... .......... 38% 19.4M 27s
194300K .......... .......... .......... .......... .......... 38% 23.3M 27s
194350K .......... .......... .......... .......... .......... 38% 17.0M 27s
194400K .......... .......... .......... .......... .......... 38% 20.0M 27s
194450K .......... .......... .......... .......... .......... 38% 21.0M 27s
194500K .......... .......... .......... .......... .......... 38% 24.5M 27s
194550K .......... .......... .......... .......... .......... 38% 24.3M 27s
194600K .......... .......... .......... .......... .......... 38% 23.2M 27s
194650K .......... .......... .......... .......... .......... 38% 24.9M 27s
194700K .......... .......... .......... .......... .......... 38% 21.7M 27s
194750K .......... .......... .......... .......... .......... 38% 24.1M 27s
194800K .......... .......... .......... .......... .......... 38% 24.2M 27s
194850K .......... .......... .......... .......... .......... 38% 22.1M 27s
194900K .......... .......... .......... .......... .......... 38% 24.7M 27s
194950K .......... .......... .......... .......... .......... 38% 22.6M 27s
195000K .......... .......... .......... .......... .......... 38% 14.1M 27s
195050K .......... .......... .......... .......... .......... 38% 27.5M 26s
195100K .......... .......... .......... .......... .......... 38% 24.7M 26s
195150K .......... .......... .......... .......... .......... 38% 17.4M 26s
195200K .......... .......... .......... .......... .......... 38% 12.7M 26s
195250K .......... .......... .......... .......... .......... 38% 18.6M 26s
195300K .......... .......... .......... .......... .......... 38% 15.5M 26s
195350K .......... .......... .......... .......... .......... 38% 14.0M 26s
195400K .......... .......... .......... .......... .......... 38% 12.1M 26s
195450K .......... .......... .......... .......... .......... 38% 11.4M 26s
195500K .......... .......... .......... .......... .......... 38% 11.0M 26s
195550K .......... .......... .......... .......... .......... 38% 11.0M 26s
195600K .......... .......... .......... .......... .......... 38% 11.4M 26s
195650K .......... .......... .......... .......... .......... 38% 13.1M 26s
195700K .......... .......... .......... .......... .......... 38% 13.5M 26s
195750K .......... .......... .......... .......... .......... 38% 16.4M 26s
195800K .......... .......... .......... .......... .......... 38% 67.9M 26s
195850K .......... .......... .......... .......... .......... 38% 21.3M 26s
195900K .......... .......... .......... .......... .......... 38% 30.1M 26s
195950K .......... .......... .......... .......... .......... 38% 20.7M 26s
196000K .......... .......... .......... .......... .......... 38% 32.8M 26s
196050K .......... .......... .......... .......... .......... 38% 42.3M 26s
196100K .......... .......... .......... .......... .......... 38% 17.5M 26s
196150K .......... .......... .......... .......... .......... 38% 15.5M 26s
196200K .......... .......... .......... .......... .......... 38% 10.9M 26s
196250K .......... .......... .......... .......... .......... 38% 9.67M 26s
196300K .......... .......... .......... .......... .......... 38% 10.6M 26s
196350K .......... .......... .......... .......... .......... 38% 9.84M 26s
196400K .......... .......... .......... .......... .......... 39% 9.91M 26s
196450K .......... .......... .......... .......... .......... 39% 9.06M 26s
196500K .......... .......... .......... .......... .......... 39% 10.9M 26s
196550K .......... .......... .......... .......... .......... 39% 11.3M 26s
196600K .......... .......... .......... .......... .......... 39% 7.58M 26s
196650K .......... .......... .......... .......... .......... 39% 14.4M 26s
196700K .......... .......... .......... .......... .......... 39% 20.1M 26s
196750K .......... .......... .......... .......... .......... 39% 17.1M 26s
196800K .......... .......... .......... .......... .......... 39% 17.5M 26s
196850K .......... .......... .......... .......... .......... 39% 10.6M 26s
196900K .......... .......... .......... .......... .......... 39% 13.7M 26s
196950K .......... .......... .......... .......... .......... 39% 8.00M 26s
197000K .......... .......... .......... .......... .......... 39% 13.6M 26s
197050K .......... .......... .......... .......... .......... 39% 13.5M 26s
197100K .......... .......... .......... .......... .......... 39% 2.83M 26s
197150K .......... .......... .......... .......... .......... 39% 4.73M 26s
197200K .......... .......... .......... .......... .......... 39% 7.92M 26s
197250K .......... .......... .......... .......... .......... 39% 7.67M 26s
197300K .......... .......... .......... .......... .......... 39% 9.73M 26s
197350K .......... .......... .......... .......... .......... 39% 6.29M 26s
197400K .......... .......... .......... .......... .......... 39% 12.1M 26s
197450K .......... .......... .......... .......... .......... 39% 11.3M 26s
197500K .......... .......... .......... .......... .......... 39% 11.2M 26s
197550K .......... .......... .......... .......... .......... 39% 16.9M 26s
197600K .......... .......... .......... .......... .......... 39% 7.26M 26s
197650K .......... .......... .......... .......... .......... 39% 6.83M 26s
197700K .......... .......... .......... .......... .......... 39% 6.74M 26s
197750K .......... .......... .......... .......... .......... 39% 9.70M 26s
197800K .......... .......... .......... .......... .......... 39% 7.99M 26s
197850K .......... .......... .......... .......... .......... 39% 6.76M 26s
197900K .......... .......... .......... .......... .......... 39% 10.5M 26s
197950K .......... .......... .......... .......... .......... 39% 8.55M 26s
198000K .......... .......... .......... .......... .......... 39% 7.31M 26s
198050K .......... .......... .......... .......... .......... 39% 7.68M 26s
198100K .......... .......... .......... .......... .......... 39% 4.84M 26s
198150K .......... .......... .......... .......... .......... 39% 5.92M 26s
198200K .......... .......... .......... .......... .......... 39% 11.1M 26s
198250K .......... .......... .......... .......... .......... 39% 14.4M 26s
198300K .......... .......... .......... .......... .......... 39% 32.5M 26s
198350K .......... .......... .......... .......... .......... 39% 11.8M 26s
198400K .......... .......... .......... .......... .......... 39% 12.1M 26s
198450K .......... .......... .......... .......... .......... 39% 9.74M 26s
198500K .......... .......... .......... .......... .......... 39% 9.85M 26s
198550K .......... .......... .......... .......... .......... 39% 11.1M 26s
198600K .......... .......... .......... .......... .......... 39% 9.69M 26s
198650K .......... .......... .......... .......... .......... 39% 9.70M 26s
198700K .......... .......... .......... .......... .......... 39% 12.8M 26s
198750K .......... .......... .......... .......... .......... 39% 12.9M 26s
198800K .......... .......... .......... .......... .......... 39% 15.4M 26s
198850K .......... .......... .......... .......... .......... 39% 10.7M 26s
198900K .......... .......... .......... .......... .......... 39% 13.3M 26s
198950K .......... .......... .......... .......... .......... 39% 9.99M 26s
199000K .......... .......... .......... .......... .......... 39% 15.7M 26s
199050K .......... .......... .......... .......... .......... 39% 16.8M 26s
199100K .......... .......... .......... .......... .......... 39% 12.9M 26s
199150K .......... .......... .......... .......... .......... 39% 12.9M 26s
199200K .......... .......... .......... .......... .......... 39% 11.8M 26s
199250K .......... .......... .......... .......... .......... 39% 24.5M 26s
199300K .......... .......... .......... .......... .......... 39% 33.7M 26s
199350K .......... .......... .......... .......... .......... 39% 39.2M 26s
199400K .......... .......... .......... .......... .......... 39% 73.8M 26s
199450K .......... .......... .......... .......... .......... 39% 55.1M 26s
199500K .......... .......... .......... .......... .......... 39% 30.4M 26s
199550K .......... .......... .......... .......... .......... 39% 80.7M 26s
199600K .......... .......... .......... .......... .......... 39%  103M 26s
199650K .......... .......... .......... .......... .......... 39% 26.6M 26s
199700K .......... .......... .......... .......... .......... 39% 62.4M 26s
199750K .......... .......... .......... .......... .......... 39% 39.5M 26s
199800K .......... .......... .......... .......... .......... 39% 35.8M 26s
199850K .......... .......... .......... .......... .......... 39% 19.2M 26s
199900K .......... .......... .......... .......... .......... 39% 42.4M 26s
199950K .......... .......... .......... .......... .......... 39% 19.0M 26s
200000K .......... .......... .......... .......... .......... 39% 23.4M 26s
200050K .......... .......... .......... .......... .......... 39% 23.1M 26s
200100K .......... .......... .......... .......... .......... 39% 13.2M 26s
200150K .......... .......... .......... .......... .......... 39% 18.1M 26s
200200K .......... .......... .......... .......... .......... 39% 16.7M 26s
200250K .......... .......... .......... .......... .......... 39% 16.9M 26s
200300K .......... .......... .......... .......... .......... 39% 14.9M 26s
200350K .......... .......... .......... .......... .......... 39% 8.58M 26s
200400K .......... .......... .......... .......... .......... 39% 12.4M 26s
200450K .......... .......... .......... .......... .......... 39% 9.75M 26s
200500K .......... .......... .......... .......... .......... 39% 12.1M 26s
200550K .......... .......... .......... .......... .......... 39% 9.91M 26s
200600K .......... .......... .......... .......... .......... 39% 11.3M 26s
200650K .......... .......... .......... .......... .......... 39% 10.9M 26s
200700K .......... .......... .......... .......... .......... 39% 7.74M 26s
200750K .......... .......... .......... .......... .......... 39% 6.07M 26s
200800K .......... .......... .......... .......... .......... 39% 9.53M 26s
200850K .......... .......... .......... .......... .......... 39% 8.71M 26s
200900K .......... .......... .......... .......... .......... 39% 7.16M 26s
200950K .......... .......... .......... .......... .......... 39% 6.20M 26s
201000K .......... .......... .......... .......... .......... 39% 6.46M 26s
201050K .......... .......... .......... .......... .......... 39% 5.28M 26s
201100K .......... .......... .......... .......... .......... 39% 9.10M 26s
201150K .......... .......... .......... .......... .......... 39% 16.2M 26s
201200K .......... .......... .......... .......... .......... 39% 13.3M 26s
201250K .......... .......... .......... .......... .......... 39% 13.4M 26s
201300K .......... .......... .......... .......... .......... 39% 11.2M 26s
201350K .......... .......... .......... .......... .......... 39% 7.75M 26s
201400K .......... .......... .......... .......... .......... 40% 11.3M 26s
201450K .......... .......... .......... .......... .......... 40% 9.96M 26s
201500K .......... .......... .......... .......... .......... 40% 15.0M 26s
201550K .......... .......... .......... .......... .......... 40% 16.7M 26s
201600K .......... .......... .......... .......... .......... 40% 9.87M 26s
201650K .......... .......... .......... .......... .......... 40% 12.1M 26s
201700K .......... .......... .......... .......... .......... 40% 11.1M 26s
201750K .......... .......... .......... .......... .......... 40% 12.5M 26s
201800K .......... .......... .......... .......... .......... 40% 10.4M 26s
201850K .......... .......... .......... .......... .......... 40% 13.6M 26s
201900K .......... .......... .......... .......... .......... 40% 11.7M 26s
201950K .......... .......... .......... .......... .......... 40% 25.0M 26s
202000K .......... .......... .......... .......... .......... 40% 29.2M 26s
202050K .......... .......... .......... .......... .......... 40% 16.9M 26s
202100K .......... .......... .......... .......... .......... 40% 25.2M 26s
202150K .......... .......... .......... .......... .......... 40% 32.5M 26s
202200K .......... .......... .......... .......... .......... 40% 17.0M 26s
202250K .......... .......... .......... .......... .......... 40% 30.0M 26s
202300K .......... .......... .......... .......... .......... 40% 20.2M 26s
202350K .......... .......... .......... .......... .......... 40% 24.8M 26s
202400K .......... .......... .......... .......... .......... 40% 31.7M 26s
202450K .......... .......... .......... .......... .......... 40% 17.8M 26s
202500K .......... .......... .......... .......... .......... 40% 26.5M 26s
202550K .......... .......... .......... .......... .......... 40% 40.8M 26s
202600K .......... .......... .......... .......... .......... 40% 22.4M 26s
202650K .......... .......... .......... .......... .......... 40% 17.8M 26s
202700K .......... .......... .......... .......... .......... 40% 13.9M 26s
202750K .......... .......... .......... .......... .......... 40% 14.3M 26s
202800K .......... .......... .......... .......... .......... 40% 14.6M 26s
202850K .......... .......... .......... .......... .......... 40% 10.9M 26s
202900K .......... .......... .......... .......... .......... 40% 14.5M 26s
202950K .......... .......... .......... .......... .......... 40% 8.78M 26s
203000K .......... .......... .......... .......... .......... 40% 13.4M 26s
203050K .......... .......... .......... .......... .......... 40% 10.8M 26s
203100K .......... .......... .......... .......... .......... 40% 10.7M 26s
203150K .......... .......... .......... .......... .......... 40% 14.7M 26s
203200K .......... .......... .......... .......... .......... 40% 20.6M 26s
203250K .......... .......... .......... .......... .......... 40% 26.2M 26s
203300K .......... .......... .......... .......... .......... 40% 16.5M 26s
203350K .......... .......... .......... .......... .......... 40% 51.8M 26s
203400K .......... .......... .......... .......... .......... 40% 23.4M 26s
203450K .......... .......... .......... .......... .......... 40% 25.4M 26s
203500K .......... .......... .......... .......... .......... 40% 27.9M 26s
203550K .......... .......... .......... .......... .......... 40% 22.6M 26s
203600K .......... .......... .......... .......... .......... 40% 18.9M 26s
203650K .......... .......... .......... .......... .......... 40% 32.3M 26s
203700K .......... .......... .......... .......... .......... 40% 16.8M 26s
203750K .......... .......... .......... .......... .......... 40% 15.6M 26s
203800K .......... .......... .......... .......... .......... 40% 20.6M 26s
203850K .......... .......... .......... .......... .......... 40% 14.1M 26s
203900K .......... .......... .......... .......... .......... 40% 13.5M 26s
203950K .......... .......... .......... .......... .......... 40% 9.54M 26s
204000K .......... .......... .......... .......... .......... 40% 11.2M 26s
204050K .......... .......... .......... .......... .......... 40% 13.3M 26s
204100K .......... .......... .......... .......... .......... 40% 11.1M 26s
204150K .......... .......... .......... .......... .......... 40% 8.42M 26s
204200K .......... .......... .......... .......... .......... 40% 6.84M 26s
204250K .......... .......... .......... .......... .......... 40% 6.09M 26s
204300K .......... .......... .......... .......... .......... 40% 3.04M 26s
204350K .......... .......... .......... .......... .......... 40% 1.51M 26s
204400K .......... .......... .......... .......... .......... 40% 1.56M 26s
204450K .......... .......... .......... .......... .......... 40% 1.38M 26s
204500K .......... .......... .......... .......... .......... 40% 5.58M 26s
204550K .......... .......... .......... .......... .......... 40% 4.80M 26s
204600K .......... .......... .......... .......... .......... 40% 7.67M 26s
204650K .......... .......... .......... .......... .......... 40% 12.4M 26s
204700K .......... .......... .......... .......... .......... 40% 9.66M 26s
204750K .......... .......... .......... .......... .......... 40% 11.0M 26s
204800K .......... .......... .......... .......... .......... 40% 15.6M 26s
204850K .......... .......... .......... .......... .......... 40% 16.0M 26s
204900K .......... .......... .......... .......... .......... 40% 12.7M 26s
204950K .......... .......... .......... .......... .......... 40% 9.46M 26s
205000K .......... .......... .......... .......... .......... 40% 12.6M 26s
205050K .......... .......... .......... .......... .......... 40% 9.72M 26s
205100K .......... .......... .......... .......... .......... 40% 7.00M 26s
205150K .......... .......... .......... .......... .......... 40% 17.2M 26s
205200K .......... .......... .......... .......... .......... 40% 16.5M 26s
205250K .......... .......... .......... .......... .......... 40% 57.5M 26s
205300K .......... .......... .......... .......... .......... 40% 21.1M 26s
205350K .......... .......... .......... .......... .......... 40% 15.8M 26s
205400K .......... .......... .......... .......... .......... 40% 20.1M 26s
205450K .......... .......... .......... .......... .......... 40% 9.85M 26s
205500K .......... .......... .......... .......... .......... 40% 17.1M 26s
205550K .......... .......... .......... .......... .......... 40% 15.6M 26s
205600K .......... .......... .......... .......... .......... 40% 8.89M 26s
205650K .......... .......... .......... .......... .......... 40% 13.4M 26s
205700K .......... .......... .......... .......... .......... 40% 12.2M 26s
205750K .......... .......... .......... .......... .......... 40% 9.21M 26s
205800K .......... .......... .......... .......... .......... 40% 11.4M 26s
205850K .......... .......... .......... .......... .......... 40% 5.48M 26s
205900K .......... .......... .......... .......... .......... 40% 5.93M 26s
205950K .......... .......... .......... .......... .......... 40% 5.59M 26s
206000K .......... .......... .......... .......... .......... 40% 4.73M 26s
206050K .......... .......... .......... .......... .......... 40% 10.3M 26s
206100K .......... .......... .......... .......... .......... 40% 7.95M 26s
206150K .......... .......... .......... .......... .......... 40% 9.46M 26s
206200K .......... .......... .......... .......... .......... 40% 7.51M 26s
206250K .......... .......... .......... .......... .......... 40% 5.50M 26s
206300K .......... .......... .......... .......... .......... 40% 5.38M 26s
206350K .......... .......... .......... .......... .......... 40% 5.15M 26s
206400K .......... .......... .......... .......... .......... 40% 5.75M 26s
206450K .......... .......... .......... .......... .......... 41% 5.25M 26s
206500K .......... .......... .......... .......... .......... 41% 4.42M 26s
206550K .......... .......... .......... .......... .......... 41% 3.48M 26s
206600K .......... .......... .......... .......... .......... 41% 3.10M 26s
206650K .......... .......... .......... .......... .......... 41% 12.7M 26s
206700K .......... .......... .......... .......... .......... 41% 26.8M 26s
206750K .......... .......... .......... .......... .......... 41% 16.5M 26s
206800K .......... .......... .......... .......... .......... 41% 26.1M 26s
206850K .......... .......... .......... .......... .......... 41% 21.4M 26s
206900K .......... .......... .......... .......... .......... 41% 28.3M 26s
206950K .......... .......... .......... .......... .......... 41% 19.6M 26s
207000K .......... .......... .......... .......... .......... 41% 21.0M 26s
207050K .......... .......... .......... .......... .......... 41% 17.1M 26s
207100K .......... .......... .......... .......... .......... 41% 16.2M 26s
207150K .......... .......... .......... .......... .......... 41% 17.8M 26s
207200K .......... .......... .......... .......... .......... 41% 12.1M 26s
207250K .......... .......... .......... .......... .......... 41% 10.8M 26s
207300K .......... .......... .......... .......... .......... 41% 12.5M 26s
207350K .......... .......... .......... .......... .......... 41% 9.50M 26s
207400K .......... .......... .......... .......... .......... 41% 8.39M 26s
207450K .......... .......... .......... .......... .......... 41% 8.42M 26s
207500K .......... .......... .......... .......... .......... 41% 6.76M 26s
207550K .......... .......... .......... .......... .......... 41% 7.85M 26s
207600K .......... .......... .......... .......... .......... 41% 5.83M 26s
207650K .......... .......... .......... .......... .......... 41% 6.37M 26s
207700K .......... .......... .......... .......... .......... 41% 5.13M 26s
207750K .......... .......... .......... .......... .......... 41% 9.21M 26s
207800K .......... .......... .......... .......... .......... 41% 13.3M 26s
207850K .......... .......... .......... .......... .......... 41% 31.1M 26s
207900K .......... .......... .......... .......... .......... 41% 19.9M 26s
207950K .......... .......... .......... .......... .......... 41% 10.2M 26s
208000K .......... .......... .......... .......... .......... 41% 13.9M 26s
208050K .......... .......... .......... .......... .......... 41% 12.1M 26s
208100K .......... .......... .......... .......... .......... 41% 7.72M 26s
208150K .......... .......... .......... .......... .......... 41% 8.85M 26s
208200K .......... .......... .......... .......... .......... 41% 9.16M 26s
208250K .......... .......... .......... .......... .......... 41% 18.7M 26s
208300K .......... .......... .......... .......... .......... 41% 14.5M 26s
208350K .......... .......... .......... .......... .......... 41% 11.0M 26s
208400K .......... .......... .......... .......... .......... 41% 10.6M 25s
208450K .......... .......... .......... .......... .......... 41% 8.04M 25s
208500K .......... .......... .......... .......... .......... 41% 9.45M 25s
208550K .......... .......... .......... .......... .......... 41% 8.73M 25s
208600K .......... .......... .......... .......... .......... 41% 5.85M 25s
208650K .......... .......... .......... .......... .......... 41% 9.83M 25s
208700K .......... .......... .......... .......... .......... 41% 8.03M 25s
208750K .......... .......... .......... .......... .......... 41% 10.2M 25s
208800K .......... .......... .......... .......... .......... 41% 6.03M 25s
208850K .......... .......... .......... .......... .......... 41% 8.36M 25s
208900K .......... .......... .......... .......... .......... 41% 7.55M 25s
208950K .......... .......... .......... .......... .......... 41% 9.21M 25s
209000K .......... .......... .......... .......... .......... 41% 10.6M 25s
209050K .......... .......... .......... .......... .......... 41% 9.52M 25s
209100K .......... .......... .......... .......... .......... 41% 8.43M 25s
209150K .......... .......... .......... .......... .......... 41% 10.2M 25s
209200K .......... .......... .......... .......... .......... 41% 9.01M 25s
209250K .......... .......... .......... .......... .......... 41% 16.8M 25s
209300K .......... .......... .......... .......... .......... 41% 16.2M 25s
209350K .......... .......... .......... .......... .......... 41% 28.0M 25s
209400K .......... .......... .......... .......... .......... 41% 28.5M 25s
209450K .......... .......... .......... .......... .......... 41% 17.7M 25s
209500K .......... .......... .......... .......... .......... 41% 26.8M 25s
209550K .......... .......... .......... .......... .......... 41% 18.5M 25s
209600K .......... .......... .......... .......... .......... 41% 23.4M 25s
209650K .......... .......... .......... .......... .......... 41% 28.8M 25s
209700K .......... .......... .......... .......... .......... 41% 23.4M 25s
209750K .......... .......... .......... .......... .......... 41% 23.6M 25s
209800K .......... .......... .......... .......... .......... 41% 20.7M 25s
209850K .......... .......... .......... .......... .......... 41% 20.6M 25s
209900K .......... .......... .......... .......... .......... 41% 28.6M 25s
209950K .......... .......... .......... .......... .......... 41% 11.5M 25s
210000K .......... .......... .......... .......... .......... 41% 45.8M 25s
210050K .......... .......... .......... .......... .......... 41% 26.9M 25s
210100K .......... .......... .......... .......... .......... 41% 15.0M 25s
210150K .......... .......... .......... .......... .......... 41% 19.7M 25s
210200K .......... .......... .......... .......... .......... 41% 9.69M 25s
210250K .......... .......... .......... .......... .......... 41% 16.2M 25s
210300K .......... .......... .......... .......... .......... 41% 12.5M 25s
210350K .......... .......... .......... .......... .......... 41% 10.7M 25s
210400K .......... .......... .......... .......... .......... 41% 12.1M 25s
210450K .......... .......... .......... .......... .......... 41% 7.01M 25s
210500K .......... .......... .......... .......... .......... 41% 7.28M 25s
210550K .......... .......... .......... .......... .......... 41% 6.54M 25s
210600K .......... .......... .......... .......... .......... 41% 6.02M 25s
210650K .......... .......... .......... .......... .......... 41% 16.2M 25s
210700K .......... .......... .......... .......... .......... 41% 13.6M 25s
210750K .......... .......... .......... .......... .......... 41% 14.0M 25s
210800K .......... .......... .......... .......... .......... 41% 14.5M 25s
210850K .......... .......... .......... .......... .......... 41% 11.0M 25s
210900K .......... .......... .......... .......... .......... 41% 10.4M 25s
210950K .......... .......... .......... .......... .......... 41% 7.41M 25s
211000K .......... .......... .......... .......... .......... 41% 12.7M 25s
211050K .......... .......... .......... .......... .......... 41% 17.1M 25s
211100K .......... .......... .......... .......... .......... 41% 9.74M 25s
211150K .......... .......... .......... .......... .......... 41% 8.20M 25s
211200K .......... .......... .......... .......... .......... 41% 9.92M 25s
211250K .......... .......... .......... .......... .......... 41% 13.9M 25s
211300K .......... .......... .......... .......... .......... 41% 9.70M 25s
211350K .......... .......... .......... .......... .......... 41% 8.22M 25s
211400K .......... .......... .......... .......... .......... 41% 8.74M 25s
211450K .......... .......... .......... .......... .......... 41% 7.28M 25s
211500K .......... .......... .......... .......... .......... 42% 8.57M 25s
211550K .......... .......... .......... .......... .......... 42% 8.28M 25s
211600K .......... .......... .......... .......... .......... 42% 6.36M 25s
211650K .......... .......... .......... .......... .......... 42% 9.46M 25s
211700K .......... .......... .......... .......... .......... 42% 9.22M 25s
211750K .......... .......... .......... .......... .......... 42% 7.53M 25s
211800K .......... .......... .......... .......... .......... 42% 7.08M 25s
211850K .......... .......... .......... .......... .......... 42% 4.89M 25s
211900K .......... .......... .......... .......... .......... 42% 7.28M 25s
211950K .......... .......... .......... .......... .......... 42% 7.16M 25s
212000K .......... .......... .......... .......... .......... 42% 9.21M 25s
212050K .......... .......... .......... .......... .......... 42% 8.27M 25s
212100K .......... .......... .......... .......... .......... 42% 6.30M 25s
212150K .......... .......... .......... .......... .......... 42% 5.83M 25s
212200K .......... .......... .......... .......... .......... 42% 5.51M 25s
212250K .......... .......... .......... .......... .......... 42% 5.88M 25s
212300K .......... .......... .......... .......... .......... 42% 4.69M 25s
212350K .......... .......... .......... .......... .......... 42% 4.78M 25s
212400K .......... .......... .......... .......... .......... 42% 5.43M 25s
212450K .......... .......... .......... .......... .......... 42% 4.24M 25s
212500K .......... .......... .......... .......... .......... 42% 6.82M 25s
212550K .......... .......... .......... .......... .......... 42% 25.6M 25s
212600K .......... .......... .......... .......... .......... 42% 18.7M 25s
212650K .......... .......... .......... .......... .......... 42% 22.2M 25s
212700K .......... .......... .......... .......... .......... 42% 21.0M 25s
212750K .......... .......... .......... .......... .......... 42% 23.8M 25s
212800K .......... .......... .......... .......... .......... 42% 21.5M 25s
212850K .......... .......... .......... .......... .......... 42% 15.8M 25s
212900K .......... .......... .......... .......... .......... 42% 14.1M 25s
212950K .......... .......... .......... .......... .......... 42% 9.38M 25s
213000K .......... .......... .......... .......... .......... 42% 17.3M 25s
213050K .......... .......... .......... .......... .......... 42% 12.6M 25s
213100K .......... .......... .......... .......... .......... 42% 11.2M 25s
213150K .......... .......... .......... .......... .......... 42% 10.2M 25s
213200K .......... .......... .......... .......... .......... 42% 8.50M 25s
213250K .......... .......... .......... .......... .......... 42% 9.47M 25s
213300K .......... .......... .......... .......... .......... 42% 13.0M 25s
213350K .......... .......... .......... .......... .......... 42% 28.7M 25s
213400K .......... .......... .......... .......... .......... 42% 26.8M 25s
213450K .......... .......... .......... .......... .......... 42% 12.6M 25s
213500K .......... .......... .......... .......... .......... 42% 12.1M 25s
213550K .......... .......... .......... .......... .......... 42% 11.8M 25s
213600K .......... .......... .......... .......... .......... 42% 10.4M 25s
213650K .......... .......... .......... .......... .......... 42% 7.57M 25s
213700K .......... .......... .......... .......... .......... 42% 6.64M 25s
213750K .......... .......... .......... .......... .......... 42% 10.0M 25s
213800K .......... .......... .......... .......... .......... 42% 8.05M 25s
213850K .......... .......... .......... .......... .......... 42% 6.75M 25s
213900K .......... .......... .......... .......... .......... 42% 9.24M 25s
213950K .......... .......... .......... .......... .......... 42% 8.04M 25s
214000K .......... .......... .......... .......... .......... 42% 8.39M 25s
214050K .......... .......... .......... .......... .......... 42% 13.0M 25s
214100K .......... .......... .......... .......... .......... 42% 26.9M 25s
214150K .......... .......... .......... .......... .......... 42% 27.2M 25s
214200K .......... .......... .......... .......... .......... 42% 18.5M 25s
214250K .......... .......... .......... .......... .......... 42% 15.6M 25s
214300K .......... .......... .......... .......... .......... 42% 16.4M 25s
214350K .......... .......... .......... .......... .......... 42% 12.5M 25s
214400K .......... .......... .......... .......... .......... 42%  230K 25s
214450K .......... .......... .......... .......... .......... 42% 9.64M 25s
214500K .......... .......... .......... .......... .......... 42% 17.2M 25s
214550K .......... .......... .......... .......... .......... 42% 13.5M 25s
214600K .......... .......... .......... .......... .......... 42% 11.0M 25s
214650K .......... .......... .......... .......... .......... 42% 41.9M 25s
214700K .......... .......... .......... .......... .......... 42% 15.2M 25s
214750K .......... .......... .......... .......... .......... 42% 16.8M 25s
214800K .......... .......... .......... .......... .......... 42% 18.1M 25s
214850K .......... .......... .......... .......... .......... 42% 8.66M 25s
214900K .......... .......... .......... .......... .......... 42% 9.99M 25s
214950K .......... .......... .......... .......... .......... 42% 11.5M 25s
215000K .......... .......... .......... .......... .......... 42% 7.67M 25s
215050K .......... .......... .......... .......... .......... 42% 18.2M 25s
215100K .......... .......... .......... .......... .......... 42% 17.0M 25s
215150K .......... .......... .......... .......... .......... 42% 19.4M 25s
215200K .......... .......... .......... .......... .......... 42% 13.8M 25s
215250K .......... .......... .......... .......... .......... 42% 21.8M 25s
215300K .......... .......... .......... .......... .......... 42% 16.3M 25s
215350K .......... .......... .......... .......... .......... 42% 17.8M 25s
215400K .......... .......... .......... .......... .......... 42% 17.8M 25s
215450K .......... .......... .......... .......... .......... 42% 17.5M 25s
215500K .......... .......... .......... .......... .......... 42% 16.0M 25s
215550K .......... .......... .......... .......... .......... 42% 14.9M 25s
215600K .......... .......... .......... .......... .......... 42% 13.3M 25s
215650K .......... .......... .......... .......... .......... 42% 13.4M 25s
215700K .......... .......... .......... .......... .......... 42% 78.0M 25s
215750K .......... .......... .......... .......... .......... 42% 83.8M 25s
215800K .......... .......... .......... .......... .......... 42% 39.8M 25s
215850K .......... .......... .......... .......... .......... 42% 26.7M 25s
215900K .......... .......... .......... .......... .......... 42% 16.2M 25s
215950K .......... .......... .......... .......... .......... 42% 19.4M 25s
216000K .......... .......... .......... .......... .......... 42% 15.2M 25s
216050K .......... .......... .......... .......... .......... 42% 42.6M 25s
216100K .......... .......... .......... .......... .......... 42% 18.6M 25s
216150K .......... .......... .......... .......... .......... 42% 15.4M 25s
216200K .......... .......... .......... .......... .......... 42% 13.2M 25s
216250K .......... .......... .......... .......... .......... 42% 19.3M 25s
216300K .......... .......... .......... .......... .......... 42% 14.3M 25s
216350K .......... .......... .......... .......... .......... 42% 13.4M 25s
216400K .......... .......... .......... .......... .......... 42% 18.7M 25s
216450K .......... .......... .......... .......... .......... 42% 10.6M 25s
216500K .......... .......... .......... .......... .......... 43% 8.79M 25s
216550K .......... .......... .......... .......... .......... 43% 11.1M 25s
216600K .......... .......... .......... .......... .......... 43% 13.3M 25s
216650K .......... .......... .......... .......... .......... 43% 13.2M 25s
216700K .......... .......... .......... .......... .......... 43% 11.0M 25s
216750K .......... .......... .......... .......... .......... 43% 12.5M 25s
216800K .......... .......... .......... .......... .......... 43% 13.4M 25s
216850K .......... .......... .......... .......... .......... 43% 10.9M 25s
216900K .......... .......... .......... .......... .......... 43% 13.5M 25s
216950K .......... .......... .......... .......... .......... 43% 13.5M 25s
217000K .......... .......... .......... .......... .......... 43% 30.1M 25s
217050K .......... .......... .......... .......... .......... 43% 35.1M 25s
217100K .......... .......... .......... .......... .......... 43% 16.1M 25s
217150K .......... .......... .......... .......... .......... 43% 24.3M 25s
217200K .......... .......... .......... .......... .......... 43% 8.99M 25s
217250K .......... .......... .......... .......... .......... 43% 86.9M 25s
217300K .......... .......... .......... .......... .......... 43% 16.3M 25s
217350K .......... .......... .......... .......... .......... 43% 16.4M 25s
217400K .......... .......... .......... .......... .......... 43% 23.1M 25s
217450K .......... .......... .......... .......... .......... 43% 9.97M 25s
217500K .......... .......... .......... .......... .......... 43% 12.4M 25s
217550K .......... .......... .......... .......... .......... 43% 8.40M 25s
217600K .......... .......... .......... .......... .......... 43% 8.01M 25s
217650K .......... .......... .......... .......... .......... 43% 9.98M 25s
217700K .......... .......... .......... .......... .......... 43% 8.29M 25s
217750K .......... .......... .......... .......... .......... 43% 11.5M 25s
217800K .......... .......... .......... .......... .......... 43% 6.50M 25s
217850K .......... .......... .......... .......... .......... 43% 4.86M 25s
217900K .......... .......... .......... .......... .......... 43% 5.24M 25s
217950K .......... .......... .......... .......... .......... 43% 5.02M 25s
218000K .......... .......... .......... .......... .......... 43% 10.5M 25s
218050K .......... .......... .......... .......... .......... 43% 10.8M 25s
218100K .......... .......... .......... .......... .......... 43% 7.99M 25s
218150K .......... .......... .......... .......... .......... 43% 8.70M 25s
218200K .......... .......... .......... .......... .......... 43% 6.31M 25s
218250K .......... .......... .......... .......... .......... 43% 9.43M 25s
218300K .......... .......... .......... .......... .......... 43% 4.85M 25s
218350K .......... .......... .......... .......... .......... 43% 7.11M 25s
218400K .......... .......... .......... .......... .......... 43% 9.19M 25s
218450K .......... .......... .......... .......... .......... 43% 7.49M 25s
218500K .......... .......... .......... .......... .......... 43% 8.53M 25s
218550K .......... .......... .......... .......... .......... 43% 9.87M 25s
218600K .......... .......... .......... .......... .......... 43% 6.37M 25s
218650K .......... .......... .......... .......... .......... 43% 16.2M 25s
218700K .......... .......... .......... .......... .......... 43% 30.9M 25s
218750K .......... .......... .......... .......... .......... 43% 19.0M 25s
218800K .......... .......... .......... .......... .......... 43% 36.7M 25s
218850K .......... .......... .......... .......... .......... 43% 21.9M 25s
218900K .......... .......... .......... .......... .......... 43% 34.0M 25s
218950K .......... .......... .......... .......... .......... 43% 27.0M 25s
219000K .......... .......... .......... .......... .......... 43% 27.8M 25s
219050K .......... .......... .......... .......... .......... 43% 15.9M 25s
219100K .......... .......... .......... .......... .......... 43% 77.3M 25s
219150K .......... .......... .......... .......... .......... 43% 26.0M 25s
219200K .......... .......... .......... .......... .......... 43% 16.1M 25s
219250K .......... .......... .......... .......... .......... 43% 16.9M 25s
219300K .......... .......... .......... .......... .......... 43% 17.0M 25s
219350K .......... .......... .......... .......... .......... 43% 10.7M 25s
219400K .......... .......... .......... .......... .......... 43% 13.6M 25s
219450K .......... .......... .......... .......... .......... 43% 7.83M 25s
219500K .......... .......... .......... .......... .......... 43% 7.13M 25s
219550K .......... .......... .......... .......... .......... 43% 5.53M 25s
219600K .......... .......... .......... .......... .......... 43% 5.06M 25s
219650K .......... .......... .......... .......... .......... 43% 6.49M 25s
219700K .......... .......... .......... .......... .......... 43% 5.75M 25s
219750K .......... .......... .......... .......... .......... 43% 10.1M 25s
219800K .......... .......... .......... .......... .......... 43% 8.63M 25s
219850K .......... .......... .......... .......... .......... 43% 5.61M 25s
219900K .......... .......... .......... .......... .......... 43% 8.46M 25s
219950K .......... .......... .......... .......... .......... 43% 5.75M 25s
220000K .......... .......... .......... .......... .......... 43% 6.66M 25s
220050K .......... .......... .......... .......... .......... 43% 3.47M 25s
220100K .......... .......... .......... .......... .......... 43% 3.48M 25s
220150K .......... .......... .......... .......... .......... 43% 5.75M 25s
220200K .......... .......... .......... .......... .......... 43% 4.41M 25s
220250K .......... .......... .......... .......... .......... 43% 4.84M 25s
220300K .......... .......... .......... .......... .......... 43% 6.33M 25s
220350K .......... .......... .......... .......... .......... 43% 8.68M 25s
220400K .......... .......... .......... .......... .......... 43% 7.14M 25s
220450K .......... .......... .......... .......... .......... 43% 13.6M 25s
220500K .......... .......... .......... .......... .......... 43% 11.0M 25s
220550K .......... .......... .......... .......... .......... 43% 13.0M 25s
220600K .......... .......... .......... .......... .......... 43% 13.4M 25s
220650K .......... .......... .......... .......... .......... 43% 11.0M 25s
220700K .......... .......... .......... .......... .......... 43% 9.34M 25s
220750K .......... .......... .......... .......... .......... 43% 15.4M 25s
220800K .......... .......... .......... .......... .......... 43% 9.00M 25s
220850K .......... .......... .......... .......... .......... 43% 8.36M 25s
220900K .......... .......... .......... .......... .......... 43% 17.9M 25s
220950K .......... .......... .......... .......... .......... 43% 9.53M 25s
221000K .......... .......... .......... .......... .......... 43% 12.8M 25s
221050K .......... .......... .......... .......... .......... 43% 10.3M 25s
221100K .......... .......... .......... .......... .......... 43% 8.72M 25s
221150K .......... .......... .......... .......... .......... 43% 6.86M 25s
221200K .......... .......... .......... .......... .......... 43% 6.89M 25s
221250K .......... .......... .......... .......... .......... 43% 12.1M 25s
221300K .......... .......... .......... .......... .......... 43% 11.4M 25s
221350K .......... .......... .......... .......... .......... 43% 6.76M 25s
221400K .......... .......... .......... .......... .......... 43% 19.8M 25s
221450K .......... .......... .......... .......... .......... 43% 12.3M 25s
221500K .......... .......... .......... .......... .......... 43% 14.7M 25s
221550K .......... .......... .......... .......... .......... 44% 15.4M 25s
221600K .......... .......... .......... .......... .......... 44% 13.1M 25s
221650K .......... .......... .......... .......... .......... 44% 13.1M 25s
221700K .......... .......... .......... .......... .......... 44% 26.4M 25s
221750K .......... .......... .......... .......... .......... 44% 14.5M 25s
221800K .......... .......... .......... .......... .......... 44% 17.7M 25s
221850K .......... .......... .......... .......... .......... 44% 10.9M 25s
221900K .......... .......... .......... .......... .......... 44% 12.0M 25s
221950K .......... .......... .......... .......... .......... 44% 7.46M 25s
222000K .......... .......... .......... .......... .......... 44% 11.9M 25s
222050K .......... .......... .......... .......... .......... 44% 16.3M 25s
222100K .......... .......... .......... .......... .......... 44% 13.4M 25s
222150K .......... .......... .......... .......... .......... 44% 11.4M 25s
222200K .......... .......... .......... .......... .......... 44% 7.80M 25s
222250K .......... .......... .......... .......... .......... 44% 9.15M 25s
222300K .......... .......... .......... .......... .......... 44% 7.96M 25s
222350K .......... .......... .......... .......... .......... 44% 8.37M 25s
222400K .......... .......... .......... .......... .......... 44% 6.49M 25s
222450K .......... .......... .......... .......... .......... 44% 6.35M 25s
222500K .......... .......... .......... .......... .......... 44% 7.82M 25s
222550K .......... .......... .......... .......... .......... 44% 7.74M 25s
222600K .......... .......... .......... .......... .......... 44% 6.57M 25s
222650K .......... .......... .......... .......... .......... 44% 9.68M 25s
222700K .......... .......... .......... .......... .......... 44% 9.21M 25s
222750K .......... .......... .......... .......... .......... 44% 17.3M 25s
222800K .......... .......... .......... .......... .......... 44% 9.12M 25s
222850K .......... .......... .......... .......... .......... 44% 23.9M 25s
222900K .......... .......... .......... .......... .......... 44% 14.4M 25s
222950K .......... .......... .......... .......... .......... 44% 11.1M 25s
223000K .......... .......... .......... .......... .......... 44% 14.1M 25s
223050K .......... .......... .......... .......... .......... 44% 14.8M 25s
223100K .......... .......... .......... .......... .......... 44% 16.6M 25s
223150K .......... .......... .......... .......... .......... 44% 15.0M 25s
223200K .......... .......... .......... .......... .......... 44% 13.6M 25s
223250K .......... .......... .......... .......... .......... 44% 12.2M 25s
223300K .......... .......... .......... .......... .......... 44% 20.5M 25s
223350K .......... .......... .......... .......... .......... 44% 7.71M 25s
223400K .......... .......... .......... .......... .......... 44% 16.4M 25s
223450K .......... .......... .......... .......... .......... 44% 13.0M 25s
223500K .......... .......... .......... .......... .......... 44% 12.9M 25s
223550K .......... .......... .......... .......... .......... 44% 13.8M 25s
223600K .......... .......... .......... .......... .......... 44% 7.98M 25s
223650K .......... .......... .......... .......... .......... 44% 13.4M 25s
223700K .......... .......... .......... .......... .......... 44% 6.98M 25s
223750K .......... .......... .......... .......... .......... 44% 7.85M 25s
223800K .......... .......... .......... .......... .......... 44% 6.69M 25s
223850K .......... .......... .......... .......... .......... 44% 5.46M 25s
223900K .......... .......... .......... .......... .......... 44% 5.82M 25s
223950K .......... .......... .......... .......... .......... 44% 6.91M 25s
224000K .......... .......... .......... .......... .......... 44% 14.6M 25s
224050K .......... .......... .......... .......... .......... 44% 24.3M 25s
224100K .......... .......... .......... .......... .......... 44% 14.1M 25s
224150K .......... .......... .......... .......... .......... 44% 10.7M 25s
224200K .......... .......... .......... .......... .......... 44% 24.0M 25s
224250K .......... .......... .......... .......... .......... 44% 13.0M 25s
224300K .......... .......... .......... .......... .......... 44% 14.0M 25s
224350K .......... .......... .......... .......... .......... 44% 15.6M 25s
224400K .......... .......... .......... .......... .......... 44% 11.7M 25s
224450K .......... .......... .......... .......... .......... 44% 8.33M 25s
224500K .......... .......... .......... .......... .......... 44% 9.84M 25s
224550K .......... .......... .......... .......... .......... 44% 8.72M 25s
224600K .......... .......... .......... .......... .......... 44% 6.66M 24s
224650K .......... .......... .......... .......... .......... 44% 8.66M 24s
224700K .......... .......... .......... .......... .......... 44% 7.43M 24s
224750K .......... .......... .......... .......... .......... 44% 7.41M 24s
224800K .......... .......... .......... .......... .......... 44% 9.06M 24s
224850K .......... .......... .......... .......... .......... 44% 13.7M 24s
224900K .......... .......... .......... .......... .......... 44% 9.88M 24s
224950K .......... .......... .......... .......... .......... 44% 34.4M 24s
225000K .......... .......... .......... .......... .......... 44% 17.7M 24s
225050K .......... .......... .......... .......... .......... 44% 15.4M 24s
225100K .......... .......... .......... .......... .......... 44% 15.3M 24s
225150K .......... .......... .......... .......... .......... 44% 14.3M 24s
225200K .......... .......... .......... .......... .......... 44% 11.4M 24s
225250K .......... .......... .......... .......... .......... 44% 13.8M 24s
225300K .......... .......... .......... .......... .......... 44% 11.5M 24s
225350K .......... .......... .......... .......... .......... 44% 8.64M 24s
225400K .......... .......... .......... .......... .......... 44% 8.42M 24s
225450K .......... .......... .......... .......... .......... 44% 10.5M 24s
225500K .......... .......... .......... .......... .......... 44% 6.90M 24s
225550K .......... .......... .......... .......... .......... 44% 7.30M 24s
225600K .......... .......... .......... .......... .......... 44% 5.57M 24s
225650K .......... .......... .......... .......... .......... 44% 11.9M 24s
225700K .......... .......... .......... .......... .......... 44% 5.97M 24s
225750K .......... .......... .......... .......... .......... 44% 7.41M 24s
225800K .......... .......... .......... .......... .......... 44% 4.21M 24s
225850K .......... .......... .......... .......... .......... 44% 4.40M 24s
225900K .......... .......... .......... .......... .......... 44% 8.47M 24s
225950K .......... .......... .......... .......... .......... 44% 6.83M 24s
226000K .......... .......... .......... .......... .......... 44% 12.8M 24s
226050K .......... .......... .......... .......... .......... 44% 14.0M 24s
226100K .......... .......... .......... .......... .......... 44% 17.3M 24s
226150K .......... .......... .......... .......... .......... 44% 28.9M 24s
226200K .......... .......... .......... .......... .......... 44% 15.7M 24s
226250K .......... .......... .......... .......... .......... 44% 15.5M 24s
226300K .......... .......... .......... .......... .......... 44% 14.9M 24s
226350K .......... .......... .......... .......... .......... 44% 15.7M 24s
226400K .......... .......... .......... .......... .......... 44% 12.6M 24s
226450K .......... .......... .......... .......... .......... 44% 17.0M 24s
226500K .......... .......... .......... .......... .......... 44% 11.8M 24s
226550K .......... .......... .......... .......... .......... 44% 10.9M 24s
226600K .......... .......... .......... .......... .......... 45% 6.48M 24s
226650K .......... .......... .......... .......... .......... 45% 17.2M 24s
226700K .......... .......... .......... .......... .......... 45% 9.68M 24s
226750K .......... .......... .......... .......... .......... 45% 12.2M 24s
226800K .......... .......... .......... .......... .......... 45% 12.0M 24s
226850K .......... .......... .......... .......... .......... 45% 8.68M 24s
226900K .......... .......... .......... .......... .......... 45% 11.0M 24s
226950K .......... .......... .......... .......... .......... 45% 6.51M 24s
227000K .......... .......... .......... .......... .......... 45% 11.4M 24s
227050K .......... .......... .......... .......... .......... 45% 8.38M 24s
227100K .......... .......... .......... .......... .......... 45% 8.52M 24s
227150K .......... .......... .......... .......... .......... 45% 10.3M 24s
227200K .......... .......... .......... .......... .......... 45% 7.04M 24s
227250K .......... .......... .......... .......... .......... 45% 9.30M 24s
227300K .......... .......... .......... .......... .......... 45% 7.05M 24s
227350K .......... .......... .......... .......... .......... 45% 9.36M 24s
227400K .......... .......... .......... .......... .......... 45% 6.67M 24s
227450K .......... .......... .......... .......... .......... 45% 6.10M 24s
227500K .......... .......... .......... .......... .......... 45% 6.38M 24s
227550K .......... .......... .......... .......... .......... 45% 7.64M 24s
227600K .......... .......... .......... .......... .......... 45% 16.4M 24s
227650K .......... .......... .......... .......... .......... 45% 16.3M 24s
227700K .......... .......... .......... .......... .......... 45% 13.5M 24s
227750K .......... .......... .......... .......... .......... 45% 19.6M 24s
227800K .......... .......... .......... .......... .......... 45% 19.0M 24s
227850K .......... .......... .......... .......... .......... 45% 18.0M 24s
227900K .......... .......... .......... .......... .......... 45% 18.0M 24s
227950K .......... .......... .......... .......... .......... 45% 13.8M 24s
228000K .......... .......... .......... .......... .......... 45% 18.1M 24s
228050K .......... .......... .......... .......... .......... 45% 16.6M 24s
228100K .......... .......... .......... .......... .......... 45% 18.3M 24s
228150K .......... .......... .......... .......... .......... 45% 17.3M 24s
228200K .......... .......... .......... .......... .......... 45% 14.5M 24s
228250K .......... .......... .......... .......... .......... 45% 16.6M 24s
228300K .......... .......... .......... .......... .......... 45% 19.1M 24s
228350K .......... .......... .......... .......... .......... 45% 22.1M 24s
228400K .......... .......... .......... .......... .......... 45% 49.1M 24s
228450K .......... .......... .......... .......... .......... 45% 29.0M 24s
228500K .......... .......... .......... .......... .......... 45% 15.9M 24s
228550K .......... .......... .......... .......... .......... 45% 50.2M 24s
228600K .......... .......... .......... .......... .......... 45% 28.3M 24s
228650K .......... .......... .......... .......... .......... 45% 74.9M 24s
228700K .......... .......... .......... .......... .......... 45% 24.9M 24s
228750K .......... .......... .......... .......... .......... 45% 34.0M 24s
228800K .......... .......... .......... .......... .......... 45% 27.6M 24s
228850K .......... .......... .......... .......... .......... 45% 26.6M 24s
228900K .......... .......... .......... .......... .......... 45% 23.7M 24s
228950K .......... .......... .......... .......... .......... 45% 27.8M 24s
229000K .......... .......... .......... .......... .......... 45% 26.9M 24s
229050K .......... .......... .......... .......... .......... 45% 25.3M 24s
229100K .......... .......... .......... .......... .......... 45% 19.0M 24s
229150K .......... .......... .......... .......... .......... 45% 30.0M 24s
229200K .......... .......... .......... .......... .......... 45% 17.9M 24s
229250K .......... .......... .......... .......... .......... 45% 30.3M 24s
229300K .......... .......... .......... .......... .......... 45% 27.9M 24s
229350K .......... .......... .......... .......... .......... 45% 12.6M 24s
229400K .......... .......... .......... .......... .......... 45% 27.2M 24s
229450K .......... .......... .......... .......... .......... 45% 17.8M 24s
229500K .......... .......... .......... .......... .......... 45% 27.1M 24s
229550K .......... .......... .......... .......... .......... 45% 19.3M 24s
229600K .......... .......... .......... .......... .......... 45% 12.2M 24s
229650K .......... .......... .......... .......... .......... 45% 14.8M 24s
229700K .......... .......... .......... .......... .......... 45% 72.0M 24s
229750K .......... .......... .......... .......... .......... 45% 16.4M 24s
229800K .......... .......... .......... .......... .......... 45% 17.1M 24s
229850K .......... .......... .......... .......... .......... 45% 9.96M 24s
229900K .......... .......... .......... .......... .......... 45% 12.2M 24s
229950K .......... .......... .......... .......... .......... 45% 20.9M 24s
230000K .......... .......... .......... .......... .......... 45% 11.1M 24s
230050K .......... .......... .......... .......... .......... 45% 12.4M 24s
230100K .......... .......... .......... .......... .......... 45% 13.9M 24s
230150K .......... .......... .......... .......... .......... 45% 13.4M 24s
230200K .......... .......... .......... .......... .......... 45% 9.59M 24s
230250K .......... .......... .......... .......... .......... 45% 15.2M 24s
230300K .......... .......... .......... .......... .......... 45% 13.5M 24s
230350K .......... .......... .......... .......... .......... 45% 10.3M 24s
230400K .......... .......... .......... .......... .......... 45% 12.2M 24s
230450K .......... .......... .......... .......... .......... 45% 12.1M 24s
230500K .......... .......... .......... .......... .......... 45% 18.6M 24s
230550K .......... .......... .......... .......... .......... 45% 27.6M 24s
230600K .......... .......... .......... .......... .......... 45% 25.4M 24s
230650K .......... .......... .......... .......... .......... 45% 30.1M 24s
230700K .......... .......... .......... .......... .......... 45% 30.8M 24s
230750K .......... .......... .......... .......... .......... 45% 22.9M 24s
230800K .......... .......... .......... .......... .......... 45% 84.3M 24s
230850K .......... .......... .......... .......... .......... 45% 20.9M 24s
230900K .......... .......... .......... .......... .......... 45% 55.5M 24s
230950K .......... .......... .......... .......... .......... 45% 14.3M 24s
231000K .......... .......... .......... .......... .......... 45% 13.5M 24s
231050K .......... .......... .......... .......... .......... 45% 9.96M 24s
231100K .......... .......... .......... .......... .......... 45% 5.46M 24s
231150K .......... .......... .......... .......... .......... 45% 10.4M 24s
231200K .......... .......... .......... .......... .......... 45% 6.76M 24s
231250K .......... .......... .......... .......... .......... 45% 5.95M 24s
231300K .......... .......... .......... .......... .......... 45% 5.94M 24s
231350K .......... .......... .......... .......... .......... 45% 5.02M 24s
231400K .......... .......... .......... .......... .......... 45% 4.78M 24s
231450K .......... .......... .......... .......... .......... 45% 6.36M 24s
231500K .......... .......... .......... .......... .......... 45% 10.6M 24s
231550K .......... .......... .......... .......... .......... 45% 11.1M 24s
231600K .......... .......... .......... .......... .......... 45% 9.02M 24s
231650K .......... .......... .......... .......... .......... 46% 9.26M 24s
231700K .......... .......... .......... .......... .......... 46% 6.20M 24s
231750K .......... .......... .......... .......... .......... 46% 10.2M 24s
231800K .......... .......... .......... .......... .......... 46% 9.19M 24s
231850K .......... .......... .......... .......... .......... 46% 7.07M 24s
231900K .......... .......... .......... .......... .......... 46% 5.78M 24s
231950K .......... .......... .......... .......... .......... 46% 6.63M 24s
232000K .......... .......... .......... .......... .......... 46% 6.66M 24s
232050K .......... .......... .......... .......... .......... 46% 3.48M 24s
232100K .......... .......... .......... .......... .......... 46% 2.92M 24s
232150K .......... .......... .......... .......... .......... 46% 5.19M 24s
232200K .......... .......... .......... .......... .......... 46% 17.7M 24s
232250K .......... .......... .......... .......... .......... 46% 27.1M 24s
232300K .......... .......... .......... .......... .......... 46% 22.7M 24s
232350K .......... .......... .......... .......... .......... 46% 13.0M 24s
232400K .......... .......... .......... .......... .......... 46% 7.90M 24s
232450K .......... .......... .......... .......... .......... 46% 68.6M 24s
232500K .......... .......... .......... .......... .......... 46% 29.5M 24s
232550K .......... .......... .......... .......... .......... 46% 32.8M 24s
232600K .......... .......... .......... .......... .......... 46% 26.0M 24s
232650K .......... .......... .......... .......... .......... 46% 18.9M 24s
232700K .......... .......... .......... .......... .......... 46% 25.3M 24s
232750K .......... .......... .......... .......... .......... 46% 17.7M 24s
232800K .......... .......... .......... .......... .......... 46% 55.9M 24s
232850K .......... .......... .......... .......... .......... 46% 17.0M 24s
232900K .......... .......... .......... .......... .......... 46% 16.4M 24s
232950K .......... .......... .......... .......... .......... 46% 14.9M 24s
233000K .......... .......... .......... .......... .......... 46% 15.0M 24s
233050K .......... .......... .......... .......... .......... 46% 17.0M 24s
233100K .......... .......... .......... .......... .......... 46% 15.2M 24s
233150K .......... .......... .......... .......... .......... 46% 15.4M 24s
233200K .......... .......... .......... .......... .......... 46% 14.4M 24s
233250K .......... .......... .......... .......... .......... 46% 18.3M 24s
233300K .......... .......... .......... .......... .......... 46% 14.9M 24s
233350K .......... .......... .......... .......... .......... 46% 13.9M 24s
233400K .......... .......... .......... .......... .......... 46% 14.3M 24s
233450K .......... .......... .......... .......... .......... 46% 14.2M 24s
233500K .......... .......... .......... .......... .......... 46% 13.0M 24s
233550K .......... .......... .......... .......... .......... 46% 13.9M 24s
233600K .......... .......... .......... .......... .......... 46% 13.7M 24s
233650K .......... .......... .......... .......... .......... 46% 31.6M 24s
233700K .......... .......... .......... .......... .......... 46% 25.1M 24s
233750K .......... .......... .......... .......... .......... 46% 95.7M 24s
233800K .......... .......... .......... .......... .......... 46% 19.4M 24s
233850K .......... .......... .......... .......... .......... 46% 7.66M 24s
233900K .......... .......... .......... .......... .......... 46% 86.0M 24s
233950K .......... .......... .......... .......... .......... 46% 73.5M 24s
234000K .......... .......... .......... .......... .......... 46% 13.3M 24s
234050K .......... .......... .......... .......... .......... 46% 21.8M 24s
234100K .......... .......... .......... .......... .......... 46% 20.6M 24s
234150K .......... .......... .......... .......... .......... 46% 20.7M 24s
234200K .......... .......... .......... .......... .......... 46% 11.8M 24s
234250K .......... .......... .......... .......... .......... 46% 16.4M 24s
234300K .......... .......... .......... .......... .......... 46% 18.5M 24s
234350K .......... .......... .......... .......... .......... 46% 10.6M 24s
234400K .......... .......... .......... .......... .......... 46% 17.7M 24s
234450K .......... .......... .......... .......... .......... 46% 10.2M 24s
234500K .......... .......... .......... .......... .......... 46% 14.9M 24s
234550K .......... .......... .......... .......... .......... 46% 13.3M 24s
234600K .......... .......... .......... .......... .......... 46% 12.1M 24s
234650K .......... .......... .......... .......... .......... 46% 15.3M 24s
234700K .......... .......... .......... .......... .......... 46% 14.0M 24s
234750K .......... .......... .......... .......... .......... 46% 12.6M 24s
234800K .......... .......... .......... .......... .......... 46% 15.7M 24s
234850K .......... .......... .......... .......... .......... 46% 9.98M 24s
234900K .......... .......... .......... .......... .......... 46% 12.6M 24s
234950K .......... .......... .......... .......... .......... 46% 9.71M 24s
235000K .......... .......... .......... .......... .......... 46% 13.9M 23s
235050K .......... .......... .......... .......... .......... 46% 10.2M 23s
235100K .......... .......... .......... .......... .......... 46% 9.71M 23s
235150K .......... .......... .......... .......... .......... 46% 17.1M 23s
235200K .......... .......... .......... .......... .......... 46% 16.2M 23s
235250K .......... .......... .......... .......... .......... 46% 10.5M 23s
235300K .......... .......... .......... .......... .......... 46% 11.7M 23s
235350K .......... .......... .......... .......... .......... 46% 9.17M 23s
235400K .......... .......... .......... .......... .......... 46% 11.7M 23s
235450K .......... .......... .......... .......... .......... 46% 9.88M 23s
235500K .......... .......... .......... .......... .......... 46% 15.3M 23s
235550K .......... .......... .......... .......... .......... 46% 13.5M 23s
235600K .......... .......... .......... .......... .......... 46% 18.3M 23s
235650K .......... .......... .......... .......... .......... 46% 31.7M 23s
235700K .......... .......... .......... .......... .......... 46% 23.1M 23s
235750K .......... .......... .......... .......... .......... 46% 53.2M 23s
235800K .......... .......... .......... .......... .......... 46% 23.8M 23s
235850K .......... .......... .......... .......... .......... 46% 18.6M 23s
235900K .......... .......... .......... .......... .......... 46% 15.9M 23s
235950K .......... .......... .......... .......... .......... 46% 14.3M 23s
236000K .......... .......... .......... .......... .......... 46% 13.4M 23s
236050K .......... .......... .......... .......... .......... 46% 13.4M 23s
236100K .......... .......... .......... .......... .......... 46% 13.5M 23s
236150K .......... .......... .......... .......... .......... 46% 13.9M 23s
236200K .......... .......... .......... .......... .......... 46% 11.1M 23s
236250K .......... .......... .......... .......... .......... 46% 10.7M 23s
236300K .......... .......... .......... .......... .......... 46% 11.1M 23s
236350K .......... .......... .......... .......... .......... 46% 9.92M 23s
236400K .......... .......... .......... .......... .......... 46% 12.8M 23s
236450K .......... .......... .......... .......... .......... 46% 9.00M 23s
236500K .......... .......... .......... .......... .......... 46% 12.2M 23s
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236750K .......... .......... .......... .......... .......... 47% 11.3M 23s
236800K .......... .......... .......... .......... .......... 47% 15.1M 23s
236850K .......... .......... .......... .......... .......... 47% 9.93M 23s
236900K .......... .......... .......... .......... .......... 47% 15.0M 23s
236950K .......... .......... .......... .......... .......... 47% 13.0M 23s
237000K .......... .......... .......... .......... .......... 47% 14.0M 23s
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237100K .......... .......... .......... .......... .......... 47% 14.5M 23s
237150K .......... .......... .......... .......... .......... 47% 25.5M 23s
237200K .......... .......... .......... .......... .......... 47% 23.8M 23s
237250K .......... .......... .......... .......... .......... 47% 42.4M 23s
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237500K .......... .......... .......... .......... .......... 47% 13.8M 23s
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237850K .......... .......... .......... .......... .......... 47% 9.42M 23s
237900K .......... .......... .......... .......... .......... 47% 10.0M 23s
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238000K .......... .......... .......... .......... .......... 47% 11.5M 23s
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238150K .......... .......... .......... .......... .......... 47% 10.3M 23s
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238750K .......... .......... .......... .......... .......... 47% 75.5M 23s
238800K .......... .......... .......... .......... .......... 47% 10.2M 23s
238850K .......... .......... .......... .......... .......... 47% 67.7M 23s
238900K .......... .......... .......... .......... .......... 47% 78.8M 23s
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239100K .......... .......... .......... .......... .......... 47% 26.9M 23s
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239250K .......... .......... .......... .......... .......... 47% 10.1M 23s
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240000K .......... .......... .......... .......... .......... 47% 36.9M 23s
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242150K .......... .......... .......... .......... .......... 48% 10.3M 23s
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242250K .......... .......... .......... .......... .......... 48% 10.3M 23s
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243000K .......... .......... .......... .......... .......... 48% 11.3M 23s
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245100K .......... .......... .......... .......... .......... 48% 27.7M 23s
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245200K .......... .......... .......... .......... .......... 48% 64.3M 23s
245250K .......... .......... .......... .......... .......... 48% 13.4M 23s
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248200K .......... .......... .......... .......... .......... 49% 75.7M 23s
248250K .......... .......... .......... .......... .......... 49% 19.9M 23s
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249100K .......... .......... .......... .......... .......... 49% 4.80M 22s
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249800K .......... .......... .......... .......... .......... 49% 4.97M 22s
249850K .......... .......... .......... .......... .......... 49% 4.97M 22s
249900K .......... .......... .......... .......... .......... 49% 5.23M 22s
249950K .......... .......... .......... .......... .......... 49% 3.35M 22s
250000K .......... .......... .......... .......... .......... 49% 8.34M 22s
250050K .......... .......... .......... .......... .......... 49% 8.05M 22s
250100K .......... .......... .......... .......... .......... 49% 4.99M 22s
250150K .......... .......... .......... .......... .......... 49% 5.31M 22s
250200K .......... .......... .......... .......... .......... 49% 7.15M 22s
250250K .......... .......... .......... .......... .......... 49% 8.99M 22s
250300K .......... .......... .......... .......... .......... 49% 5.71M 22s
250350K .......... .......... .......... .......... .......... 49% 10.1M 22s
250400K .......... .......... .......... .......... .......... 49% 13.0M 22s
250450K .......... .......... .......... .......... .......... 49% 10.7M 22s
250500K .......... .......... .......... .......... .......... 49% 14.7M 22s
250550K .......... .......... .......... .......... .......... 49% 11.4M 22s
250600K .......... .......... .......... .......... .......... 49% 7.03M 22s
250650K .......... .......... .......... .......... .......... 49% 15.7M 22s
250700K .......... .......... .......... .......... .......... 49% 4.46M 22s
250750K .......... .......... .......... .......... .......... 49% 4.87M 22s
250800K .......... .......... .......... .......... .......... 49% 4.81M 22s
250850K .......... .......... .......... .......... .......... 49% 5.10M 22s
250900K .......... .......... .......... .......... .......... 49% 7.63M 22s
250950K .......... .......... .......... .......... .......... 49% 16.4M 22s
251000K .......... .......... .......... .......... .......... 49% 16.9M 22s
251050K .......... .......... .......... .......... .......... 49% 15.2M 22s
251100K .......... .......... .......... .......... .......... 49% 11.0M 22s
251150K .......... .......... .......... .......... .......... 49% 14.0M 22s
251200K .......... .......... .......... .......... .......... 49% 12.2M 22s
251250K .......... .......... .......... .......... .......... 49% 8.87M 22s
251300K .......... .......... .......... .......... .......... 49% 10.6M 22s
251350K .......... .......... .......... .......... .......... 49% 8.35M 22s
251400K .......... .......... .......... .......... .......... 49% 7.54M 22s
251450K .......... .......... .......... .......... .......... 49% 7.14M 22s
251500K .......... .......... .......... .......... .......... 49% 8.53M 22s
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251600K .......... .......... .......... .......... .......... 49% 7.93M 22s
251650K .......... .......... .......... .......... .......... 49% 11.5M 22s
251700K .......... .......... .......... .......... .......... 49%  131M 22s
251750K .......... .......... .......... .......... .......... 49% 9.30M 22s
251800K .......... .......... .......... .......... .......... 50% 23.5M 22s
251850K .......... .......... .......... .......... .......... 50% 9.41M 22s
251900K .......... .......... .......... .......... .......... 50% 9.40M 22s
251950K .......... .......... .......... .......... .......... 50% 7.41M 22s
252000K .......... .......... .......... .......... .......... 50% 8.02M 22s
252050K .......... .......... .......... .......... .......... 50% 10.2M 22s
252100K .......... .......... .......... .......... .......... 50% 8.57M 22s
252150K .......... .......... .......... .......... .......... 50% 7.04M 22s
252200K .......... .......... .......... .......... .......... 50% 6.29M 22s
252250K .......... .......... .......... .......... .......... 50% 6.09M 22s
252300K .......... .......... .......... .......... .......... 50% 4.73M 22s
252350K .......... .......... .......... .......... .......... 50% 2.97M 22s
252400K .......... .......... .......... .......... .......... 50% 4.56M 22s
252450K .......... .......... .......... .......... .......... 50% 5.23M 22s
252500K .......... .......... .......... .......... .......... 50% 8.73M 22s
252550K .......... .......... .......... .......... .......... 50% 9.73M 22s
252600K .......... .......... .......... .......... .......... 50% 4.52M 22s
252650K .......... .......... .......... .......... .......... 50% 5.81M 22s
252700K .......... .......... .......... .......... .......... 50% 3.40M 22s
252750K .......... .......... .......... .......... .......... 50% 4.52M 22s
252800K .......... .......... .......... .......... .......... 50% 3.92M 22s
252850K .......... .......... .......... .......... .......... 50% 5.06M 22s
252900K .......... .......... .......... .......... .......... 50% 25.3M 22s
252950K .......... .......... .......... .......... .......... 50% 9.40M 22s
253000K .......... .......... .......... .......... .......... 50% 19.1M 22s
253050K .......... .......... .......... .......... .......... 50% 10.6M 22s
253100K .......... .......... .......... .......... .......... 50% 9.37M 22s
253150K .......... .......... .......... .......... .......... 50% 9.23M 22s
253200K .......... .......... .......... .......... .......... 50% 7.52M 22s
253250K .......... .......... .......... .......... .......... 50% 8.82M 22s
253300K .......... .......... .......... .......... .......... 50% 7.16M 22s
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253400K .......... .......... .......... .......... .......... 50% 7.59M 22s
253450K .......... .......... .......... .......... .......... 50% 17.8M 22s
253500K .......... .......... .......... .......... .......... 50% 16.8M 22s
253550K .......... .......... .......... .......... .......... 50% 18.0M 22s
253600K .......... .......... .......... .......... .......... 50% 8.49M 22s
253650K .......... .......... .......... .......... .......... 50% 30.2M 22s
253700K .......... .......... .......... .......... .......... 50% 10.5M 22s
253750K .......... .......... .......... .......... .......... 50% 19.9M 22s
253800K .......... .......... .......... .......... .......... 50% 22.2M 22s
253850K .......... .......... .......... .......... .......... 50% 13.7M 22s
253900K .......... .......... .......... .......... .......... 50% 16.7M 22s
253950K .......... .......... .......... .......... .......... 50% 13.5M 22s
254000K .......... .......... .......... .......... .......... 50% 11.2M 22s
254050K .......... .......... .......... .......... .......... 50% 9.68M 22s
254100K .......... .......... .......... .......... .......... 50% 10.2M 22s
254150K .......... .......... .......... .......... .......... 50% 15.6M 22s
254200K .......... .......... .......... .......... .......... 50% 9.43M 22s
254250K .......... .......... .......... .......... .......... 50% 7.19M 22s
254300K .......... .......... .......... .......... .......... 50% 10.9M 22s
254350K .......... .......... .......... .......... .......... 50% 26.5M 22s
254400K .......... .......... .......... .......... .......... 50% 17.1M 22s
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254500K .......... .......... .......... .......... .......... 50% 54.9M 22s
254550K .......... .......... .......... .......... .......... 50% 22.2M 22s
254600K .......... .......... .......... .......... .......... 50% 15.5M 22s
254650K .......... .......... .......... .......... .......... 50% 17.8M 22s
254700K .......... .......... .......... .......... .......... 50% 16.4M 22s
254750K .......... .......... .......... .......... .......... 50% 20.7M 22s
254800K .......... .......... .......... .......... .......... 50% 16.4M 22s
254850K .......... .......... .......... .......... .......... 50% 14.5M 22s
254900K .......... .......... .......... .......... .......... 50% 18.1M 22s
254950K .......... .......... .......... .......... .......... 50% 15.6M 22s
255000K .......... .......... .......... .......... .......... 50% 22.0M 22s
255050K .......... .......... .......... .......... .......... 50% 21.2M 22s
255100K .......... .......... .......... .......... .......... 50% 14.9M 22s
255150K .......... .......... .......... .......... .......... 50% 24.0M 22s
255200K .......... .......... .......... .......... .......... 50% 20.4M 22s
255250K .......... .......... .......... .......... .......... 50% 19.8M 22s
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255350K .......... .......... .......... .......... .......... 50% 17.0M 22s
255400K .......... .......... .......... .......... .......... 50% 20.9M 22s
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255500K .......... .......... .......... .......... .......... 50% 15.6M 22s
255550K .......... .......... .......... .......... .......... 50% 73.4M 22s
255600K .......... .......... .......... .......... .......... 50% 56.8M 22s
255650K .......... .......... .......... .......... .......... 50% 20.5M 22s
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255750K .......... .......... .......... .......... .......... 50% 26.9M 22s
255800K .......... .......... .......... .......... .......... 50% 20.9M 22s
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255900K .......... .......... .......... .......... .......... 50% 15.1M 22s
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256000K .......... .......... .......... .......... .......... 50% 13.9M 22s
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256100K .......... .......... .......... .......... .......... 50% 10.3M 22s
256150K .......... .......... .......... .......... .......... 50% 10.8M 22s
256200K .......... .......... .......... .......... .......... 50% 6.64M 22s
256250K .......... .......... .......... .......... .......... 50% 11.8M 22s
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256450K .......... .......... .......... .......... .......... 50% 9.47M 22s
256500K .......... .......... .......... .......... .......... 50% 8.40M 22s
256550K .......... .......... .......... .......... .......... 50% 12.2M 22s
256600K .......... .......... .......... .......... .......... 50% 7.96M 22s
256650K .......... .......... .......... .......... .......... 50% 9.40M 22s
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256800K .......... .......... .......... .......... .......... 51% 7.84M 22s
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256900K .......... .......... .......... .......... .......... 51% 8.63M 22s
256950K .......... .......... .......... .......... .......... 51% 5.31M 22s
257000K .......... .......... .......... .......... .......... 51% 6.54M 22s
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257100K .......... .......... .......... .......... .......... 51% 4.70M 22s
257150K .......... .......... .......... .......... .......... 51% 11.3M 22s
257200K .......... .......... .......... .......... .......... 51% 13.7M 22s
257250K .......... .......... .......... .......... .......... 51% 15.7M 22s
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257400K .......... .......... .......... .......... .......... 51% 6.34M 22s
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257650K .......... .......... .......... .......... .......... 51% 6.06M 22s
257700K .......... .......... .......... .......... .......... 51% 11.2M 22s
257750K .......... .......... .......... .......... .......... 51% 28.0M 22s
257800K .......... .......... .......... .......... .......... 51% 11.5M 22s
257850K .......... .......... .......... .......... .......... 51% 35.9M 22s
257900K .......... .......... .......... .......... .......... 51% 79.5M 22s
257950K .......... .......... .......... .......... .......... 51% 67.4M 22s
258000K .......... .......... .......... .......... .......... 51% 80.4M 22s
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258100K .......... .......... .......... .......... .......... 51% 32.5M 22s
258150K .......... .......... .......... .......... .......... 51% 38.3M 22s
258200K .......... .......... .......... .......... .......... 51% 23.4M 22s
258250K .......... .......... .......... .......... .......... 51% 26.8M 22s
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258650K .......... .......... .......... .......... .......... 51% 31.6M 22s
258700K .......... .......... .......... .......... .......... 51% 20.7M 22s
258750K .......... .......... .......... .......... .......... 51% 34.1M 22s
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258850K .......... .......... .......... .......... .......... 51% 14.4M 22s
258900K .......... .......... .......... .......... .......... 51% 84.8M 22s
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259000K .......... .......... .......... .......... .......... 51% 14.5M 22s
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259100K .......... .......... .......... .......... .......... 51% 25.0M 22s
259150K .......... .......... .......... .......... .......... 51% 14.5M 22s
259200K .......... .......... .......... .......... .......... 51% 10.5M 22s
259250K .......... .......... .......... .......... .......... 51% 12.5M 22s
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259500K .......... .......... .......... .......... .......... 51% 7.94M 22s
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259650K .......... .......... .......... .......... .......... 51% 11.8M 22s
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259750K .......... .......... .......... .......... .......... 51% 17.0M 22s
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259900K .......... .......... .......... .......... .......... 51% 9.07M 22s
259950K .......... .......... .......... .......... .......... 51% 7.20M 22s
260000K .......... .......... .......... .......... .......... 51% 9.40M 22s
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260200K .......... .......... .......... .......... .......... 51% 8.62M 22s
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260300K .......... .......... .......... .......... .......... 51% 7.18M 22s
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260400K .......... .......... .......... .......... .......... 51% 19.9M 22s
260450K .......... .......... .......... .......... .......... 51% 17.9M 22s
260500K .......... .......... .......... .......... .......... 51% 28.8M 22s
260550K .......... .......... .......... .......... .......... 51% 21.9M 22s
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260650K .......... .......... .......... .......... .......... 51% 10.4M 22s
260700K .......... .......... .......... .......... .......... 51% 8.70M 22s
260750K .......... .......... .......... .......... .......... 51% 8.40M 22s
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260850K .......... .......... .......... .......... .......... 51% 7.38M 22s
260900K .......... .......... .......... .......... .......... 51% 9.43M 22s
260950K .......... .......... .......... .......... .......... 51% 8.03M 22s
261000K .......... .......... .......... .......... .......... 51% 4.87M 22s
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261100K .......... .......... .......... .......... .......... 51% 4.10M 22s
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261200K .......... .......... .......... .......... .......... 51% 9.49M 22s
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261400K .......... .......... .......... .......... .......... 51% 13.7M 21s
261450K .......... .......... .......... .......... .......... 51% 46.5M 21s
261500K .......... .......... .......... .......... .......... 51% 21.6M 21s
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261600K .......... .......... .......... .......... .......... 51% 19.1M 21s
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261800K .......... .......... .......... .......... .......... 51% 13.0M 21s
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261900K .......... .......... .......... .......... .......... 52% 12.5M 21s
261950K .......... .......... .......... .......... .......... 52% 7.92M 21s
262000K .......... .......... .......... .......... .......... 52% 10.5M 21s
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262100K .......... .......... .......... .......... .......... 52% 7.55M 21s
262150K .......... .......... .......... .......... .......... 52% 11.4M 21s
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262250K .......... .......... .......... .......... .......... 52% 81.2M 21s
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262400K .......... .......... .......... .......... .......... 52% 18.9M 21s
262450K .......... .......... .......... .......... .......... 52% 12.0M 21s
262500K .......... .......... .......... .......... .......... 52% 18.1M 21s
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262600K .......... .......... .......... .......... .......... 52% 11.3M 21s
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262700K .......... .......... .......... .......... .......... 52% 7.42M 21s
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262800K .......... .......... .......... .......... .......... 52% 9.04M 21s
262850K .......... .......... .......... .......... .......... 52% 6.78M 21s
262900K .......... .......... .......... .......... .......... 52% 8.63M 21s
262950K .......... .......... .......... .......... .......... 52% 14.0M 21s
263000K .......... .......... .......... .......... .......... 52% 31.4M 21s
263050K .......... .......... .......... .......... .......... 52% 17.1M 21s
263100K .......... .......... .......... .......... .......... 52% 25.1M 21s
263150K .......... .......... .......... .......... .......... 52% 18.4M 21s
263200K .......... .......... .......... .......... .......... 52% 32.6M 21s
263250K .......... .......... .......... .......... .......... 52% 15.2M 21s
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263350K .......... .......... .......... .......... .......... 52% 13.2M 21s
263400K .......... .......... .......... .......... .......... 52% 16.4M 21s
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263500K .......... .......... .......... .......... .......... 52% 14.5M 21s
263550K .......... .......... .......... .......... .......... 52% 18.1M 21s
263600K .......... .......... .......... .......... .......... 52% 10.5M 21s
263650K .......... .......... .......... .......... .......... 52% 18.4M 21s
263700K .......... .......... .......... .......... .......... 52% 11.3M 21s
263750K .......... .......... .......... .......... .......... 52% 15.7M 21s
263800K .......... .......... .......... .......... .......... 52% 8.65M 21s
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263900K .......... .......... .......... .......... .......... 52% 10.5M 21s
263950K .......... .......... .......... .......... .......... 52% 8.99M 21s
264000K .......... .......... .......... .......... .......... 52% 8.61M 21s
264050K .......... .......... .......... .......... .......... 52% 9.05M 21s
264100K .......... .......... .......... .......... .......... 52% 8.13M 21s
264150K .......... .......... .......... .......... .......... 52% 8.84M 21s
264200K .......... .......... .......... .......... .......... 52% 7.76M 21s
264250K .......... .......... .......... .......... .......... 52% 18.8M 21s
264300K .......... .......... .......... .......... .......... 52% 30.9M 21s
264350K .......... .......... .......... .......... .......... 52% 18.4M 21s
264400K .......... .......... .......... .......... .......... 52% 38.5M 21s
264450K .......... .......... .......... .......... .......... 52% 17.0M 21s
264500K .......... .......... .......... .......... .......... 52% 18.6M 21s
264550K .......... .......... .......... .......... .......... 52% 11.4M 21s
264600K .......... .......... .......... .......... .......... 52% 11.8M 21s
264650K .......... .......... .......... .......... .......... 52% 12.6M 21s
264700K .......... .......... .......... .......... .......... 52% 9.95M 21s
264750K .......... .......... .......... .......... .......... 52% 8.26M 21s
264800K .......... .......... .......... .......... .......... 52% 9.46M 21s
264850K .......... .......... .......... .......... .......... 52% 5.74M 21s
264900K .......... .......... .......... .......... .......... 52% 7.03M 21s
264950K .......... .......... .......... .......... .......... 52% 5.57M 21s
265000K .......... .......... .......... .......... .......... 52% 5.94M 21s
265050K .......... .......... .......... .......... .......... 52% 8.86M 21s
265100K .......... .......... .......... .......... .......... 52% 18.3M 21s
265150K .......... .......... .......... .......... .......... 52% 15.8M 21s
265200K .......... .......... .......... .......... .......... 52% 11.8M 21s
265250K .......... .......... .......... .......... .......... 52% 11.2M 21s
265300K .......... .......... .......... .......... .......... 52% 11.4M 21s
265350K .......... .......... .......... .......... .......... 52% 7.86M 21s
265400K .......... .......... .......... .......... .......... 52% 8.62M 21s
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265500K .......... .......... .......... .......... .......... 52% 5.18M 21s
265550K .......... .......... .......... .......... .......... 52% 6.51M 21s
265600K .......... .......... .......... .......... .......... 52% 8.34M 21s
265650K .......... .......... .......... .......... .......... 52% 11.8M 21s
265700K .......... .......... .......... .......... .......... 52% 7.77M 21s
265750K .......... .......... .......... .......... .......... 52% 10.9M 21s
265800K .......... .......... .......... .......... .......... 52% 8.47M 21s
265850K .......... .......... .......... .......... .......... 52% 7.88M 21s
265900K .......... .......... .......... .......... .......... 52% 10.4M 21s
265950K .......... .......... .......... .......... .......... 52% 19.0M 21s
266000K .......... .......... .......... .......... .......... 52% 15.9M 21s
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266100K .......... .......... .......... .......... .......... 52% 13.1M 21s
266150K .......... .......... .......... .......... .......... 52% 13.4M 21s
266200K .......... .......... .......... .......... .......... 52% 13.3M 21s
266250K .......... .......... .......... .......... .......... 52% 13.7M 21s
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266350K .......... .......... .......... .......... .......... 52% 9.24M 21s
266400K .......... .......... .......... .......... .......... 52% 17.2M 21s
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266500K .......... .......... .......... .......... .......... 52% 44.2M 21s
266550K .......... .......... .......... .......... .......... 52% 16.5M 21s
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266650K .......... .......... .......... .......... .......... 52% 18.3M 21s
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266900K .......... .......... .......... .......... .......... 53% 12.1M 21s
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267000K .......... .......... .......... .......... .......... 53% 13.0M 21s
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267100K .......... .......... .......... .......... .......... 53% 13.7M 21s
267150K .......... .......... .......... .......... .......... 53% 13.1M 21s
267200K .......... .......... .......... .......... .......... 53% 9.94M 21s
267250K .......... .......... .......... .......... .......... 53% 24.9M 21s
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267400K .......... .......... .......... .......... .......... 53% 33.1M 21s
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267500K .......... .......... .......... .......... .......... 53% 91.3M 21s
267550K .......... .......... .......... .......... .......... 53% 21.3M 21s
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267650K .......... .......... .......... .......... .......... 53% 24.0M 21s
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267850K .......... .......... .......... .......... .......... 53% 9.16M 21s
267900K .......... .......... .......... .......... .......... 53% 11.1M 21s
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268000K .......... .......... .......... .......... .......... 53% 8.70M 21s
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268100K .......... .......... .......... .......... .......... 53% 4.71M 21s
268150K .......... .......... .......... .......... .......... 53% 5.13M 21s
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268250K .......... .......... .......... .......... .......... 53% 6.77M 21s
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268700K .......... .......... .......... .......... .......... 53% 7.63M 21s
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268900K .......... .......... .......... .......... .......... 53% 23.1M 21s
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269000K .......... .......... .......... .......... .......... 53% 12.5M 21s
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269100K .......... .......... .......... .......... .......... 53% 12.6M 21s
269150K .......... .......... .......... .......... .......... 53% 15.4M 21s
269200K .......... .......... .......... .......... .......... 53% 11.5M 21s
269250K .......... .......... .......... .......... .......... 53% 13.4M 21s
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270000K .......... .......... .......... .......... .......... 53% 12.6M 21s
270050K .......... .......... .......... .......... .......... 53% 9.95M 21s
270100K .......... .......... .......... .......... .......... 53% 5.05M 21s
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270200K .......... .......... .......... .......... .......... 53% 4.62M 21s
270250K .......... .......... .......... .......... .......... 53% 6.01M 21s
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270450K .......... .......... .......... .......... .......... 53% 69.4M 21s
270500K .......... .......... .......... .......... .......... 53% 16.5M 21s
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270600K .......... .......... .......... .......... .......... 53% 12.5M 21s
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270800K .......... .......... .......... .......... .......... 53% 17.2M 21s
270850K .......... .......... .......... .......... .......... 53% 13.6M 21s
270900K .......... .......... .......... .......... .......... 53% 11.8M 21s
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271000K .......... .......... .......... .......... .......... 53% 9.26M 21s
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271100K .......... .......... .......... .......... .......... 53% 14.6M 21s
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271200K .......... .......... .......... .......... .......... 53% 10.0M 21s
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271350K .......... .......... .......... .......... .......... 53% 9.72M 21s
271400K .......... .......... .......... .......... .......... 53% 13.0M 21s
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271500K .......... .......... .......... .......... .......... 53% 17.1M 21s
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271600K .......... .......... .......... .......... .......... 53% 15.1M 21s
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271700K .......... .......... .......... .......... .......... 53% 14.8M 21s
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271800K .......... .......... .......... .......... .......... 53% 32.3M 21s
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271900K .......... .......... .......... .......... .......... 54% 16.4M 21s
271950K .......... .......... .......... .......... .......... 54% 16.4M 20s
272000K .......... .......... .......... .......... .......... 54% 18.5M 20s
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272150K .......... .......... .......... .......... .......... 54% 12.4M 20s
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272250K .......... .......... .......... .......... .......... 54% 13.2M 20s
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272500K .......... .......... .......... .......... .......... 54% 20.1M 20s
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272600K .......... .......... .......... .......... .......... 54% 13.0M 20s
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272700K .......... .......... .......... .......... .......... 54% 10.5M 20s
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272800K .......... .......... .......... .......... .......... 54% 13.7M 20s
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272900K .......... .......... .......... .......... .......... 54% 14.3M 20s
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273000K .......... .......... .......... .......... .......... 54% 12.5M 20s
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273100K .......... .......... .......... .......... .......... 54% 10.5M 20s
273150K .......... .......... .......... .......... .......... 54% 12.5M 20s
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273250K .......... .......... .......... .......... .......... 54% 10.3M 20s
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273400K .......... .......... .......... .......... .......... 54% 12.8M 20s
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273500K .......... .......... .......... .......... .......... 54% 17.6M 20s
273550K .......... .......... .......... .......... .......... 54% 22.7M 20s
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274000K .......... .......... .......... .......... .......... 54% 16.4M 20s
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274100K .......... .......... .......... .......... .......... 54% 12.0M 20s
274150K .......... .......... .......... .......... .......... 54% 13.7M 20s
274200K .......... .......... .......... .......... .......... 54% 6.58M 20s
274250K .......... .......... .......... .......... .......... 54% 81.1M 20s
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274750K .......... .......... .......... .......... .......... 54% 12.1M 20s
274800K .......... .......... .......... .......... .......... 54% 12.6M 20s
274850K .......... .......... .......... .......... .......... 54% 8.34M 20s
274900K .......... .......... .......... .......... .......... 54% 14.7M 20s
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275000K .......... .......... .......... .......... .......... 54% 12.0M 20s
275050K .......... .......... .......... .......... .......... 54% 11.5M 20s
275100K .......... .......... .......... .......... .......... 54% 9.25M 20s
275150K .......... .......... .......... .......... .......... 54% 13.0M 20s
275200K .......... .......... .......... .......... .......... 54% 11.6M 20s
275250K .......... .......... .......... .......... .......... 54% 10.5M 20s
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275350K .......... .......... .......... .......... .......... 54% 8.45M 20s
275400K .......... .......... .......... .......... .......... 54% 9.72M 20s
275450K .......... .......... .......... .......... .......... 54% 6.99M 20s
275500K .......... .......... .......... .......... .......... 54% 7.16M 20s
275550K .......... .......... .......... .......... .......... 54% 7.65M 20s
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275750K .......... .......... .......... .......... .......... 54% 28.5M 20s
275800K .......... .......... .......... .......... .......... 54% 10.9M 20s
275850K .......... .......... .......... .......... .......... 54% 57.6M 20s
275900K .......... .......... .......... .......... .......... 54% 40.8M 20s
275950K .......... .......... .......... .......... .......... 54% 31.4M 20s
276000K .......... .......... .......... .......... .......... 54% 30.8M 20s
276050K .......... .......... .......... .......... .......... 54% 21.9M 20s
276100K .......... .......... .......... .......... .......... 54% 17.9M 20s
276150K .......... .......... .......... .......... .......... 54% 18.8M 20s
276200K .......... .......... .......... .......... .......... 54% 18.7M 20s
276250K .......... .......... .......... .......... .......... 54% 17.2M 20s
276300K .......... .......... .......... .......... .......... 54% 20.9M 20s
276350K .......... .......... .......... .......... .......... 54% 12.9M 20s
276400K .......... .......... .......... .......... .......... 54% 19.0M 20s
276450K .......... .......... .......... .......... .......... 54% 11.3M 20s
276500K .......... .......... .......... .......... .......... 54% 18.2M 20s
276550K .......... .......... .......... .......... .......... 54% 12.2M 20s
276600K .......... .......... .......... .......... .......... 54% 9.46M 20s
276650K .......... .......... .......... .......... .......... 54% 11.3M 20s
276700K .......... .......... .......... .......... .......... 54% 9.54M 20s
276750K .......... .......... .......... .......... .......... 54% 76.8M 20s
276800K .......... .......... .......... .......... .......... 54% 16.6M 20s
276850K .......... .......... .......... .......... .......... 54% 14.1M 20s
276900K .......... .......... .......... .......... .......... 54% 15.6M 20s
276950K .......... .......... .......... .......... .......... 55% 15.1M 20s
277000K .......... .......... .......... .......... .......... 55% 11.5M 20s
277050K .......... .......... .......... .......... .......... 55% 16.2M 20s
277100K .......... .......... .......... .......... .......... 55% 11.6M 20s
277150K .......... .......... .......... .......... .......... 55% 13.6M 20s
277200K .......... .......... .......... .......... .......... 55% 10.5M 20s
277250K .......... .......... .......... .......... .......... 55% 12.2M 20s
277300K .......... .......... .......... .......... .......... 55% 9.82M 20s
277350K .......... .......... .......... .......... .......... 55% 9.44M 20s
277400K .......... .......... .......... .......... .......... 55% 12.3M 20s
277450K .......... .......... .......... .......... .......... 55% 16.4M 20s
277500K .......... .......... .......... .......... .......... 55% 82.9M 20s
277550K .......... .......... .......... .......... .......... 55% 27.4M 20s
277600K .......... .......... .......... .......... .......... 55% 13.9M 20s
277650K .......... .......... .......... .......... .......... 55% 31.1M 20s
277700K .......... .......... .......... .......... .......... 55% 14.7M 20s
277750K .......... .......... .......... .......... .......... 55% 14.4M 20s
277800K .......... .......... .......... .......... .......... 55% 11.8M 20s
277850K .......... .......... .......... .......... .......... 55% 7.60M 20s
277900K .......... .......... .......... .......... .......... 55% 11.7M 20s
277950K .......... .......... .......... .......... .......... 55% 10.2M 20s
278000K .......... .......... .......... .......... .......... 55% 8.87M 20s
278050K .......... .......... .......... .......... .......... 55% 12.3M 20s
278100K .......... .......... .......... .......... .......... 55% 8.39M 20s
278150K .......... .......... .......... .......... .......... 55% 10.8M 20s
278200K .......... .......... .......... .......... .......... 55% 8.86M 20s
278250K .......... .......... .......... .......... .......... 55% 18.4M 20s
278300K .......... .......... .......... .......... .......... 55% 17.8M 20s
278350K .......... .......... .......... .......... .......... 55% 10.5M 20s
278400K .......... .......... .......... .......... .......... 55% 12.4M 20s
278450K .......... .......... .......... .......... .......... 55% 18.7M 20s
278500K .......... .......... .......... .......... .......... 55% 30.4M 20s
278550K .......... .......... .......... .......... .......... 55% 11.8M 20s
278600K .......... .......... .......... .......... .......... 55% 14.9M 20s
278650K .......... .......... .......... .......... .......... 55% 14.7M 20s
278700K .......... .......... .......... .......... .......... 55% 14.2M 20s
278750K .......... .......... .......... .......... .......... 55% 16.5M 20s
278800K .......... .......... .......... .......... .......... 55% 13.9M 20s
278850K .......... .......... .......... .......... .......... 55% 12.9M 20s
278900K .......... .......... .......... .......... .......... 55% 12.2M 20s
278950K .......... .......... .......... .......... .......... 55% 12.3M 20s
279000K .......... .......... .......... .......... .......... 55% 13.1M 20s
279050K .......... .......... .......... .......... .......... 55% 18.2M 20s
279100K .......... .......... .......... .......... .......... 55% 12.4M 20s
279150K .......... .......... .......... .......... .......... 55% 15.7M 20s
279200K .......... .......... .......... .......... .......... 55% 17.8M 20s
279250K .......... .......... .......... .......... .......... 55% 30.8M 20s
279300K .......... .......... .......... .......... .......... 55% 26.7M 20s
279350K .......... .......... .......... .......... .......... 55% 12.8M 20s
279400K .......... .......... .......... .......... .......... 55% 85.5M 20s
279450K .......... .......... .......... .......... .......... 55% 13.3M 20s
279500K .......... .......... .......... .......... .......... 55% 90.6M 20s
279550K .......... .......... .......... .......... .......... 55% 26.9M 20s
279600K .......... .......... .......... .......... .......... 55% 15.5M 20s
279650K .......... .......... .......... .......... .......... 55% 38.1M 20s
279700K .......... .......... .......... .......... .......... 55% 25.5M 20s
279750K .......... .......... .......... .......... .......... 55% 18.8M 20s
279800K .......... .......... .......... .......... .......... 55% 18.9M 20s
279850K .......... .......... .......... .......... .......... 55% 17.5M 20s
279900K .......... .......... .......... .......... .......... 55% 16.5M 20s
279950K .......... .......... .......... .......... .......... 55% 15.8M 20s
280000K .......... .......... .......... .......... .......... 55% 19.9M 20s
280050K .......... .......... .......... .......... .......... 55% 16.5M 20s
280100K .......... .......... .......... .......... .......... 55% 13.4M 20s
280150K .......... .......... .......... .......... .......... 55% 25.3M 20s
280200K .......... .......... .......... .......... .......... 55% 15.0M 20s
280250K .......... .......... .......... .......... .......... 55% 14.7M 20s
280300K .......... .......... .......... .......... .......... 55% 18.1M 20s
280350K .......... .......... .......... .......... .......... 55% 7.78M 20s
280400K .......... .......... .......... .......... .......... 55% 13.1M 20s
280450K .......... .......... .......... .......... .......... 55% 7.33M 20s
280500K .......... .......... .......... .......... .......... 55% 13.1M 20s
280550K .......... .......... .......... .......... .......... 55% 12.2M 20s
280600K .......... .......... .......... .......... .......... 55% 12.2M 20s
280650K .......... .......... .......... .......... .......... 55% 10.2M 20s
280700K .......... .......... .......... .......... .......... 55% 9.41M 20s
280750K .......... .......... .......... .......... .......... 55% 13.6M 20s
280800K .......... .......... .......... .......... .......... 55% 8.37M 20s
280850K .......... .......... .......... .......... .......... 55% 5.01M 20s
280900K .......... .......... .......... .......... .......... 55% 18.8M 20s
280950K .......... .......... .......... .......... .......... 55% 8.09M 20s
281000K .......... .......... .......... .......... .......... 55% 21.0M 20s
281050K .......... .......... .......... .......... .......... 55% 87.3M 20s
281100K .......... .......... .......... .......... .......... 55% 9.23M 20s
281150K .......... .......... .......... .......... .......... 55% 18.6M 20s
281200K .......... .......... .......... .......... .......... 55% 9.72M 20s
281250K .......... .......... .......... .......... .......... 55% 8.91M 20s
281300K .......... .......... .......... .......... .......... 55% 8.98M 20s
281350K .......... .......... .......... .......... .......... 55% 8.38M 20s
281400K .......... .......... .......... .......... .......... 55% 13.4M 20s
281450K .......... .......... .......... .......... .......... 55% 12.2M 20s
281500K .......... .......... .......... .......... .......... 55% 9.14M 20s
281550K .......... .......... .......... .......... .......... 55% 8.80M 20s
281600K .......... .......... .......... .......... .......... 55% 6.01M 20s
281650K .......... .......... .......... .......... .......... 55% 6.91M 20s
281700K .......... .......... .......... .......... .......... 55% 5.22M 20s
281750K .......... .......... .......... .......... .......... 55% 4.27M 20s
281800K .......... .......... .......... .......... .......... 55% 7.78M 20s
281850K .......... .......... .......... .......... .......... 55% 18.9M 20s
281900K .......... .......... .......... .......... .......... 55% 14.5M 20s
281950K .......... .......... .......... .......... .......... 55% 10.5M 20s
282000K .......... .......... .......... .......... .......... 56% 10.2M 20s
282050K .......... .......... .......... .......... .......... 56% 14.9M 20s
282100K .......... .......... .......... .......... .......... 56% 10.4M 20s
282150K .......... .......... .......... .......... .......... 56% 10.6M 20s
282200K .......... .......... .......... .......... .......... 56% 8.70M 19s
282250K .......... .......... .......... .......... .......... 56% 12.2M 19s
282300K .......... .......... .......... .......... .......... 56% 14.0M 19s
282350K .......... .......... .......... .......... .......... 56% 9.49M 19s
282400K .......... .......... .......... .......... .......... 56% 24.7M 19s
282450K .......... .......... .......... .......... .......... 56% 24.1M 19s
282500K .......... .......... .......... .......... .......... 56% 12.7M 19s
282550K .......... .......... .......... .......... .......... 56%  142M 19s
282600K .......... .......... .......... .......... .......... 56% 23.5M 19s
282650K .......... .......... .......... .......... .......... 56% 46.8M 19s
282700K .......... .......... .......... .......... .......... 56% 13.0M 19s
282750K .......... .......... .......... .......... .......... 56% 30.4M 19s
282800K .......... .......... .......... .......... .......... 56% 21.4M 19s
282850K .......... .......... .......... .......... .......... 56% 17.0M 19s
282900K .......... .......... .......... .......... .......... 56% 15.1M 19s
282950K .......... .......... .......... .......... .......... 56% 18.7M 19s
283000K .......... .......... .......... .......... .......... 56% 13.7M 19s
283050K .......... .......... .......... .......... .......... 56% 19.3M 19s
283100K .......... .......... .......... .......... .......... 56% 16.1M 19s
283150K .......... .......... .......... .......... .......... 56% 17.9M 19s
283200K .......... .......... .......... .......... .......... 56% 13.5M 19s
283250K .......... .......... .......... .......... .......... 56% 16.3M 19s
283300K .......... .......... .......... .......... .......... 56% 12.5M 19s
283350K .......... .......... .......... .......... .......... 56% 17.0M 19s
283400K .......... .......... .......... .......... .......... 56% 17.1M 19s
283450K .......... .......... .......... .......... .......... 56% 12.6M 19s
283500K .......... .......... .......... .......... .......... 56% 15.1M 19s
283550K .......... .......... .......... .......... .......... 56% 16.7M 19s
283600K .......... .......... .......... .......... .......... 56% 11.0M 19s
283650K .......... .......... .......... .......... .......... 56% 18.2M 19s
283700K .......... .......... .......... .......... .......... 56% 9.93M 19s
283750K .......... .......... .......... .......... .......... 56% 18.9M 19s
283800K .......... .......... .......... .......... .......... 56% 10.9M 19s
283850K .......... .......... .......... .......... .......... 56% 8.88M 19s
283900K .......... .......... .......... .......... .......... 56% 7.67M 19s
283950K .......... .......... .......... .......... .......... 56% 71.5M 19s
284000K .......... .......... .......... .......... .......... 56% 9.10M 19s
284050K .......... .......... .......... .......... .......... 56% 37.1M 19s
284100K .......... .......... .......... .......... .......... 56% 12.5M 19s
284150K .......... .......... .......... .......... .......... 56% 41.1M 19s
284200K .......... .......... .......... .......... .......... 56% 12.5M 19s
284250K .......... .......... .......... .......... .......... 56% 18.8M 19s
284300K .......... .......... .......... .......... .......... 56% 14.6M 19s
284350K .......... .......... .......... .......... .......... 56% 11.6M 19s
284400K .......... .......... .......... .......... .......... 56% 12.2M 19s
284450K .......... .......... .......... .......... .......... 56% 11.2M 19s
284500K .......... .......... .......... .......... .......... 56% 11.8M 19s
284550K .......... .......... .......... .......... .......... 56% 10.6M 19s
284600K .......... .......... .......... .......... .......... 56% 10.5M 19s
284650K .......... .......... .......... .......... .......... 56% 13.6M 19s
284700K .......... .......... .......... .......... .......... 56% 26.8M 19s
284750K .......... .......... .......... .......... .......... 56% 22.6M 19s
284800K .......... .......... .......... .......... .......... 56% 17.1M 19s
284850K .......... .......... .......... .......... .......... 56% 16.9M 19s
284900K .......... .......... .......... .......... .......... 56% 17.2M 19s
284950K .......... .......... .......... .......... .......... 56% 13.9M 19s
285000K .......... .......... .......... .......... .......... 56% 20.7M 19s
285050K .......... .......... .......... .......... .......... 56% 19.6M 19s
285100K .......... .......... .......... .......... .......... 56% 16.0M 19s
285150K .......... .......... .......... .......... .......... 56% 17.9M 19s
285200K .......... .......... .......... .......... .......... 56% 16.5M 19s
285250K .......... .......... .......... .......... .......... 56% 13.9M 19s
285300K .......... .......... .......... .......... .......... 56% 19.8M 19s
285350K .......... .......... .......... .......... .......... 56% 21.1M 19s
285400K .......... .......... .......... .......... .......... 56% 15.3M 19s
285450K .......... .......... .......... .......... .......... 56% 28.3M 19s
285500K .......... .......... .......... .......... .......... 56% 23.2M 19s
285550K .......... .......... .......... .......... .......... 56% 33.2M 19s
285600K .......... .......... .......... .......... .......... 56% 20.7M 19s
285650K .......... .......... .......... .......... .......... 56% 12.2M 19s
285700K .......... .......... .......... .......... .......... 56% 23.6M 19s
285750K .......... .......... .......... .......... .......... 56% 11.0M 19s
285800K .......... .......... .......... .......... .......... 56% 8.72M 19s
285850K .......... .......... .......... .......... .......... 56% 13.0M 19s
285900K .......... .......... .......... .......... .......... 56% 12.2M 19s
285950K .......... .......... .......... .......... .......... 56% 11.8M 19s
286000K .......... .......... .......... .......... .......... 56% 12.1M 19s
286050K .......... .......... .......... .......... .......... 56% 12.1M 19s
286100K .......... .......... .......... .......... .......... 56% 9.20M 19s
286150K .......... .......... .......... .......... .......... 56% 13.1M 19s
286200K .......... .......... .......... .......... .......... 56% 6.60M 19s
286250K .......... .......... .......... .......... .......... 56% 9.57M 19s
286300K .......... .......... .......... .......... .......... 56% 74.3M 19s
286350K .......... .......... .......... .......... .......... 56% 16.6M 19s
286400K .......... .......... .......... .......... .......... 56% 23.1M 19s
286450K .......... .......... .......... .......... .......... 56% 13.3M 19s
286500K .......... .......... .......... .......... .......... 56% 11.0M 19s
286550K .......... .......... .......... .......... .......... 56% 14.0M 19s
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286650K .......... .......... .......... .......... .......... 56% 11.8M 19s
286700K .......... .......... .......... .......... .......... 56% 8.50M 19s
286750K .......... .......... .......... .......... .......... 56% 11.2M 19s
286800K .......... .......... .......... .......... .......... 56% 11.2M 19s
286850K .......... .......... .......... .......... .......... 56% 8.98M 19s
286900K .......... .......... .......... .......... .......... 56% 6.56M 19s
286950K .......... .......... .......... .......... .......... 56% 16.7M 19s
287000K .......... .......... .......... .......... .......... 56% 23.1M 19s
287050K .......... .......... .......... .......... .......... 57% 14.8M 19s
287100K .......... .......... .......... .......... .......... 57% 28.2M 19s
287150K .......... .......... .......... .......... .......... 57% 36.6M 19s
287200K .......... .......... .......... .......... .......... 57% 19.9M 19s
287250K .......... .......... .......... .......... .......... 57% 24.5M 19s
287300K .......... .......... .......... .......... .......... 57% 20.0M 19s
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287400K .......... .......... .......... .......... .......... 57% 22.1M 19s
287450K .......... .......... .......... .......... .......... 57% 23.6M 19s
287500K .......... .......... .......... .......... .......... 57% 21.2M 19s
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287600K .......... .......... .......... .......... .......... 57% 27.3M 19s
287650K .......... .......... .......... .......... .......... 57% 22.7M 19s
287700K .......... .......... .......... .......... .......... 57% 27.7M 19s
287750K .......... .......... .......... .......... .......... 57% 27.4M 19s
287800K .......... .......... .......... .......... .......... 57% 27.3M 19s
287850K .......... .......... .......... .......... .......... 57% 20.4M 19s
287900K .......... .......... .......... .......... .......... 57% 20.2M 19s
287950K .......... .......... .......... .......... .......... 57% 14.9M 19s
288000K .......... .......... .......... .......... .......... 57% 18.7M 19s
288050K .......... .......... .......... .......... .......... 57% 13.1M 19s
288100K .......... .......... .......... .......... .......... 57% 38.6M 19s
288150K .......... .......... .......... .......... .......... 57% 86.7M 19s
288200K .......... .......... .......... .......... .......... 57% 19.7M 19s
288250K .......... .......... .......... .......... .......... 57% 24.3M 19s
288300K .......... .......... .......... .......... .......... 57% 19.9M 19s
288350K .......... .......... .......... .......... .......... 57% 18.4M 19s
288400K .......... .......... .......... .......... .......... 57% 27.5M 19s
288450K .......... .......... .......... .......... .......... 57% 14.9M 19s
288500K .......... .......... .......... .......... .......... 57% 22.7M 19s
288550K .......... .......... .......... .......... .......... 57% 22.9M 19s
288600K .......... .......... .......... .......... .......... 57% 16.8M 19s
288650K .......... .......... .......... .......... .......... 57% 18.5M 19s
288700K .......... .......... .......... .......... .......... 57% 19.3M 19s
288750K .......... .......... .......... .......... .......... 57% 24.1M 19s
288800K .......... .......... .......... .......... .......... 57% 16.1M 19s
288850K .......... .......... .......... .......... .......... 57% 22.4M 19s
288900K .......... .......... .......... .......... .......... 57% 16.3M 19s
288950K .......... .......... .......... .......... .......... 57% 22.6M 19s
289000K .......... .......... .......... .......... .......... 57% 31.6M 19s
289050K .......... .......... .......... .......... .......... 57% 24.2M 19s
289100K .......... .......... .......... .......... .......... 57% 21.5M 19s
289150K .......... .......... .......... .......... .......... 57% 38.5M 19s
289200K .......... .......... .......... .......... .......... 57% 11.7M 19s
289250K .......... .......... .......... .......... .......... 57% 58.1M 19s
289300K .......... .......... .......... .......... .......... 57% 35.4M 19s
289350K .......... .......... .......... .......... .......... 57% 56.4M 19s
289400K .......... .......... .......... .......... .......... 57% 35.3M 19s
289450K .......... .......... .......... .......... .......... 57% 25.7M 19s
289500K .......... .......... .......... .......... .......... 57% 23.9M 19s
289550K .......... .......... .......... .......... .......... 57% 23.0M 19s
289600K .......... .......... .......... .......... .......... 57% 21.8M 19s
289650K .......... .......... .......... .......... .......... 57% 30.7M 19s
289700K .......... .......... .......... .......... .......... 57% 19.3M 19s
289750K .......... .......... .......... .......... .......... 57% 34.9M 19s
289800K .......... .......... .......... .......... .......... 57% 23.8M 19s
289850K .......... .......... .......... .......... .......... 57% 16.9M 19s
289900K .......... .......... .......... .......... .......... 57% 32.2M 19s
289950K .......... .......... .......... .......... .......... 57% 21.4M 19s
290000K .......... .......... .......... .......... .......... 57% 20.2M 19s
290050K .......... .......... .......... .......... .......... 57% 22.7M 19s
290100K .......... .......... .......... .......... .......... 57% 24.2M 19s
290150K .......... .......... .......... .......... .......... 57% 25.4M 19s
290200K .......... .......... .......... .......... .......... 57% 20.5M 19s
290250K .......... .......... .......... .......... .......... 57% 22.4M 19s
290300K .......... .......... .......... .......... .......... 57% 17.6M 19s
290350K .......... .......... .......... .......... .......... 57% 10.7M 19s
290400K .......... .......... .......... .......... .......... 57% 12.2M 19s
290450K .......... .......... .......... .......... .......... 57% 12.2M 19s
290500K .......... .......... .......... .......... .......... 57% 20.3M 19s
290550K .......... .......... .......... .......... .......... 57% 14.6M 19s
290600K .......... .......... .......... .......... .......... 57% 14.9M 19s
290650K .......... .......... .......... .......... .......... 57% 14.9M 19s
290700K .......... .......... .......... .......... .......... 57% 14.6M 19s
290750K .......... .......... .......... .......... .......... 57% 16.6M 19s
290800K .......... .......... .......... .......... .......... 57% 16.7M 19s
290850K .......... .......... .......... .......... .......... 57% 15.6M 19s
290900K .......... .......... .......... .......... .......... 57% 22.6M 19s
290950K .......... .......... .......... .......... .......... 57% 32.1M 19s
291000K .......... .......... .......... .......... .......... 57% 43.6M 19s
291050K .......... .......... .......... .......... .......... 57% 35.0M 19s
291100K .......... .......... .......... .......... .......... 57% 20.8M 19s
291150K .......... .......... .......... .......... .......... 57%  479M 19s
291200K .......... .......... .......... .......... .......... 57% 32.6M 19s
291250K .......... .......... .......... .......... .......... 57% 43.6M 18s
291300K .......... .......... .......... .......... .......... 57% 38.4M 18s
291350K .......... .......... .......... .......... .......... 57% 29.7M 18s
291400K .......... .......... .......... .......... .......... 57% 38.5M 18s
291450K .......... .......... .......... .......... .......... 57% 38.5M 18s
291500K .......... .......... .......... .......... .......... 57% 38.6M 18s
291550K .......... .......... .......... .......... .......... 57% 29.1M 18s
291600K .......... .......... .......... .......... .......... 57% 28.0M 18s
291650K .......... .......... .......... .......... .......... 57% 35.2M 18s
291700K .......... .......... .......... .......... .......... 57% 38.5M 18s
291750K .......... .......... .......... .......... .......... 57% 37.9M 18s
291800K .......... .......... .......... .......... .......... 57% 32.0M 18s
291850K .......... .......... .......... .......... .......... 57% 27.4M 18s
291900K .......... .......... .......... .......... .......... 57% 39.7M 18s
291950K .......... .......... .......... .......... .......... 57% 20.3M 18s
292000K .......... .......... .......... .......... .......... 57% 47.5M 18s
292050K .......... .......... .......... .......... .......... 58% 38.9M 18s
292100K .......... .......... .......... .......... .......... 58% 24.1M 18s
292150K .......... .......... .......... .......... .......... 58% 42.8M 18s
292200K .......... .......... .......... .......... .......... 58% 25.7M 18s
292250K .......... .......... .......... .......... .......... 58% 48.2M 18s
292300K .......... .......... .......... .......... .......... 58% 29.8M 18s
292350K .......... .......... .......... .......... .......... 58% 29.6M 18s
292400K .......... .......... .......... .......... .......... 58% 32.2M 18s
292450K .......... .......... .......... .......... .......... 58% 29.3M 18s
292500K .......... .......... .......... .......... .......... 58% 12.5M 18s
292550K .......... .......... .......... .......... .......... 58% 30.0M 18s
292600K .......... .......... .......... .......... .......... 58% 9.37M 18s
292650K .......... .......... .......... .......... .......... 58% 15.5M 18s
292700K .......... .......... .......... .......... .......... 58% 12.6M 18s
292750K .......... .......... .......... .......... .......... 58% 13.5M 18s
292800K .......... .......... .......... .......... .......... 58% 14.0M 18s
292850K .......... .......... .......... .......... .......... 58% 13.3M 18s
292900K .......... .......... .......... .......... .......... 58% 14.0M 18s
292950K .......... .......... .......... .......... .......... 58% 12.6M 18s
293000K .......... .......... .......... .......... .......... 58% 11.5M 18s
293050K .......... .......... .......... .......... .......... 58% 15.3M 18s
293100K .......... .......... .......... .......... .......... 58% 14.0M 18s
293150K .......... .......... .......... .......... .......... 58% 9.65M 18s
293200K .......... .......... .......... .......... .......... 58% 42.1M 18s
293250K .......... .......... .......... .......... .......... 58% 37.8M 18s
293300K .......... .......... .......... .......... .......... 58% 28.0M 18s
293350K .......... .......... .......... .......... .......... 58% 21.4M 18s
293400K .......... .......... .......... .......... .......... 58% 24.0M 18s
293450K .......... .......... .......... .......... .......... 58% 21.7M 18s
293500K .......... .......... .......... .......... .......... 58% 23.9M 18s
293550K .......... .......... .......... .......... .......... 58% 25.8M 18s
293600K .......... .......... .......... .......... .......... 58% 17.3M 18s
293650K .......... .......... .......... .......... .......... 58% 25.8M 18s
293700K .......... .......... .......... .......... .......... 58% 21.4M 18s
293750K .......... .......... .......... .......... .......... 58% 27.4M 18s
293800K .......... .......... .......... .......... .......... 58% 25.0M 18s
293850K .......... .......... .......... .......... .......... 58% 20.9M 18s
293900K .......... .......... .......... .......... .......... 58% 25.6M 18s
293950K .......... .......... .......... .......... .......... 58% 19.5M 18s
294000K .......... .......... .......... .......... .......... 58% 27.6M 18s
294050K .......... .......... .......... .......... .......... 58% 17.5M 18s
294100K .......... .......... .......... .......... .......... 58% 34.7M 18s
294150K .......... .......... .......... .......... .......... 58% 43.0M 18s
294200K .......... .......... .......... .......... .......... 58% 32.6M 18s
294250K .......... .......... .......... .......... .......... 58% 29.7M 18s
294300K .......... .......... .......... .......... .......... 58% 14.0M 18s
294350K .......... .......... .......... .......... .......... 58%  128M 18s
294400K .......... .......... .......... .......... .......... 58% 30.4M 18s
294450K .......... .......... .......... .......... .......... 58% 77.3M 18s
294500K .......... .......... .......... .......... .......... 58% 30.5M 18s
294550K .......... .......... .......... .......... .......... 58% 30.8M 18s
294600K .......... .......... .......... .......... .......... 58% 27.4M 18s
294650K .......... .......... .......... .......... .......... 58% 25.7M 18s
294700K .......... .......... .......... .......... .......... 58% 25.1M 18s
294750K .......... .......... .......... .......... .......... 58% 35.1M 18s
294800K .......... .......... .......... .......... .......... 58% 21.3M 18s
294850K .......... .......... .......... .......... .......... 58% 25.6M 18s
294900K .......... .......... .......... .......... .......... 58% 40.9M 18s
294950K .......... .......... .......... .......... .......... 58% 29.2M 18s
295000K .......... .......... .......... .......... .......... 58% 27.2M 18s
295050K .......... .......... .......... .......... .......... 58% 43.3M 18s
295100K .......... .......... .......... .......... .......... 58% 22.4M 18s
295150K .......... .......... .......... .......... .......... 58% 30.4M 18s
295200K .......... .......... .......... .......... .......... 58% 20.4M 18s
295250K .......... .......... .......... .......... .......... 58% 38.3M 18s
295300K .......... .......... .......... .......... .......... 58% 25.7M 18s
295350K .......... .......... .......... .......... .......... 58% 27.3M 18s
295400K .......... .......... .......... .......... .......... 58% 21.3M 18s
295450K .......... .......... .......... .......... .......... 58% 20.5M 18s
295500K .......... .......... .......... .......... .......... 58% 14.5M 18s
295550K .......... .......... .......... .......... .......... 58% 9.53M 18s
295600K .......... .......... .......... .......... .......... 58% 8.61M 18s
295650K .......... .......... .......... .......... .......... 58% 14.7M 18s
295700K .......... .......... .......... .......... .......... 58% 10.5M 18s
295750K .......... .......... .......... .......... .......... 58% 18.3M 18s
295800K .......... .......... .......... .......... .......... 58% 15.0M 18s
295850K .......... .......... .......... .......... .......... 58% 12.1M 18s
295900K .......... .......... .......... .......... .......... 58% 18.4M 18s
295950K .......... .......... .......... .......... .......... 58% 12.9M 18s
296000K .......... .......... .......... .......... .......... 58% 16.8M 18s
296050K .......... .......... .......... .......... .......... 58% 16.8M 18s
296100K .......... .......... .......... .......... .......... 58% 12.5M 18s
296150K .......... .......... .......... .......... .......... 58% 14.9M 18s
296200K .......... .......... .......... .......... .......... 58% 8.35M 18s
296250K .......... .......... .......... .......... .......... 58% 10.7M 18s
296300K .......... .......... .......... .......... .......... 58% 10.5M 18s
296350K .......... .......... .......... .......... .......... 58% 33.0M 18s
296400K .......... .......... .......... .......... .......... 58% 13.4M 18s
296450K .......... .......... .......... .......... .......... 58% 27.5M 18s
296500K .......... .......... .......... .......... .......... 58% 20.3M 18s
296550K .......... .......... .......... .......... .......... 58% 24.1M 18s
296600K .......... .......... .......... .......... .......... 58% 17.6M 18s
296650K .......... .......... .......... .......... .......... 58% 22.6M 18s
296700K .......... .......... .......... .......... .......... 58% 23.7M 18s
296750K .......... .......... .......... .......... .......... 58% 22.6M 18s
296800K .......... .......... .......... .......... .......... 58% 20.2M 18s
296850K .......... .......... .......... .......... .......... 58% 20.8M 18s
296900K .......... .......... .......... .......... .......... 58% 20.3M 18s
296950K .......... .......... .......... .......... .......... 58% 25.1M 18s
297000K .......... .......... .......... .......... .......... 58% 20.5M 18s
297050K .......... .......... .......... .......... .......... 58% 21.4M 18s
297100K .......... .......... .......... .......... .......... 59% 21.2M 18s
297150K .......... .......... .......... .......... .......... 59% 22.8M 18s
297200K .......... .......... .......... .......... .......... 59% 16.6M 18s
297250K .......... .......... .......... .......... .......... 59% 29.4M 18s
297300K .......... .......... .......... .......... .......... 59% 47.1M 18s
297350K .......... .......... .......... .......... .......... 59% 37.6M 18s
297400K .......... .......... .......... .......... .......... 59% 44.6M 18s
297450K .......... .......... .......... .......... .......... 59% 22.3M 18s
297500K .......... .......... .......... .......... .......... 59% 25.7M 18s
297550K .......... .......... .......... .......... .......... 59%  381M 18s
297600K .......... .......... .......... .......... .......... 59% 18.0M 18s
297650K .......... .......... .......... .......... .......... 59% 46.6M 18s
297700K .......... .......... .......... .......... .......... 59%  474M 18s
297750K .......... .......... .......... .......... .......... 59% 22.3M 18s
297800K .......... .......... .......... .......... .......... 59%  106M 18s
297850K .......... .......... .......... .......... .......... 59% 25.4M 18s
297900K .......... .......... .......... .......... .......... 59% 31.9M 18s
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298000K .......... .......... .......... .......... .......... 59% 23.7M 18s
298050K .......... .......... .......... .......... .......... 59% 47.5M 18s
298100K .......... .......... .......... .......... .......... 59% 23.9M 18s
298150K .......... .......... .......... .......... .......... 59% 31.9M 18s
298200K .......... .......... .......... .......... .......... 59% 29.5M 18s
298250K .......... .......... .......... .......... .......... 59% 31.5M 18s
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298350K .......... .......... .......... .......... .......... 59% 24.6M 18s
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298450K .......... .......... .......... .......... .......... 59% 27.5M 18s
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298550K .......... .......... .......... .......... .......... 59% 47.0M 18s
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298650K .......... .......... .......... .......... .......... 59% 29.7M 18s
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298750K .......... .......... .......... .......... .......... 59% 34.4M 18s
298800K .......... .......... .......... .......... .......... 59% 30.2M 18s
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298900K .......... .......... .......... .......... .......... 59% 11.4M 18s
298950K .......... .......... .......... .......... .......... 59%  313M 18s
299000K .......... .......... .......... .......... .......... 59% 32.0M 18s
299050K .......... .......... .......... .......... .......... 59%  452M 18s
299100K .......... .......... .......... .......... .......... 59% 17.3M 18s
299150K .......... .......... .......... .......... .......... 59%  337M 18s
299200K .......... .......... .......... .......... .......... 59% 16.3M 18s
299250K .......... .......... .......... .......... .......... 59%  110M 18s
299300K .......... .......... .......... .......... .......... 59% 36.5M 18s
299350K .......... .......... .......... .......... .......... 59% 35.1M 18s
299400K .......... .......... .......... .......... .......... 59% 29.6M 18s
299450K .......... .......... .......... .......... .......... 59% 27.3M 18s
299500K .......... .......... .......... .......... .......... 59% 21.6M 18s
299550K .......... .......... .......... .......... .......... 59% 55.2M 18s
299600K .......... .......... .......... .......... .......... 59% 20.3M 18s
299650K .......... .......... .......... .......... .......... 59% 34.6M 18s
299700K .......... .......... .......... .......... .......... 59% 26.1M 18s
299750K .......... .......... .......... .......... .......... 59% 25.8M 17s
299800K .......... .......... .......... .......... .......... 59% 32.2M 17s
299850K .......... .......... .......... .......... .......... 59% 22.8M 17s
299900K .......... .......... .......... .......... .......... 59% 24.1M 17s
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300000K .......... .......... .......... .......... .......... 59% 24.1M 17s
300050K .......... .......... .......... .......... .......... 59% 35.0M 17s
300100K .......... .......... .......... .......... .......... 59% 25.6M 17s
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300250K .......... .......... .......... .......... .......... 59% 27.0M 17s
300300K .......... .......... .......... .......... .......... 59% 42.9M 17s
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300400K .......... .......... .......... .......... .......... 59% 31.5M 17s
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300500K .......... .......... .......... .......... .......... 59% 27.2M 17s
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300700K .......... .......... .......... .......... .......... 59% 18.2M 17s
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300950K .......... .......... .......... .......... .......... 59% 33.4M 17s
301000K .......... .......... .......... .......... .......... 59% 47.8M 17s
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301100K .......... .......... .......... .......... .......... 59% 27.3M 17s
301150K .......... .......... .......... .......... .......... 59% 25.3M 17s
301200K .......... .......... .......... .......... .......... 59% 25.4M 17s
301250K .......... .......... .......... .......... .......... 59% 24.0M 17s
301300K .......... .......... .......... .......... .......... 59% 32.1M 17s
301350K .......... .......... .......... .......... .......... 59% 21.2M 17s
301400K .......... .......... .......... .......... .......... 59% 41.9M 17s
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301500K .......... .......... .......... .......... .......... 59% 38.4M 17s
301550K .......... .......... .......... .......... .......... 59% 29.4M 17s
301600K .......... .......... .......... .......... .......... 59% 25.3M 17s
301650K .......... .......... .......... .......... .......... 59% 21.7M 17s
301700K .......... .......... .......... .......... .......... 59% 19.3M 17s
301750K .......... .......... .......... .......... .......... 59% 35.0M 17s
301800K .......... .......... .......... .......... .......... 59% 27.6M 17s
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301900K .......... .......... .......... .......... .......... 59% 45.1M 17s
301950K .......... .......... .......... .......... .......... 59% 20.4M 17s
302000K .......... .......... .......... .......... .......... 59% 22.3M 17s
302050K .......... .......... .......... .......... .......... 59%  183M 17s
302100K .......... .......... .......... .......... .......... 59% 13.2M 17s
302150K .......... .......... .......... .......... .......... 60%  166M 17s
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302250K .......... .......... .......... .......... .......... 60%  448M 17s
302300K .......... .......... .......... .......... .......... 60% 37.3M 17s
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302400K .......... .......... .......... .......... .......... 60% 18.3M 17s
302450K .......... .......... .......... .......... .......... 60% 50.3M 17s
302500K .......... .......... .......... .......... .......... 60% 51.0M 17s
302550K .......... .......... .......... .......... .......... 60%  119M 17s
302600K .......... .......... .......... .......... .......... 60% 24.3M 17s
302650K .......... .......... .......... .......... .......... 60% 42.7M 17s
302700K .......... .......... .......... .......... .......... 60% 21.2M 17s
302750K .......... .......... .......... .......... .......... 60% 22.3M 17s
302800K .......... .......... .......... .......... .......... 60% 27.4M 17s
302850K .......... .......... .......... .......... .......... 60% 25.2M 17s
302900K .......... .......... .......... .......... .......... 60% 25.3M 17s
302950K .......... .......... .......... .......... .......... 60% 21.1M 17s
303000K .......... .......... .......... .......... .......... 60% 37.4M 17s
303050K .......... .......... .......... .......... .......... 60% 21.1M 17s
303100K .......... .......... .......... .......... .......... 60% 25.5M 17s
303150K .......... .......... .......... .......... .......... 60% 27.6M 17s
303200K .......... .......... .......... .......... .......... 60% 27.0M 17s
303250K .......... .......... .......... .......... .......... 60% 25.6M 17s
303300K .......... .......... .......... .......... .......... 60% 28.9M 17s
303350K .......... .......... .......... .......... .......... 60% 22.4M 17s
303400K .......... .......... .......... .......... .......... 60% 31.9M 17s
303450K .......... .......... .......... .......... .......... 60% 26.8M 17s
303500K .......... .......... .......... .......... .......... 60% 21.5M 17s
303550K .......... .......... .......... .......... .......... 60% 18.8M 17s
303600K .......... .......... .......... .......... .......... 60% 11.9M 17s
303650K .......... .......... .......... .......... .......... 60% 16.6M 17s
303700K .......... .......... .......... .......... .......... 60%  367M 17s
303750K .......... .......... .......... .......... .......... 60% 15.1M 17s
303800K .......... .......... .......... .......... .......... 60% 21.4M 17s
303850K .......... .......... .......... .......... .......... 60% 21.8M 17s
303900K .......... .......... .......... .......... .......... 60% 29.2M 17s
303950K .......... .......... .......... .......... .......... 60% 18.1M 17s
304000K .......... .......... .......... .......... .......... 60% 27.2M 17s
304050K .......... .......... .......... .......... .......... 60% 29.3M 17s
304100K .......... .......... .......... .......... .......... 60% 18.1M 17s
304150K .......... .......... .......... .......... .......... 60% 27.3M 17s
304200K .......... .......... .......... .......... .......... 60% 19.0M 17s
304250K .......... .......... .......... .......... .......... 60% 29.3M 17s
304300K .......... .......... .......... .......... .......... 60% 24.1M 17s
304350K .......... .......... .......... .......... .......... 60% 23.0M 17s
304400K .......... .......... .......... .......... .......... 60% 23.6M 17s
304450K .......... .......... .......... .......... .......... 60% 22.7M 17s
304500K .......... .......... .......... .......... .......... 60% 25.2M 17s
304550K .......... .......... .......... .......... .......... 60% 25.7M 17s
304600K .......... .......... .......... .......... .......... 60% 20.2M 17s
304650K .......... .......... .......... .......... .......... 60% 26.9M 17s
304700K .......... .......... .......... .......... .......... 60% 8.50M 17s
304750K .......... .......... .......... .......... .......... 60%  479M 17s
304800K .......... .......... .......... .......... .......... 60% 18.5M 17s
304850K .......... .......... .......... .......... .......... 60% 57.6M 17s
304900K .......... .......... .......... .......... .......... 60% 10.5M 17s
304950K .......... .......... .......... .......... .......... 60%  397M 17s
305000K .......... .......... .......... .......... .......... 60% 26.6M 17s
305050K .......... .......... .......... .......... .......... 60% 17.3M 17s
305100K .......... .......... .......... .......... .......... 60%  317M 17s
305150K .......... .......... .......... .......... .......... 60% 29.1M 17s
305200K .......... .......... .......... .......... .......... 60% 27.2M 17s
305250K .......... .......... .......... .......... .......... 60% 25.7M 17s
305300K .......... .......... .......... .......... .......... 60% 28.3M 17s
305350K .......... .......... .......... .......... .......... 60% 24.0M 17s
305400K .......... .......... .......... .......... .......... 60% 25.7M 17s
305450K .......... .......... .......... .......... .......... 60% 33.8M 17s
305500K .......... .......... .......... .......... .......... 60% 26.0M 17s
305550K .......... .......... .......... .......... .......... 60% 34.3M 17s
305600K .......... .......... .......... .......... .......... 60% 27.3M 17s
305650K .......... .......... .......... .......... .......... 60% 29.2M 17s
305700K .......... .......... .......... .......... .......... 60% 28.5M 17s
305750K .......... .......... .......... .......... .......... 60% 37.4M 17s
305800K .......... .......... .......... .......... .......... 60% 27.6M 17s
305850K .......... .......... .......... .......... .......... 60% 23.7M 17s
305900K .......... .......... .......... .......... .......... 60% 43.6M 17s
305950K .......... .......... .......... .......... .......... 60% 29.7M 17s
306000K .......... .......... .......... .......... .......... 60% 34.8M 17s
306050K .......... .......... .......... .......... .......... 60% 27.1M 17s
306100K .......... .......... .......... .......... .......... 60% 25.1M 17s
306150K .......... .......... .......... .......... .......... 60% 38.5M 17s
306200K .......... .......... .......... .......... .......... 60% 27.1M 17s
306250K .......... .......... .......... .......... .......... 60% 30.4M 17s
306300K .......... .......... .......... .......... .......... 60% 34.9M 17s
306350K .......... .......... .......... .......... .......... 60% 11.9M 17s
306400K .......... .......... .......... .......... .......... 60%  428M 17s
306450K .......... .......... .......... .......... .......... 60%  216M 17s
306500K .......... .......... .......... .......... .......... 60% 15.9M 17s
306550K .......... .......... .......... .......... .......... 60% 35.4M 17s
306600K .......... .......... .......... .......... .......... 60% 39.7M 17s
306650K .......... .......... .......... .......... .......... 60% 24.2M 17s
306700K .......... .......... .......... .......... .......... 60% 20.4M 17s
306750K .......... .......... .......... .......... .......... 60% 34.9M 17s
306800K .......... .......... .......... .......... .......... 60% 24.3M 17s
306850K .......... .......... .......... .......... .......... 60% 18.3M 17s
306900K .......... .......... .......... .......... .......... 60% 25.7M 17s
306950K .......... .......... .......... .......... .......... 60% 22.9M 17s
307000K .......... .......... .......... .......... .......... 60% 25.6M 17s
307050K .......... .......... .......... .......... .......... 60% 29.6M 17s
307100K .......... .......... .......... .......... .......... 60% 22.6M 17s
307150K .......... .......... .......... .......... .......... 61% 25.7M 17s
307200K .......... .......... .......... .......... .......... 61% 25.8M 17s
307250K .......... .......... .......... .......... .......... 61% 25.8M 17s
307300K .......... .......... .......... .......... .......... 61% 24.1M 17s
307350K .......... .......... .......... .......... .......... 61% 25.4M 17s
307400K .......... .......... .......... .......... .......... 61% 22.8M 17s
307450K .......... .......... .......... .......... .......... 61% 21.6M 17s
307500K .......... .......... .......... .......... .......... 61% 23.9M 17s
307550K .......... .......... .......... .......... .......... 61% 22.8M 17s
307600K .......... .......... .......... .......... .......... 61% 41.4M 17s
307650K .......... .......... .......... .......... .......... 61% 65.4M 17s
307700K .......... .......... .......... .......... .......... 61% 48.8M 17s
307750K .......... .......... .......... .......... .......... 61% 19.2M 17s
307800K .......... .......... .......... .......... .......... 61%  109M 17s
307850K .......... .......... .......... .......... .......... 61%  391M 17s
307900K .......... .......... .......... .......... .......... 61%  154M 17s
307950K .......... .......... .......... .......... .......... 61% 20.1M 17s
308000K .......... .......... .......... .......... .......... 61%  359M 17s
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308100K .......... .......... .......... .......... .......... 61% 38.2M 17s
308150K .......... .......... .......... .......... .......... 61% 54.4M 17s
308200K .......... .......... .......... .......... .......... 61% 42.5M 16s
308250K .......... .......... .......... .......... .......... 61% 48.5M 16s
308300K .......... .......... .......... .......... .......... 61% 34.8M 16s
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308400K .......... .......... .......... .......... .......... 61% 19.2M 16s
308450K .......... .......... .......... .......... .......... 61%  341M 16s
308500K .......... .......... .......... .......... .......... 61% 35.3M 16s
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308600K .......... .......... .......... .......... .......... 61% 32.1M 16s
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308700K .......... .......... .......... .......... .......... 61% 34.7M 16s
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308800K .......... .......... .......... .......... .......... 61% 38.5M 16s
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308900K .......... .......... .......... .......... .......... 61% 27.6M 16s
308950K .......... .......... .......... .......... .......... 61% 42.9M 16s
309000K .......... .......... .......... .......... .......... 61% 27.5M 16s
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309100K .......... .......... .......... .......... .......... 61% 38.8M 16s
309150K .......... .......... .......... .......... .......... 61% 35.0M 16s
309200K .......... .......... .......... .......... .......... 61% 38.2M 16s
309250K .......... .......... .......... .......... .......... 61% 54.4M 16s
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309400K .......... .......... .......... .......... .......... 61% 42.7M 16s
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309600K .......... .......... .......... .......... .......... 61% 23.8M 16s
309650K .......... .......... .......... .......... .......... 61% 7.34M 16s
309700K .......... .......... .......... .......... .......... 61%  417M 16s
309750K .......... .......... .......... .......... .......... 61%  440M 16s
309800K .......... .......... .......... .......... .......... 61% 16.9M 16s
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309900K .......... .......... .......... .......... .......... 61% 30.2M 16s
309950K .......... .......... .......... .......... .......... 61% 16.8M 16s
310000K .......... .......... .......... .......... .......... 61% 22.7M 16s
310050K .......... .......... .......... .......... .......... 61% 21.3M 16s
310100K .......... .......... .......... .......... .......... 61% 14.4M 16s
310150K .......... .......... .......... .......... .......... 61% 24.2M 16s
310200K .......... .......... .......... .......... .......... 61% 18.4M 16s
310250K .......... .......... .......... .......... .......... 61% 18.4M 16s
310300K .......... .......... .......... .......... .......... 61% 20.4M 16s
310350K .......... .......... .......... .......... .......... 61% 16.8M 16s
310400K .......... .......... .......... .......... .......... 61% 27.3M 16s
310450K .......... .......... .......... .......... .......... 61% 16.1M 16s
310500K .......... .......... .......... .......... .......... 61% 19.5M 16s
310550K .......... .......... .......... .......... .......... 61% 23.9M 16s
310600K .......... .......... .......... .......... .......... 61% 35.6M 16s
310650K .......... .......... .......... .......... .......... 61% 34.6M 16s
310700K .......... .......... .......... .......... .......... 61% 14.1M 16s
310750K .......... .......... .......... .......... .......... 61% 28.7M 16s
310800K .......... .......... .......... .......... .......... 61%  391M 16s
310850K .......... .......... .......... .......... .......... 61% 21.3M 16s
310900K .......... .......... .......... .......... .......... 61% 38.9M 16s
310950K .......... .......... .......... .......... .......... 61% 54.7M 16s
311000K .......... .......... .......... .......... .......... 61% 27.2M 16s
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311100K .......... .......... .......... .......... .......... 61% 26.0M 16s
311150K .......... .......... .......... .......... .......... 61% 29.7M 16s
311200K .......... .......... .......... .......... .......... 61% 32.1M 16s
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311300K .......... .......... .......... .......... .......... 61% 17.5M 16s
311350K .......... .......... .......... .......... .......... 61% 77.6M 16s
311400K .......... .......... .......... .......... .......... 61% 27.6M 16s
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311500K .......... .......... .......... .......... .......... 61% 20.5M 16s
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311600K .......... .......... .......... .......... .......... 61% 27.5M 16s
311650K .......... .......... .......... .......... .......... 61% 21.5M 16s
311700K .......... .......... .......... .......... .......... 61% 27.4M 16s
311750K .......... .......... .......... .......... .......... 61% 26.0M 16s
311800K .......... .......... .......... .......... .......... 61% 27.5M 16s
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311900K .......... .......... .......... .......... .......... 61% 25.7M 16s
311950K .......... .......... .......... .......... .......... 61% 25.3M 16s
312000K .......... .......... .......... .......... .......... 61% 16.9M 16s
312050K .......... .......... .......... .......... .......... 61% 11.0M 16s
312100K .......... .......... .......... .......... .......... 61% 15.4M 16s
312150K .......... .......... .......... .......... .......... 61% 19.3M 16s
312200K .......... .......... .......... .......... .......... 62% 18.1M 16s
312250K .......... .......... .......... .......... .......... 62% 18.2M 16s
312300K .......... .......... .......... .......... .......... 62% 20.2M 16s
312350K .......... .......... .......... .......... .......... 62% 13.7M 16s
312400K .......... .......... .......... .......... .......... 62% 14.1M 16s
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312500K .......... .......... .......... .......... .......... 62% 19.5M 16s
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312600K .......... .......... .......... .......... .......... 62% 14.5M 16s
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312700K .......... .......... .......... .......... .......... 62% 42.2M 16s
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312850K .......... .......... .......... .......... .......... 62% 11.1M 16s
312900K .......... .......... .......... .......... .......... 62%  168M 16s
312950K .......... .......... .......... .......... .......... 62%  142M 16s
313000K .......... .......... .......... .......... .......... 62% 21.5M 16s
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313100K .......... .......... .......... .......... .......... 62% 13.7M 16s
313150K .......... .......... .......... .......... .......... 62% 93.5M 16s
313200K .......... .......... .......... .......... .......... 62% 23.2M 16s
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313300K .......... .......... .......... .......... .......... 62% 24.2M 16s
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313400K .......... .......... .......... .......... .......... 62% 32.1M 16s
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313500K .......... .......... .......... .......... .......... 62% 35.0M 16s
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313700K .......... .......... .......... .......... .......... 62% 21.5M 16s
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313800K .......... .......... .......... .......... .......... 62% 24.3M 16s
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313900K .......... .......... .......... .......... .......... 62% 24.1M 16s
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314000K .......... .......... .......... .......... .......... 62% 27.7M 16s
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314100K .......... .......... .......... .......... .......... 62% 9.67M 16s
314150K .......... .......... .......... .......... .......... 62% 35.1M 16s
314200K .......... .......... .......... .......... .......... 62%  140M 16s
314250K .......... .......... .......... .......... .......... 62% 14.7M 16s
314300K .......... .......... .......... .......... .......... 62% 42.2M 16s
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314400K .......... .......... .......... .......... .......... 62% 24.0M 16s
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314600K .......... .......... .......... .......... .......... 62% 25.3M 16s
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314700K .......... .......... .......... .......... .......... 62% 17.5M 16s
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314800K .......... .......... .......... .......... .......... 62% 8.04M 16s
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315000K .......... .......... .......... .......... .......... 62% 22.8M 16s
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315100K .......... .......... .......... .......... .......... 62% 22.6M 16s
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315200K .......... .......... .......... .......... .......... 62%  281M 16s
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315300K .......... .......... .......... .......... .......... 62% 33.4M 16s
315350K .......... .......... .......... .......... .......... 62% 67.7M 16s
315400K .......... .......... .......... .......... .......... 62% 35.4M 16s
315450K .......... .......... .......... .......... .......... 62% 29.1M 16s
315500K .......... .......... .......... .......... .......... 62% 36.5M 16s
315550K .......... .......... .......... .......... .......... 62% 42.3M 16s
315600K .......... .......... .......... .......... .......... 62% 33.2M 16s
315650K .......... .......... .......... .......... .......... 62% 46.2M 16s
315700K .......... .......... .......... .......... .......... 62% 38.6M 16s
315750K .......... .......... .......... .......... .......... 62% 33.8M 16s
315800K .......... .......... .......... .......... .......... 62% 39.8M 16s
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315900K .......... .......... .......... .......... .......... 62% 43.2M 16s
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316000K .......... .......... .......... .......... .......... 62% 51.6M 16s
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316100K .......... .......... .......... .......... .......... 62% 45.0M 16s
316150K .......... .......... .......... .......... .......... 62% 34.9M 16s
316200K .......... .......... .......... .......... .......... 62% 35.1M 16s
316250K .......... .......... .......... .......... .......... 62% 42.7M 16s
316300K .......... .......... .......... .......... .......... 62% 38.6M 16s
316350K .......... .......... .......... .......... .......... 62% 35.1M 16s
316400K .......... .......... .......... .......... .......... 62% 48.3M 16s
316450K .......... .......... .......... .......... .......... 62% 42.5M 16s
316500K .......... .......... .......... .......... .......... 62% 38.5M 16s
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316600K .......... .......... .......... .......... .......... 62% 29.7M 16s
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316700K .......... .......... .......... .......... .......... 62% 37.8M 16s
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316800K .......... .......... .......... .......... .......... 62%  311M 16s
316850K .......... .......... .......... .......... .......... 62% 70.3M 16s
316900K .......... .......... .......... .......... .......... 62%  493M 16s
316950K .......... .......... .......... .......... .......... 62% 27.8M 16s
317000K .......... .......... .......... .......... .......... 62% 50.6M 16s
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317150K .......... .......... .......... .......... .......... 62%  425M 15s
317200K .......... .......... .......... .......... .......... 62%  448M 15s
317250K .......... .......... .......... .......... .......... 63% 29.0M 15s
317300K .......... .......... .......... .......... .......... 63% 42.9M 15s
317350K .......... .......... .......... .......... .......... 63% 24.2M 15s
317400K .......... .......... .......... .......... .......... 63% 27.2M 15s
317450K .......... .......... .......... .......... .......... 63% 41.9M 15s
317500K .......... .......... .......... .......... .......... 63% 28.6M 15s
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317600K .......... .......... .......... .......... .......... 63% 28.7M 15s
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317700K .......... .......... .......... .......... .......... 63% 25.4M 15s
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317800K .......... .......... .......... .......... .......... 63% 26.7M 15s
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317900K .......... .......... .......... .......... .......... 63% 27.3M 15s
317950K .......... .......... .......... .......... .......... 63% 23.9M 15s
318000K .......... .......... .......... .......... .......... 63% 22.9M 15s
318050K .......... .......... .......... .......... .......... 63% 41.3M 15s
318100K .......... .......... .......... .......... .......... 63% 19.1M 15s
318150K .......... .......... .......... .......... .......... 63% 34.2M 15s
318200K .......... .......... .......... .......... .......... 63% 19.0M 15s
318250K .......... .......... .......... .......... .......... 63% 42.3M 15s
318300K .......... .......... .......... .......... .......... 63% 22.4M 15s
318350K .......... .......... .......... .......... .......... 63% 22.5M 15s
318400K .......... .......... .......... .......... .......... 63%  263M 15s
318450K .......... .......... .......... .......... .......... 63% 28.7M 15s
318500K .......... .......... .......... .......... .......... 63% 39.7M 15s
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318600K .......... .......... .......... .......... .......... 63% 34.5M 15s
318650K .......... .......... .......... .......... .......... 63% 42.3M 15s
318700K .......... .......... .......... .......... .......... 63% 38.1M 15s
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318800K .......... .......... .......... .......... .......... 63% 23.7M 15s
318850K .......... .......... .......... .......... .......... 63% 66.1M 15s
318900K .......... .......... .......... .......... .......... 63% 31.5M 15s
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319000K .......... .......... .......... .......... .......... 63% 32.1M 15s
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319100K .......... .......... .......... .......... .......... 63% 29.6M 15s
319150K .......... .......... .......... .......... .......... 63% 38.3M 15s
319200K .......... .......... .......... .......... .......... 63% 29.7M 15s
319250K .......... .......... .......... .......... .......... 63% 34.8M 15s
319300K .......... .......... .......... .......... .......... 63% 38.2M 15s
319350K .......... .......... .......... .......... .......... 63% 24.1M 15s
319400K .......... .......... .......... .......... .......... 63% 38.4M 15s
319450K .......... .......... .......... .......... .......... 63% 29.3M 15s
319500K .......... .......... .......... .......... .......... 63% 27.8M 15s
319550K .......... .......... .......... .......... .......... 63% 47.2M 15s
319600K .......... .......... .......... .......... .......... 63% 27.9M 15s
319650K .......... .......... .......... .......... .......... 63% 23.9M 15s
319700K .......... .......... .......... .......... .......... 63% 12.8M 15s
319750K .......... .......... .......... .......... .......... 63% 29.7M 15s
319800K .......... .......... .......... .......... .......... 63% 27.4M 15s
319850K .......... .......... .......... .......... .......... 63% 18.3M 15s
319900K .......... .......... .......... .......... .......... 63% 29.6M 15s
319950K .......... .......... .......... .......... .......... 63% 15.1M 15s
320000K .......... .......... .......... .......... .......... 63% 21.1M 15s
320050K .......... .......... .......... .......... .......... 63% 22.1M 15s
320100K .......... .......... .......... .......... .......... 63% 18.4M 15s
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320200K .......... .......... .......... .......... .......... 63% 15.3M 15s
320250K .......... .......... .......... .......... .......... 63% 16.6M 15s
320300K .......... .......... .......... .......... .......... 63% 16.6M 15s
320350K .......... .......... .......... .......... .......... 63% 12.1M 15s
320400K .......... .......... .......... .......... .......... 63% 17.4M 15s
320450K .......... .......... .......... .......... .......... 63% 14.9M 15s
320500K .......... .......... .......... .......... .......... 63% 13.1M 15s
320550K .......... .......... .......... .......... .......... 63% 17.4M 15s
320600K .......... .......... .......... .......... .......... 63% 17.0M 15s
320650K .......... .......... .......... .......... .......... 63% 11.8M 15s
320700K .......... .......... .......... .......... .......... 63% 13.9M 15s
320750K .......... .......... .......... .......... .......... 63% 8.46M 15s
320800K .......... .......... .......... .......... .......... 63% 12.5M 15s
320850K .......... .......... .......... .......... .......... 63% 9.96M 15s
320900K .......... .......... .......... .......... .......... 63% 7.42M 15s
320950K .......... .......... .......... .......... .......... 63% 10.6M 15s
321000K .......... .......... .......... .......... .......... 63% 11.2M 15s
321050K .......... .......... .......... .......... .......... 63% 10.5M 15s
321100K .......... .......... .......... .......... .......... 63% 9.52M 15s
321150K .......... .......... .......... .......... .......... 63% 14.5M 15s
321200K .......... .......... .......... .......... .......... 63% 14.2M 15s
321250K .......... .......... .......... .......... .......... 63%  279M 15s
321300K .......... .......... .......... .......... .......... 63% 19.7M 15s
321350K .......... .......... .......... .......... .......... 63% 23.4M 15s
321400K .......... .......... .......... .......... .......... 63% 20.9M 15s
321450K .......... .......... .......... .......... .......... 63% 20.9M 15s
321500K .......... .......... .......... .......... .......... 63% 21.1M 15s
321550K .......... .......... .......... .......... .......... 63% 23.4M 15s
321600K .......... .......... .......... .......... .......... 63% 16.4M 15s
321650K .......... .......... .......... .......... .......... 63% 20.0M 15s
321700K .......... .......... .......... .......... .......... 63% 18.6M 15s
321750K .......... .......... .......... .......... .......... 63% 18.9M 15s
321800K .......... .......... .......... .......... .......... 63% 24.2M 15s
321850K .......... .......... .......... .......... .......... 63% 11.0M 15s
321900K .......... .......... .......... .......... .......... 63% 18.2M 15s
321950K .......... .......... .......... .......... .......... 63% 14.4M 15s
322000K .......... .......... .......... .......... .......... 63% 22.1M 15s
322050K .......... .......... .......... .......... .......... 63% 13.1M 15s
322100K .......... .......... .......... .......... .......... 63% 14.1M 15s
322150K .......... .......... .......... .......... .......... 63% 14.7M 15s
322200K .......... .......... .......... .......... .......... 63% 15.7M 15s
322250K .......... .......... .......... .......... .......... 63% 14.8M 15s
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322350K .......... .......... .......... .......... .......... 64% 11.7M 15s
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322500K .......... .......... .......... .......... .......... 64% 13.2M 15s
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322600K .......... .......... .......... .......... .......... 64% 6.34M 15s
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322700K .......... .......... .......... .......... .......... 64% 8.37M 15s
322750K .......... .......... .......... .......... .......... 64% 9.69M 15s
322800K .......... .......... .......... .......... .......... 64% 11.2M 15s
322850K .......... .......... .......... .......... .......... 64% 6.05M 15s
322900K .......... .......... .......... .......... .......... 64% 7.85M 15s
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323000K .......... .......... .......... .......... .......... 64% 11.1M 15s
323050K .......... .......... .......... .......... .......... 64% 29.2M 15s
323100K .......... .......... .......... .......... .......... 64% 33.5M 15s
323150K .......... .......... .......... .......... .......... 64% 37.6M 15s
323200K .......... .......... .......... .......... .......... 64% 21.3M 15s
323250K .......... .......... .......... .......... .......... 64%  102M 15s
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323700K .......... .......... .......... .......... .......... 64% 26.0M 15s
323750K .......... .......... .......... .......... .......... 64% 47.4M 15s
323800K .......... .......... .......... .......... .......... 64% 22.9M 15s
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323900K .......... .......... .......... .......... .......... 64% 38.4M 15s
323950K .......... .......... .......... .......... .......... 64% 27.3M 15s
324000K .......... .......... .......... .......... .......... 64% 26.0M 15s
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324100K .......... .......... .......... .......... .......... 64% 27.2M 15s
324150K .......... .......... .......... .......... .......... 64% 23.0M 15s
324200K .......... .......... .......... .......... .......... 64% 25.7M 15s
324250K .......... .......... .......... .......... .......... 64% 38.2M 15s
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324450K .......... .......... .......... .......... .......... 64% 95.4M 15s
324500K .......... .......... .......... .......... .......... 64% 19.7M 15s
324550K .......... .......... .......... .......... .......... 64%  470M 15s
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324650K .......... .......... .......... .......... .......... 64% 68.6M 15s
324700K .......... .......... .......... .......... .......... 64% 29.5M 15s
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324800K .......... .......... .......... .......... .......... 64% 21.4M 15s
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324900K .......... .......... .......... .......... .......... 64% 18.5M 15s
324950K .......... .......... .......... .......... .......... 64% 16.1M 15s
325000K .......... .......... .......... .......... .......... 64% 21.4M 15s
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325100K .......... .......... .......... .......... .......... 64% 16.7M 15s
325150K .......... .......... .......... .......... .......... 64% 21.3M 15s
325200K .......... .......... .......... .......... .......... 64% 16.7M 15s
325250K .......... .......... .......... .......... .......... 64% 17.0M 15s
325300K .......... .......... .......... .......... .......... 64% 15.4M 15s
325350K .......... .......... .......... .......... .......... 64% 16.7M 15s
325400K .......... .......... .......... .......... .......... 64% 19.2M 15s
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325500K .......... .......... .......... .......... .......... 64% 22.6M 15s
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325650K .......... .......... .......... .......... .......... 64% 24.2M 15s
325700K .......... .......... .......... .......... .......... 64% 24.1M 15s
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325800K .......... .......... .......... .......... .......... 64%  391M 15s
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325900K .......... .......... .......... .......... .......... 64% 12.4M 15s
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326000K .......... .......... .......... .......... .......... 64% 64.2M 15s
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326100K .......... .......... .......... .......... .......... 64% 19.1M 15s
326150K .......... .......... .......... .......... .......... 64% 16.7M 15s
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326250K .......... .......... .......... .......... .......... 64% 12.8M 15s
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326900K .......... .......... .......... .......... .......... 64% 10.1M 15s
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327000K .......... .......... .......... .......... .......... 64% 17.9M 15s
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327100K .......... .......... .......... .......... .......... 64% 12.9M 14s
327150K .......... .......... .......... .......... .......... 64% 35.3M 14s
327200K .......... .......... .......... .......... .......... 64% 11.1M 14s
327250K .......... .......... .......... .......... .......... 64% 19.4M 14s
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327850K .......... .......... .......... .......... .......... 65% 10.7M 14s
327900K .......... .......... .......... .......... .......... 65%  210M 14s
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328000K .......... .......... .......... .......... .......... 65% 44.2M 14s
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328100K .......... .......... .......... .......... .......... 65% 16.1M 14s
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328250K .......... .......... .......... .......... .......... 65% 20.4M 14s
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329000K .......... .......... .......... .......... .......... 65% 14.3M 14s
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329250K .......... .......... .......... .......... .......... 65% 42.4M 14s
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330000K .......... .......... .......... .......... .......... 65% 12.4M 14s
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330100K .......... .......... .......... .......... .......... 65% 14.9M 14s
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330200K .......... .......... .......... .......... .......... 65% 11.7M 14s
330250K .......... .......... .......... .......... .......... 65% 14.3M 14s
330300K .......... .......... .......... .......... .......... 65% 13.7M 14s
330350K .......... .......... .......... .......... .......... 65% 11.5M 14s
330400K .......... .......... .......... .......... .......... 65% 14.4M 14s
330450K .......... .......... .......... .......... .......... 65% 11.4M 14s
330500K .......... .......... .......... .......... .......... 65% 13.4M 14s
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330600K .......... .......... .......... .......... .......... 65%  135M 14s
330650K .......... .......... .......... .......... .......... 65% 14.4M 14s
330700K .......... .......... .......... .......... .......... 65% 12.1M 14s
330750K .......... .......... .......... .......... .......... 65% 35.1M 14s
330800K .......... .......... .......... .......... .......... 65% 18.3M 14s
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330900K .......... .......... .......... .......... .......... 65% 22.3M 14s
330950K .......... .......... .......... .......... .......... 65% 11.5M 14s
331000K .......... .......... .......... .......... .......... 65% 16.1M 14s
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331400K .......... .......... .......... .......... .......... 65% 16.1M 14s
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331500K .......... .......... .......... .......... .......... 65% 10.4M 14s
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331600K .......... .......... .......... .......... .......... 65% 12.9M 14s
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331700K .......... .......... .......... .......... .......... 65% 13.8M 14s
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331900K .......... .......... .......... .......... .......... 65% 14.4M 14s
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332000K .......... .......... .......... .......... .......... 65% 12.1M 14s
332050K .......... .......... .......... .......... .......... 65% 11.4M 14s
332100K .......... .......... .......... .......... .......... 65% 7.43M 14s
332150K .......... .......... .......... .......... .......... 65% 9.44M 14s
332200K .......... .......... .......... .......... .......... 65% 9.00M 14s
332250K .......... .......... .......... .......... .......... 65% 7.76M 14s
332300K .......... .......... .......... .......... .......... 65% 11.4M 14s
332350K .......... .......... .......... .......... .......... 66% 5.88M 14s
332400K .......... .......... .......... .......... .......... 66% 8.08M 14s
332450K .......... .......... .......... .......... .......... 66% 19.2M 14s
332500K .......... .......... .......... .......... .......... 66% 11.6M 14s
332550K .......... .......... .......... .......... .......... 66% 15.8M 14s
332600K .......... .......... .......... .......... .......... 66% 21.4M 14s
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332700K .......... .......... .......... .......... .......... 66% 23.9M 14s
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332800K .......... .......... .......... .......... .......... 66% 24.3M 14s
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332900K .......... .......... .......... .......... .......... 66% 22.7M 14s
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333000K .......... .......... .......... .......... .......... 66% 25.8M 14s
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333100K .......... .......... .......... .......... .......... 66% 25.4M 14s
333150K .......... .......... .......... .......... .......... 66% 25.8M 14s
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333250K .......... .......... .......... .......... .......... 66% 27.6M 14s
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333350K .......... .......... .......... .......... .......... 66% 25.8M 14s
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333500K .......... .......... .......... .......... .......... 66% 20.4M 14s
333550K .......... .......... .......... .......... .......... 66% 34.7M 14s
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333700K .......... .......... .......... .......... .......... 66% 23.4M 14s
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333800K .......... .......... .......... .......... .......... 66% 55.4M 14s
333850K .......... .......... .......... .......... .......... 66% 18.9M 14s
333900K .......... .......... .......... .......... .......... 66% 30.5M 14s
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334000K .......... .......... .......... .......... .......... 66% 20.3M 14s
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334100K .......... .......... .......... .......... .......... 66% 16.8M 14s
334150K .......... .......... .......... .......... .......... 66% 25.5M 14s
334200K .......... .......... .......... .......... .......... 66% 16.3M 14s
334250K .......... .......... .......... .......... .......... 66% 25.4M 14s
334300K .......... .......... .......... .......... .......... 66% 17.0M 14s
334350K .......... .......... .......... .......... .......... 66% 20.3M 14s
334400K .......... .......... .......... .......... .......... 66% 27.2M 14s
334450K .......... .......... .......... .......... .......... 66% 19.3M 14s
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334600K .......... .......... .......... .......... .......... 66% 24.5M 14s
334650K .......... .......... .......... .......... .......... 66% 22.8M 14s
334700K .......... .......... .......... .......... .......... 66% 24.2M 14s
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334800K .......... .......... .......... .......... .......... 66% 27.4M 14s
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334900K .......... .......... .......... .......... .......... 66% 19.2M 14s
334950K .......... .......... .......... .......... .......... 66% 33.3M 14s
335000K .......... .......... .......... .......... .......... 66% 47.9M 14s
335050K .......... .......... .......... .......... .......... 66% 43.9M 14s
335100K .......... .......... .......... .......... .......... 66% 36.0M 14s
335150K .......... .......... .......... .......... .......... 66% 27.5M 14s
335200K .......... .......... .......... .......... .......... 66% 20.3M 14s
335250K .......... .......... .......... .......... .......... 66% 27.5M 14s
335300K .......... .......... .......... .......... .......... 66% 21.5M 14s
335350K .......... .......... .......... .......... .......... 66% 22.7M 14s
335400K .......... .......... .......... .......... .......... 66% 25.7M 14s
335450K .......... .......... .......... .......... .......... 66% 25.5M 14s
335500K .......... .......... .......... .......... .......... 66% 27.6M 14s
335550K .......... .......... .......... .......... .......... 66% 25.7M 14s
335600K .......... .......... .......... .......... .......... 66% 24.4M 14s
335650K .......... .......... .......... .......... .......... 66% 24.1M 14s
335700K .......... .......... .......... .......... .......... 66% 21.4M 14s
335750K .......... .......... .......... .......... .......... 66% 27.6M 14s
335800K .......... .......... .......... .......... .......... 66% 27.5M 14s
335850K .......... .......... .......... .......... .......... 66% 17.5M 14s
335900K .......... .......... .......... .......... .......... 66% 27.6M 14s
335950K .......... .......... .......... .......... .......... 66% 23.9M 14s
336000K .......... .......... .......... .......... .......... 66% 35.1M 14s
336050K .......... .......... .......... .......... .......... 66% 25.5M 14s
336100K .......... .......... .......... .......... .......... 66% 11.4M 14s
336150K .......... .......... .......... .......... .......... 66%  428M 14s
336200K .......... .......... .......... .......... .......... 66% 24.1M 14s
336250K .......... .......... .......... .......... .......... 66% 52.8M 14s
336300K .......... .......... .......... .......... .......... 66% 27.8M 14s
336350K .......... .......... .......... .......... .......... 66% 43.8M 14s
336400K .......... .......... .......... .......... .......... 66% 21.3M 14s
336450K .......... .......... .......... .......... .......... 66% 18.5M 14s
336500K .......... .......... .......... .......... .......... 66% 15.4M 14s
336550K .......... .......... .......... .......... .......... 66% 24.4M 14s
336600K .......... .......... .......... .......... .......... 66% 21.5M 14s
336650K .......... .......... .......... .......... .......... 66% 17.5M 14s
336700K .......... .......... .......... .......... .......... 66% 15.5M 14s
336750K .......... .......... .......... .......... .......... 66% 24.3M 14s
336800K .......... .......... .......... .......... .......... 66% 22.8M 14s
336850K .......... .......... .......... .......... .......... 66% 14.8M 14s
336900K .......... .......... .......... .......... .......... 66% 21.3M 14s
336950K .......... .......... .......... .......... .......... 66% 17.0M 14s
337000K .......... .......... .......... .......... .......... 66% 24.1M 14s
337050K .......... .......... .......... .......... .......... 66% 18.0M 14s
337100K .......... .......... .......... .......... .......... 66% 23.3M 14s
337150K .......... .......... .......... .......... .......... 66% 16.2M 14s
337200K .......... .......... .......... .......... .......... 66% 28.5M 14s
337250K .......... .......... .......... .......... .......... 66% 35.1M 14s
337300K .......... .......... .......... .......... .......... 66% 44.6M 14s
337350K .......... .......... .......... .......... .......... 66% 38.2M 14s
337400K .......... .......... .......... .......... .......... 67% 37.8M 14s
337450K .......... .......... .......... .......... .......... 67% 16.7M 14s
337500K .......... .......... .......... .......... .......... 67% 56.4M 14s
337550K .......... .......... .......... .......... .......... 67%  407M 13s
337600K .......... .......... .......... .......... .......... 67% 24.9M 13s
337650K .......... .......... .......... .......... .......... 67%  105M 13s
337700K .......... .......... .......... .......... .......... 67% 25.5M 13s
337750K .......... .......... .......... .......... .......... 67% 27.4M 13s
337800K .......... .......... .......... .......... .......... 67% 22.7M 13s
337850K .......... .......... .......... .......... .......... 67% 21.4M 13s
337900K .......... .......... .......... .......... .......... 67% 25.7M 13s
337950K .......... .......... .......... .......... .......... 67% 27.6M 13s
338000K .......... .......... .......... .......... .......... 67% 34.8M 13s
338050K .......... .......... .......... .......... .......... 67% 24.2M 13s
338100K .......... .......... .......... .......... .......... 67% 24.0M 13s
338150K .......... .......... .......... .......... .......... 67% 22.7M 13s
338200K .......... .......... .......... .......... .......... 67% 29.5M 13s
338250K .......... .......... .......... .......... .......... 67% 29.7M 13s
338300K .......... .......... .......... .......... .......... 67% 34.8M 13s
338350K .......... .......... .......... .......... .......... 67% 22.5M 13s
338400K .......... .......... .......... .......... .......... 67% 28.0M 13s
338450K .......... .......... .......... .......... .......... 67% 25.6M 13s
338500K .......... .......... .......... .......... .......... 67% 25.5M 13s
338550K .......... .......... .......... .......... .......... 67% 24.1M 13s
338600K .......... .......... .......... .......... .......... 67% 20.6M 13s
338650K .......... .......... .......... .......... .......... 67% 42.2M 13s
338700K .......... .......... .......... .......... .......... 67% 35.6M 13s
338750K .......... .......... .......... .......... .......... 67% 13.9M 13s
338800K .......... .......... .......... .......... .......... 67% 34.9M 13s
338850K .......... .......... .......... .......... .......... 67%  400M 13s
338900K .......... .......... .......... .......... .......... 67% 38.7M 13s
338950K .......... .......... .......... .......... .......... 67% 84.5M 13s
339000K .......... .......... .......... .......... .......... 67% 26.2M 13s
339050K .......... .......... .......... .......... .......... 67% 22.8M 13s
339100K .......... .......... .......... .......... .......... 67% 25.1M 13s
339150K .......... .......... .......... .......... .......... 67% 25.7M 13s
339200K .......... .......... .......... .......... .......... 67% 25.9M 13s
339250K .......... .......... .......... .......... .......... 67% 23.9M 13s
339300K .......... .......... .......... .......... .......... 67% 28.0M 13s
339350K .......... .......... .......... .......... .......... 67% 24.0M 13s
339400K .......... .......... .......... .......... .......... 67% 27.7M 13s
339450K .......... .......... .......... .......... .......... 67% 15.5M 13s
339500K .......... .......... .......... .......... .......... 67% 25.8M 13s
339550K .......... .......... .......... .......... .......... 67% 29.4M 13s
339600K .......... .......... .......... .......... .......... 67% 21.8M 13s
339650K .......... .......... .......... .......... .......... 67% 25.2M 13s
339700K .......... .......... .......... .......... .......... 67% 17.5M 13s
339750K .......... .......... .......... .......... .......... 67% 25.6M 13s
339800K .......... .......... .......... .......... .......... 67% 27.5M 13s
339850K .......... .......... .......... .......... .......... 67% 24.3M 13s
339900K .......... .......... .......... .......... .......... 67% 25.7M 13s
339950K .......... .......... .......... .......... .......... 67% 29.7M 13s
340000K .......... .......... .......... .......... .......... 67% 29.3M 13s
340050K .......... .......... .......... .......... .......... 67% 21.9M 13s
340100K .......... .......... .......... .......... .......... 67% 35.1M 13s
340150K .......... .......... .......... .......... .......... 67% 13.5M 13s
340200K .......... .......... .......... .......... .......... 67%  294M 13s
340250K .......... .......... .......... .......... .......... 67% 22.0M 13s
340300K .......... .......... .......... .......... .......... 67% 23.7M 13s
340350K .......... .......... .......... .......... .......... 67%  154M 13s
340400K .......... .......... .......... .......... .......... 67% 25.3M 13s
340450K .......... .......... .......... .......... .......... 67% 29.0M 13s
340500K .......... .......... .......... .......... .......... 67% 36.6M 13s
340550K .......... .......... .......... .......... .......... 67% 29.5M 13s
340600K .......... .......... .......... .......... .......... 67% 27.2M 13s
340650K .......... .......... .......... .......... .......... 67% 34.9M 13s
340700K .......... .......... .......... .......... .......... 67% 19.5M 13s
340750K .......... .......... .......... .......... .......... 67% 47.6M 13s
340800K .......... .......... .......... .......... .......... 67% 24.2M 13s
340850K .......... .......... .......... .......... .......... 67% 27.6M 13s
340900K .......... .......... .......... .......... .......... 67% 35.0M 13s
340950K .......... .......... .......... .......... .......... 67% 21.5M 13s
341000K .......... .......... .......... .......... .......... 67% 38.2M 13s
341050K .......... .......... .......... .......... .......... 67% 24.2M 13s
341100K .......... .......... .......... .......... .......... 67% 27.6M 13s
341150K .......... .......... .......... .......... .......... 67% 29.7M 13s
341200K .......... .......... .......... .......... .......... 67% 27.6M 13s
341250K .......... .......... .......... .......... .......... 67% 25.6M 13s
341300K .......... .......... .......... .......... .......... 67% 42.7M 13s
341350K .......... .......... .......... .......... .......... 67% 20.3M 13s
341400K .......... .......... .......... .......... .......... 67% 20.4M 13s
341450K .......... .......... .......... .......... .......... 67% 18.2M 13s
341500K .......... .......... .......... .......... .......... 67% 18.0M 13s
341550K .......... .......... .......... .......... .......... 67% 35.3M 13s
341600K .......... .......... .......... .......... .......... 67% 14.7M 13s
341650K .......... .......... .......... .......... .......... 67% 23.0M 13s
341700K .......... .......... .......... .......... .......... 67% 27.1M 13s
341750K .......... .......... .......... .......... .......... 67% 25.2M 13s
341800K .......... .......... .......... .......... .......... 67% 21.4M 13s
341850K .......... .......... .......... .......... .......... 67% 14.9M 13s
341900K .......... .......... .......... .......... .......... 67% 20.3M 13s
341950K .......... .......... .......... .......... .......... 67% 19.3M 13s
342000K .......... .......... .......... .......... .......... 67% 25.8M 13s
342050K .......... .......... .......... .......... .......... 67% 21.5M 13s
342100K .......... .......... .......... .......... .......... 67% 21.5M 13s
342150K .......... .......... .......... .......... .......... 67% 24.1M 13s
342200K .......... .......... .......... .......... .......... 67% 20.3M 13s
342250K .......... .......... .......... .......... .......... 67% 24.0M 13s
342300K .......... .......... .......... .......... .......... 67% 23.8M 13s
342350K .......... .......... .......... .......... .......... 67% 17.7M 13s
342400K .......... .......... .......... .......... .......... 67% 19.3M 13s
342450K .......... .......... .......... .......... .......... 68% 22.8M 13s
342500K .......... .......... .......... .......... .......... 68% 42.7M 13s
342550K .......... .......... .......... .......... .......... 68% 55.0M 13s
342600K .......... .......... .......... .......... .......... 68% 19.9M 13s
342650K .......... .......... .......... .......... .......... 68%  111M 13s
342700K .......... .......... .......... .......... .......... 68%  276M 13s
342750K .......... .......... .......... .......... .......... 68% 20.5M 13s
342800K .......... .......... .......... .......... .......... 68% 55.7M 13s
342850K .......... .......... .......... .......... .......... 68% 85.2M 13s
342900K .......... .......... .......... .......... .......... 68% 22.7M 13s
342950K .......... .......... .......... .......... .......... 68% 27.0M 13s
343000K .......... .......... .......... .......... .......... 68% 24.0M 13s
343050K .......... .......... .......... .......... .......... 68% 31.0M 13s
343100K .......... .......... .......... .......... .......... 68% 17.4M 13s
343150K .......... .......... .......... .......... .......... 68% 31.1M 13s
343200K .......... .......... .......... .......... .......... 68% 27.8M 13s
343250K .......... .......... .......... .......... .......... 68% 25.4M 13s
343300K .......... .......... .......... .......... .......... 68% 25.9M 13s
343350K .......... .......... .......... .......... .......... 68% 24.1M 13s
343400K .......... .......... .......... .......... .......... 68% 15.8M 13s
343450K .......... .......... .......... .......... .......... 68% 20.6M 13s
343500K .......... .......... .......... .......... .......... 68% 17.9M 13s
343550K .......... .......... .......... .......... .......... 68% 34.3M 13s
343600K .......... .......... .......... .......... .......... 68% 18.4M 13s
343650K .......... .......... .......... .......... .......... 68% 25.7M 13s
343700K .......... .......... .......... .......... .......... 68% 16.7M 13s
343750K .......... .......... .......... .......... .......... 68% 32.8M 13s
343800K .......... .......... .......... .......... .......... 68% 10.6M 13s
343850K .......... .......... .......... .......... .......... 68% 29.5M 13s
343900K .......... .......... .......... .......... .......... 68% 31.4M 13s
343950K .......... .......... .......... .......... .......... 68% 18.8M 13s
344000K .......... .......... .......... .......... .......... 68% 43.2M 13s
344050K .......... .......... .......... .......... .......... 68% 15.8M 13s
344100K .......... .......... .......... .......... .......... 68% 38.1M 13s
344150K .......... .......... .......... .......... .......... 68% 17.2M 13s
344200K .......... .......... .......... .......... .......... 68% 15.8M 13s
344250K .......... .......... .......... .......... .......... 68% 19.1M 13s
344300K .......... .......... .......... .......... .......... 68% 18.5M 13s
344350K .......... .......... .......... .......... .......... 68% 17.6M 13s
344400K .......... .......... .......... .......... .......... 68% 19.1M 13s
344450K .......... .......... .......... .......... .......... 68% 15.9M 13s
344500K .......... .......... .......... .......... .......... 68% 21.9M 13s
344550K .......... .......... .......... .......... .......... 68% 15.6M 13s
344600K .......... .......... .......... .......... .......... 68% 15.9M 13s
344650K .......... .......... .......... .......... .......... 68% 21.0M 13s
344700K .......... .......... .......... .......... .......... 68% 9.82M 13s
344750K .......... .......... .......... .......... .......... 68% 11.8M 13s
344800K .......... .......... .......... .......... .......... 68% 10.4M 13s
344850K .......... .......... .......... .......... .......... 68% 17.1M 13s
344900K .......... .......... .......... .......... .......... 68% 36.7M 13s
344950K .......... .......... .......... .......... .......... 68% 22.7M 13s
345000K .......... .......... .......... .......... .......... 68% 24.1M 13s
345050K .......... .......... .......... .......... .......... 68% 25.4M 13s
345100K .......... .......... .......... .......... .......... 68% 21.0M 13s
345150K .......... .......... .......... .......... .......... 68% 23.2M 13s
345200K .......... .......... .......... .......... .......... 68% 16.7M 13s
345250K .......... .......... .......... .......... .......... 68% 26.7M 13s
345300K .......... .......... .......... .......... .......... 68% 26.2M 13s
345350K .......... .......... .......... .......... .......... 68% 21.4M 13s
345400K .......... .......... .......... .......... .......... 68% 23.3M 13s
345450K .......... .......... .......... .......... .......... 68% 20.7M 13s
345500K .......... .......... .......... .......... .......... 68% 23.5M 13s
345550K .......... .......... .......... .......... .......... 68% 24.3M 13s
345600K .......... .......... .......... .......... .......... 68% 18.0M 13s
345650K .......... .......... .......... .......... .......... 68% 19.3M 13s
345700K .......... .......... .......... .......... .......... 68% 16.3M 13s
345750K .......... .......... .......... .......... .......... 68% 17.1M 13s
345800K .......... .......... .......... .......... .......... 68%  461M 13s
345850K .......... .......... .......... .......... .......... 68% 65.3M 13s
345900K .......... .......... .......... .......... .......... 68% 27.4M 13s
345950K .......... .......... .......... .......... .......... 68% 14.8M 13s
346000K .......... .......... .......... .......... .......... 68%  498M 13s
346050K .......... .......... .......... .......... .......... 68% 18.8M 13s
346100K .......... .......... .......... .......... .......... 68% 24.7M 13s
346150K .......... .......... .......... .......... .......... 68% 22.4M 13s
346200K .......... .......... .......... .......... .......... 68% 15.5M 13s
346250K .......... .......... .......... .......... .......... 68% 35.0M 13s
346300K .......... .......... .......... .......... .......... 68% 17.6M 13s
346350K .......... .......... .......... .......... .......... 68% 21.2M 13s
346400K .......... .......... .......... .......... .......... 68% 19.6M 13s
346450K .......... .......... .......... .......... .......... 68% 17.6M 13s
346500K .......... .......... .......... .......... .......... 68% 25.7M 13s
346550K .......... .......... .......... .......... .......... 68% 20.4M 13s
346600K .......... .......... .......... .......... .......... 68% 20.4M 13s
346650K .......... .......... .......... .......... .......... 68% 27.4M 13s
346700K .......... .......... .......... .......... .......... 68% 16.2M 13s
346750K .......... .......... .......... .......... .......... 68% 25.5M 13s
346800K .......... .......... .......... .......... .......... 68% 26.0M 13s
346850K .......... .......... .......... .......... .......... 68% 18.3M 13s
346900K .......... .......... .......... .......... .......... 68% 18.3M 13s
346950K .......... .......... .......... .......... .......... 68% 11.3M 13s
347000K .......... .......... .......... .......... .......... 68% 18.3M 13s
347050K .......... .......... .......... .......... .......... 68% 23.1M 13s
347100K .......... .......... .......... .......... .......... 68% 43.9M 13s
347150K .......... .......... .......... .......... .......... 68% 22.6M 13s
347200K .......... .......... .......... .......... .......... 68% 24.1M 13s
347250K .......... .......... .......... .......... .......... 68% 24.3M 13s
347300K .......... .......... .......... .......... .......... 68% 38.5M 13s
347350K .......... .......... .......... .......... .......... 68% 17.5M 13s
347400K .......... .......... .......... .......... .......... 68% 21.4M 13s
347450K .......... .......... .......... .......... .......... 69% 19.3M 13s
347500K .......... .......... .......... .......... .......... 69% 20.3M 13s
347550K .......... .......... .......... .......... .......... 69% 19.2M 13s
347600K .......... .......... .......... .......... .......... 69% 21.7M 12s
347650K .......... .......... .......... .......... .......... 69% 22.6M 12s
347700K .......... .......... .......... .......... .......... 69% 18.2M 12s
347750K .......... .......... .......... .......... .......... 69% 21.7M 12s
347800K .......... .......... .......... .......... .......... 69% 25.3M 12s
347850K .......... .......... .......... .......... .......... 69% 17.2M 12s
347900K .......... .......... .......... .......... .......... 69% 19.8M 12s
347950K .......... .......... .......... .......... .......... 69% 16.5M 12s
348000K .......... .......... .......... .......... .......... 69% 5.74M 12s
348050K .......... .......... .......... .......... .......... 69% 12.2M 12s
348100K .......... .......... .......... .......... .......... 69% 12.0M 12s
348150K .......... .......... .......... .......... .......... 69% 14.7M 12s
348200K .......... .......... .......... .......... .......... 69% 11.5M 12s
348250K .......... .......... .......... .......... .......... 69% 14.1M 12s
348300K .......... .......... .......... .......... .......... 69% 13.9M 12s
348350K .......... .......... .......... .......... .......... 69% 10.6M 12s
348400K .......... .......... .......... .......... .......... 69% 13.6M 12s
348450K .......... .......... .......... .......... .......... 69% 11.1M 12s
348500K .......... .......... .......... .......... .......... 69% 16.1M 12s
348550K .......... .......... .......... .......... .......... 69% 29.8M 12s
348600K .......... .......... .......... .......... .......... 69% 20.3M 12s
348650K .......... .......... .......... .......... .......... 69% 21.4M 12s
348700K .......... .......... .......... .......... .......... 69% 17.7M 12s
348750K .......... .......... .......... .......... .......... 69% 20.1M 12s
348800K .......... .......... .......... .......... .......... 69% 12.4M 12s
348850K .......... .......... .......... .......... .......... 69% 48.1M 12s
348900K .......... .......... .......... .......... .......... 69% 19.9M 12s
348950K .......... .......... .......... .......... .......... 69% 20.4M 12s
349000K .......... .......... .......... .......... .......... 69% 25.6M 12s
349050K .......... .......... .......... .......... .......... 69% 25.4M 12s
349100K .......... .......... .......... .......... .......... 69% 16.1M 12s
349150K .......... .......... .......... .......... .......... 69% 27.5M 12s
349200K .......... .......... .......... .......... .......... 69% 16.7M 12s
349250K .......... .......... .......... .......... .......... 69% 15.1M 12s
349300K .......... .......... .......... .......... .......... 69% 17.4M 12s
349350K .......... .......... .......... .......... .......... 69% 24.8M 12s
349400K .......... .......... .......... .......... .......... 69% 16.9M 12s
349450K .......... .......... .......... .......... .......... 69% 17.0M 12s
349500K .......... .......... .......... .......... .......... 69% 26.8M 12s
349550K .......... .......... .......... .......... .......... 69% 26.2M 12s
349600K .......... .......... .......... .......... .......... 69% 17.6M 12s
349650K .......... .......... .......... .......... .......... 69% 20.3M 12s
349700K .......... .......... .......... .......... .......... 69% 16.8M 12s
349750K .......... .......... .......... .......... .......... 69% 25.2M 12s
349800K .......... .......... .......... .......... .......... 69% 15.7M 12s
349850K .......... .......... .......... .......... .......... 69% 12.4M 12s
349900K .......... .......... .......... .......... .......... 69% 14.4M 12s
349950K .......... .......... .......... .......... .......... 69% 14.3M 12s
350000K .......... .......... .......... .......... .......... 69% 15.1M 12s
350050K .......... .......... .......... .......... .......... 69% 51.2M 12s
350100K .......... .......... .......... .......... .......... 69% 15.0M 12s
350150K .......... .......... .......... .......... .......... 69% 32.1M 12s
350200K .......... .......... .......... .......... .......... 69% 22.4M 12s
350250K .......... .......... .......... .......... .......... 69% 24.4M 12s
350300K .......... .......... .......... .......... .......... 69% 21.5M 12s
350350K .......... .......... .......... .......... .......... 69% 16.1M 12s
350400K .......... .......... .......... .......... .......... 69% 15.4M 12s
350450K .......... .......... .......... .......... .......... 69% 16.8M 12s
350500K .......... .......... .......... .......... .......... 69% 23.9M 12s
350550K .......... .......... .......... .......... .......... 69% 16.2M 12s
350600K .......... .......... .......... .......... .......... 69% 16.8M 12s
350650K .......... .......... .......... .......... .......... 69% 16.2M 12s
350700K .......... .......... .......... .......... .......... 69% 18.4M 12s
350750K .......... .......... .......... .......... .......... 69% 24.2M 12s
350800K .......... .......... .......... .......... .......... 69% 16.8M 12s
350850K .......... .......... .......... .......... .......... 69% 16.2M 12s
350900K .......... .......... .......... .......... .......... 69% 20.3M 12s
350950K .......... .......... .......... .......... .......... 69% 14.9M 12s
351000K .......... .......... .......... .......... .......... 69% 24.0M 12s
351050K .......... .......... .......... .......... .......... 69% 25.8M 12s
351100K .......... .......... .......... .......... .......... 69% 22.2M 12s
351150K .......... .......... .......... .......... .......... 69% 6.85M 12s
351200K .......... .......... .......... .......... .......... 69%  313M 12s
351250K .......... .......... .......... .......... .......... 69%  356M 12s
351300K .......... .......... .......... .......... .......... 69% 27.4M 12s
351350K .......... .......... .......... .......... .......... 69% 22.8M 12s
351400K .......... .......... .......... .......... .......... 69% 19.3M 12s
351450K .......... .......... .......... .......... .......... 69% 38.7M 12s
351500K .......... .......... .......... .......... .......... 69% 25.8M 12s
351550K .......... .......... .......... .......... .......... 69% 35.0M 12s
351600K .......... .......... .......... .......... .......... 69% 25.8M 12s
351650K .......... .......... .......... .......... .......... 69% 19.1M 12s
351700K .......... .......... .......... .......... .......... 69% 43.3M 12s
351750K .......... .......... .......... .......... .......... 69% 27.5M 12s
351800K .......... .......... .......... .......... .......... 69% 32.1M 12s
351850K .......... .......... .......... .......... .......... 69% 27.5M 12s
351900K .......... .......... .......... .......... .......... 69% 25.8M 12s
351950K .......... .......... .......... .......... .......... 69% 23.8M 12s
352000K .......... .......... .......... .......... .......... 69% 27.9M 12s
352050K .......... .......... .......... .......... .......... 69% 32.2M 12s
352100K .......... .......... .......... .......... .......... 69% 24.1M 12s
352150K .......... .......... .......... .......... .......... 69% 34.9M 12s
352200K .......... .......... .......... .......... .......... 69% 27.4M 12s
352250K .......... .......... .......... .......... .......... 69% 29.9M 12s
352300K .......... .......... .......... .......... .......... 69% 27.9M 12s
352350K .......... .......... .......... .......... .......... 69% 31.7M 12s
352400K .......... .......... .......... .......... .......... 69% 24.3M 12s
352450K .......... .......... .......... .......... .......... 69% 17.5M 12s
352500K .......... .......... .......... .......... .......... 70% 55.7M 12s
352550K .......... .......... .......... .......... .......... 70% 29.3M 12s
352600K .......... .......... .......... .......... .......... 70% 16.2M 12s
352650K .......... .......... .......... .......... .......... 70% 21.5M 12s
352700K .......... .......... .......... .......... .......... 70% 13.8M 12s
352750K .......... .......... .......... .......... .......... 70% 8.23M 12s
352800K .......... .......... .......... .......... .......... 70% 13.4M 12s
352850K .......... .......... .......... .......... .......... 70% 11.0M 12s
352900K .......... .......... .......... .......... .......... 70% 12.1M 12s
352950K .......... .......... .......... .......... .......... 70% 11.1M 12s
353000K .......... .......... .......... .......... .......... 70% 16.1M 12s
353050K .......... .......... .......... .......... .......... 70% 12.1M 12s
353100K .......... .......... .......... .......... .......... 70% 12.5M 12s
353150K .......... .......... .......... .......... .......... 70% 13.7M 12s
353200K .......... .......... .......... .......... .......... 70% 9.48M 12s
353250K .......... .......... .......... .......... .......... 70% 14.3M 12s
353300K .......... .......... .......... .......... .......... 70% 14.4M 12s
353350K .......... .......... .......... .......... .......... 70% 8.19M 12s
353400K .......... .......... .......... .......... .......... 70% 32.7M 12s
353450K .......... .......... .......... .......... .......... 70% 12.1M 12s
353500K .......... .......... .......... .......... .......... 70% 17.2M 12s
353550K .......... .......... .......... .......... .......... 70% 14.6M 12s
353600K .......... .......... .......... .......... .......... 70% 16.0M 12s
353650K .......... .......... .......... .......... .......... 70% 14.3M 12s
353700K .......... .......... .......... .......... .......... 70% 14.3M 12s
353750K .......... .......... .......... .......... .......... 70% 17.6M 12s
353800K .......... .......... .......... .......... .......... 70% 13.3M 12s
353850K .......... .......... .......... .......... .......... 70% 14.3M 12s
353900K .......... .......... .......... .......... .......... 70% 16.1M 12s
353950K .......... .......... .......... .......... .......... 70% 15.5M 12s
354000K .......... .......... .......... .......... .......... 70% 17.5M 12s
354050K .......... .......... .......... .......... .......... 70% 15.6M 12s
354100K .......... .......... .......... .......... .......... 70% 32.2M 12s
354150K .......... .......... .......... .......... .......... 70% 21.1M 12s
354200K .......... .......... .......... .......... .......... 70% 38.4M 12s
354250K .......... .......... .......... .......... .......... 70% 24.2M 12s
354300K .......... .......... .......... .......... .......... 70%  131M 12s
354350K .......... .......... .......... .......... .......... 70% 20.3M 12s
354400K .......... .......... .......... .......... .......... 70% 34.9M 12s
354450K .......... .......... .......... .......... .......... 70% 25.4M 12s
354500K .......... .......... .......... .......... .......... 70% 21.7M 12s
354550K .......... .......... .......... .......... .......... 70% 34.8M 12s
354600K .......... .......... .......... .......... .......... 70% 22.7M 12s
354650K .......... .......... .......... .......... .......... 70% 24.2M 12s
354700K .......... .......... .......... .......... .......... 70% 24.0M 12s
354750K .......... .......... .......... .......... .......... 70% 32.0M 12s
354800K .......... .......... .......... .......... .......... 70% 31.9M 12s
354850K .......... .......... .......... .......... .......... 70% 19.7M 12s
354900K .......... .......... .......... .......... .......... 70% 36.4M 12s
354950K .......... .......... .......... .......... .......... 70% 20.2M 12s
355000K .......... .......... .......... .......... .......... 70% 25.5M 12s
355050K .......... .......... .......... .......... .......... 70% 21.4M 12s
355100K .......... .......... .......... .......... .......... 70% 22.7M 12s
355150K .......... .......... .......... .......... .......... 70% 27.5M 12s
355200K .......... .......... .......... .......... .......... 70% 21.3M 12s
355250K .......... .......... .......... .......... .......... 70% 22.9M 12s
355300K .......... .......... .......... .......... .......... 70% 27.2M 12s
355350K .......... .......... .......... .......... .......... 70% 16.2M 12s
355400K .......... .......... .......... .......... .......... 70% 26.8M 12s
355450K .......... .......... .......... .......... .......... 70% 17.3M 12s
355500K .......... .......... .......... .......... .......... 70% 24.1M 12s
355550K .......... .......... .......... .......... .......... 70% 17.7M 12s
355600K .......... .......... .......... .......... .......... 70% 7.59M 12s
355650K .......... .......... .......... .......... .......... 70% 19.2M 12s
355700K .......... .......... .......... .......... .......... 70% 12.5M 12s
355750K .......... .......... .......... .......... .......... 70% 19.3M 12s
355800K .......... .......... .......... .......... .......... 70% 16.7M 12s
355850K .......... .......... .......... .......... .......... 70% 14.5M 12s
355900K .......... .......... .......... .......... .......... 70% 18.2M 12s
355950K .......... .......... .......... .......... .......... 70% 14.3M 12s
356000K .......... .......... .......... .......... .......... 70% 14.9M 12s
356050K .......... .......... .......... .......... .......... 70% 21.5M 12s
356100K .......... .......... .......... .......... .......... 70% 11.7M 12s
356150K .......... .......... .......... .......... .......... 70% 21.3M 12s
356200K .......... .......... .......... .......... .......... 70% 11.1M 12s
356250K .......... .......... .......... .......... .......... 70% 8.19M 12s
356300K .......... .......... .......... .......... .......... 70%  425M 12s
356350K .......... .......... .......... .......... .......... 70% 98.4M 12s
356400K .......... .......... .......... .......... .......... 70% 12.0M 12s
356450K .......... .......... .......... .......... .......... 70% 19.4M 12s
356500K .......... .......... .......... .......... .......... 70% 48.2M 12s
356550K .......... .......... .......... .......... .......... 70% 20.3M 12s
356600K .......... .......... .......... .......... .......... 70% 19.3M 12s
356650K .......... .......... .......... .......... .......... 70% 16.8M 12s
356700K .......... .......... .......... .......... .......... 70% 20.2M 12s
356750K .......... .......... .......... .......... .......... 70% 20.3M 12s
356800K .......... .......... .......... .......... .......... 70% 16.9M 12s
356850K .......... .......... .......... .......... .......... 70% 20.3M 12s
356900K .......... .......... .......... .......... .......... 70% 22.7M 12s
356950K .......... .......... .......... .......... .......... 70% 18.3M 12s
357000K .......... .......... .......... .......... .......... 70% 21.6M 12s
357050K .......... .......... .......... .......... .......... 70% 22.5M 12s
357100K .......... .......... .......... .......... .......... 70% 17.6M 12s
357150K .......... .......... .......... .......... .......... 70% 14.4M 12s
357200K .......... .......... .......... .......... .......... 70% 32.2M 12s
357250K .......... .......... .......... .......... .......... 70% 22.8M 12s
357300K .......... .......... .......... .......... .......... 70% 12.0M 12s
357350K .......... .......... .......... .......... .......... 70% 29.3M 12s
357400K .......... .......... .......... .......... .......... 70% 27.8M 12s
357450K .......... .......... .......... .......... .......... 70% 48.2M 12s
357500K .......... .......... .......... .......... .......... 70% 22.9M 12s
357550K .......... .......... .......... .......... .......... 71% 27.5M 12s
357600K .......... .......... .......... .......... .......... 71% 21.4M 12s
357650K .......... .......... .......... .......... .......... 71% 19.2M 12s
357700K .......... .......... .......... .......... .......... 71% 25.6M 12s
357750K .......... .......... .......... .......... .......... 71% 29.1M 12s
357800K .......... .......... .......... .......... .......... 71% 18.6M 12s
357850K .......... .......... .......... .......... .......... 71% 22.7M 12s
357900K .......... .......... .......... .......... .......... 71% 22.8M 12s
357950K .......... .......... .......... .......... .......... 71% 18.4M 12s
358000K .......... .......... .......... .......... .......... 71% 20.3M 12s
358050K .......... .......... .......... .......... .......... 71% 24.2M 12s
358100K .......... .......... .......... .......... .......... 71% 17.5M 12s
358150K .......... .......... .......... .......... .......... 71% 24.0M 12s
358200K .......... .......... .......... .......... .......... 71% 16.9M 12s
358250K .......... .......... .......... .......... .......... 71% 24.1M 12s
358300K .......... .......... .......... .......... .......... 71% 13.7M 12s
358350K .......... .......... .......... .......... .......... 71% 32.1M 12s
358400K .......... .......... .......... .......... .......... 71%  397M 12s
358450K .......... .......... .......... .......... .......... 71%  215M 12s
358500K .......... .......... .......... .......... .......... 71% 9.86M 12s
358550K .......... .......... .......... .......... .......... 71%  470M 11s
358600K .......... .......... .......... .......... .......... 71% 87.3M 11s
358650K .......... .......... .......... .......... .......... 71% 30.3M 11s
358700K .......... .......... .......... .......... .......... 71% 27.5M 11s
358750K .......... .......... .......... .......... .......... 71% 38.6M 11s
358800K .......... .......... .......... .......... .......... 71% 38.4M 11s
358850K .......... .......... .......... .......... .......... 71% 24.1M 11s
358900K .......... .......... .......... .......... .......... 71% 29.8M 11s
358950K .......... .......... .......... .......... .......... 71% 27.6M 11s
359000K .......... .......... .......... .......... .......... 71% 34.7M 11s
359050K .......... .......... .......... .......... .......... 71% 27.2M 11s
359100K .......... .......... .......... .......... .......... 71% 24.3M 11s
359150K .......... .......... .......... .......... .......... 71% 42.7M 11s
359200K .......... .......... .......... .......... .......... 71% 24.1M 11s
359250K .......... .......... .......... .......... .......... 71% 25.6M 11s
359300K .......... .......... .......... .......... .......... 71% 38.4M 11s
359350K .......... .......... .......... .......... .......... 71% 25.8M 11s
359400K .......... .......... .......... .......... .......... 71% 27.7M 11s
359450K .......... .......... .......... .......... .......... 71% 27.5M 11s
359500K .......... .......... .......... .......... .......... 71% 42.9M 11s
359550K .......... .......... .......... .......... .......... 71% 34.6M 11s
359600K .......... .......... .......... .......... .......... 71% 26.0M 11s
359650K .......... .......... .......... .......... .......... 71% 29.7M 11s
359700K .......... .......... .......... .......... .......... 71% 25.4M 11s
359750K .......... .......... .......... .......... .......... 71% 35.6M 11s
359800K .......... .......... .......... .......... .......... 71% 11.2M 11s
359850K .......... .......... .......... .......... .......... 71% 24.5M 11s
359900K .......... .......... .......... .......... .......... 71% 62.9M 11s
359950K .......... .......... .......... .......... .......... 71% 51.1M 11s
360000K .......... .......... .......... .......... .......... 71% 23.4M 11s
360050K .......... .......... .......... .......... .......... 71% 23.5M 11s
360100K .......... .......... .......... .......... .......... 71% 51.8M 11s
360150K .......... .......... .......... .......... .......... 71% 25.5M 11s
360200K .......... .......... .......... .......... .......... 71% 26.0M 11s
360250K .......... .......... .......... .......... .......... 71% 25.5M 11s
360300K .......... .......... .......... .......... .......... 71% 19.5M 11s
360350K .......... .......... .......... .......... .......... 71% 21.5M 11s
360400K .......... .......... .......... .......... .......... 71% 24.0M 11s
360450K .......... .......... .......... .......... .......... 71% 21.5M 11s
360500K .......... .......... .......... .......... .......... 71% 24.1M 11s
360550K .......... .......... .......... .......... .......... 71% 21.5M 11s
360600K .......... .......... .......... .......... .......... 71% 19.3M 11s
360650K .......... .......... .......... .......... .......... 71% 21.4M 11s
360700K .......... .......... .......... .......... .......... 71% 25.6M 11s
360750K .......... .......... .......... .......... .......... 71% 19.3M 11s
360800K .......... .......... .......... .......... .......... 71% 24.2M 11s
360850K .......... .......... .......... .......... .......... 71% 22.7M 11s
360900K .......... .......... .......... .......... .......... 71% 21.4M 11s
360950K .......... .......... .......... .......... .......... 71% 25.7M 11s
361000K .......... .......... .......... .......... .......... 71% 27.8M 11s
361050K .......... .......... .......... .......... .......... 71% 31.9M 11s
361100K .......... .......... .......... .......... .......... 71% 14.9M 11s
361150K .......... .......... .......... .......... .......... 71%  149M 11s
361200K .......... .......... .......... .......... .......... 71% 27.9M 11s
361250K .......... .......... .......... .......... .......... 71% 83.2M 11s
361300K .......... .......... .......... .......... .......... 71% 29.5M 11s
361350K .......... .......... .......... .......... .......... 71% 24.1M 11s
361400K .......... .......... .......... .......... .......... 71% 21.5M 11s
361450K .......... .......... .......... .......... .......... 71% 25.7M 11s
361500K .......... .......... .......... .......... .......... 71% 19.3M 11s
361550K .......... .......... .......... .......... .......... 71% 27.5M 11s
361600K .......... .......... .......... .......... .......... 71% 25.7M 11s
361650K .......... .......... .......... .......... .......... 71% 24.2M 11s
361700K .......... .......... .......... .......... .......... 71% 24.1M 11s
361750K .......... .......... .......... .......... .......... 71% 29.3M 11s
361800K .......... .......... .......... .......... .......... 71% 27.8M 11s
361850K .......... .......... .......... .......... .......... 71% 22.6M 11s
361900K .......... .......... .......... .......... .......... 71% 22.5M 11s
361950K .......... .......... .......... .......... .......... 71% 25.0M 11s
362000K .......... .......... .......... .......... .......... 71% 23.8M 11s
362050K .......... .......... .......... .......... .......... 71% 23.8M 11s
362100K .......... .......... .......... .......... .......... 71% 27.5M 11s
362150K .......... .......... .......... .......... .......... 71% 22.7M 11s
362200K .......... .......... .......... .......... .......... 71% 27.5M 11s
362250K .......... .......... .......... .......... .......... 71% 10.9M 11s
362300K .......... .......... .......... .......... .......... 71% 27.9M 11s
362350K .......... .......... .......... .......... .......... 71%  444M 11s
362400K .......... .......... .......... .......... .......... 71%  103M 11s
362450K .......... .......... .......... .......... .......... 71% 27.3M 11s
362500K .......... .......... .......... .......... .......... 71% 30.0M 11s
362550K .......... .......... .......... .......... .......... 72% 34.6M 11s
362600K .......... .......... .......... .......... .......... 72% 20.4M 11s
362650K .......... .......... .......... .......... .......... 72% 42.0M 11s
362700K .......... .......... .......... .......... .......... 72% 35.5M 11s
362750K .......... .......... .......... .......... .......... 72% 38.1M 11s
362800K .......... .......... .......... .......... .......... 72% 24.3M 11s
362850K .......... .......... .......... .......... .......... 72% 27.3M 11s
362900K .......... .......... .......... .......... .......... 72% 22.8M 11s
362950K .......... .......... .......... .......... .......... 72% 27.4M 11s
363000K .......... .......... .......... .......... .......... 72% 38.5M 11s
363050K .......... .......... .......... .......... .......... 72% 23.8M 11s
363100K .......... .......... .......... .......... .......... 72% 22.9M 11s
363150K .......... .......... .......... .......... .......... 72% 32.5M 11s
363200K .......... .......... .......... .......... .......... 72% 27.6M 11s
363250K .......... .......... .......... .......... .......... 72% 29.2M 11s
363300K .......... .......... .......... .......... .......... 72% 23.0M 11s
363350K .......... .......... .......... .......... .......... 72% 27.4M 11s
363400K .......... .......... .......... .......... .......... 72% 31.5M 11s
363450K .......... .......... .......... .......... .......... 72% 24.2M 11s
363500K .......... .......... .......... .......... .......... 72% 28.0M 11s
363550K .......... .......... .......... .......... .......... 72% 37.9M 11s
363600K .......... .......... .......... .......... .......... 72% 19.4M 11s
363650K .......... .......... .......... .......... .......... 72% 42.1M 11s
363700K .......... .......... .......... .......... .......... 72% 25.5M 11s
363750K .......... .......... .......... .......... .......... 72% 48.8M 11s
363800K .......... .......... .......... .......... .......... 72% 10.5M 11s
363850K .......... .......... .......... .......... .......... 72%  376M 11s
363900K .......... .......... .......... .......... .......... 72%  128M 11s
363950K .......... .......... .......... .......... .......... 72% 25.4M 11s
364000K .......... .......... .......... .......... .......... 72% 16.5M 11s
364050K .......... .......... .......... .......... .......... 72% 51.6M 11s
364100K .......... .......... .......... .......... .......... 72% 38.4M 11s
364150K .......... .......... .......... .......... .......... 72% 92.1M 11s
364200K .......... .......... .......... .......... .......... 72% 32.6M 11s
364250K .......... .......... .......... .......... .......... 72% 32.1M 11s
364300K .......... .......... .......... .......... .......... 72% 34.8M 11s
364350K .......... .......... .......... .......... .......... 72% 29.6M 11s
364400K .......... .......... .......... .......... .......... 72% 25.6M 11s
364450K .......... .......... .......... .......... .......... 72% 38.4M 11s
364500K .......... .......... .......... .......... .......... 72% 27.4M 11s
364550K .......... .......... .......... .......... .......... 72% 38.2M 11s
364600K .......... .......... .......... .......... .......... 72% 29.0M 11s
364650K .......... .......... .......... .......... .......... 72% 32.8M 11s
364700K .......... .......... .......... .......... .......... 72% 24.1M 11s
364750K .......... .......... .......... .......... .......... 72% 31.1M 11s
364800K .......... .......... .......... .......... .......... 72% 28.5M 11s
364850K .......... .......... .......... .......... .......... 72% 24.8M 11s
364900K .......... .......... .......... .......... .......... 72% 29.7M 11s
364950K .......... .......... .......... .......... .......... 72% 38.0M 11s
365000K .......... .......... .......... .......... .......... 72% 24.3M 11s
365050K .......... .......... .......... .......... .......... 72% 31.2M 11s
365100K .......... .......... .......... .......... .......... 72% 32.4M 11s
365150K .......... .......... .......... .......... .......... 72% 24.3M 11s
365200K .......... .......... .......... .......... .......... 72% 15.6M 11s
365250K .......... .......... .......... .......... .......... 72% 29.8M 11s
365300K .......... .......... .......... .......... .......... 72% 17.5M 11s
365350K .......... .......... .......... .......... .......... 72%  349M 11s
365400K .......... .......... .......... .......... .......... 72%  125M 11s
365450K .......... .......... .......... .......... .......... 72% 21.2M 11s
365500K .......... .......... .......... .......... .......... 72%  102M 11s
365550K .......... .......... .......... .......... .......... 72% 35.7M 11s
365600K .......... .......... .......... .......... .......... 72% 37.6M 11s
365650K .......... .......... .......... .......... .......... 72% 42.9M 11s
365700K .......... .......... .......... .......... .......... 72% 27.3M 11s
365750K .......... .......... .......... .......... .......... 72% 29.8M 11s
365800K .......... .......... .......... .......... .......... 72% 29.6M 11s
365850K .......... .......... .......... .......... .......... 72% 32.0M 11s
365900K .......... .......... .......... .......... .......... 72% 38.6M 11s
365950K .......... .......... .......... .......... .......... 72% 27.5M 11s
366000K .......... .......... .......... .......... .......... 72% 35.0M 11s
366050K .......... .......... .......... .......... .......... 72% 35.1M 11s
366100K .......... .......... .......... .......... .......... 72% 25.7M 11s
366150K .......... .......... .......... .......... .......... 72% 42.5M 11s
366200K .......... .......... .......... .......... .......... 72% 29.6M 11s
366250K .......... .......... .......... .......... .......... 72% 29.7M 11s
366300K .......... .......... .......... .......... .......... 72% 48.0M 11s
366350K .......... .......... .......... .......... .......... 72% 27.3M 11s
366400K .......... .......... .......... .......... .......... 72% 43.2M 11s
366450K .......... .......... .......... .......... .......... 72% 23.4M 11s
366500K .......... .......... .......... .......... .......... 72% 47.6M 11s
366550K .......... .......... .......... .......... .......... 72% 32.7M 11s
366600K .......... .......... .......... .......... .......... 72% 22.1M 11s
366650K .......... .......... .......... .......... .......... 72% 26.7M 11s
366700K .......... .......... .......... .......... .......... 72% 19.8M 11s
366750K .......... .......... .......... .......... .......... 72% 12.8M 11s
366800K .......... .......... .......... .......... .......... 72%  373M 11s
366850K .......... .......... .......... .......... .......... 72% 32.8M 11s
366900K .......... .......... .......... .......... .......... 72% 20.8M 11s
366950K .......... .......... .......... .......... .......... 72% 24.9M 11s
367000K .......... .......... .......... .......... .......... 72% 64.5M 11s
367050K .......... .......... .......... .......... .......... 72% 29.6M 11s
367100K .......... .......... .......... .......... .......... 72% 26.1M 11s
367150K .......... .......... .......... .......... .......... 72% 28.1M 11s
367200K .......... .......... .......... .......... .......... 72% 29.3M 11s
367250K .......... .......... .......... .......... .......... 72% 31.0M 11s
367300K .......... .......... .......... .......... .......... 72% 30.8M 11s
367350K .......... .......... .......... .......... .......... 72% 22.5M 11s
367400K .......... .......... .......... .......... .......... 72% 25.8M 11s
367450K .......... .......... .......... .......... .......... 72% 42.1M 11s
367500K .......... .......... .......... .......... .......... 72% 23.0M 11s
367550K .......... .......... .......... .......... .......... 72% 42.4M 11s
367600K .......... .......... .......... .......... .......... 73% 27.5M 11s
367650K .......... .......... .......... .......... .......... 73% 27.5M 11s
367700K .......... .......... .......... .......... .......... 73% 28.9M 11s
367750K .......... .......... .......... .......... .......... 73% 26.2M 11s
367800K .......... .......... .......... .......... .......... 73% 38.3M 11s
367850K .......... .......... .......... .......... .......... 73% 27.4M 11s
367900K .......... .......... .......... .......... .......... 73% 25.2M 11s
367950K .......... .......... .......... .......... .......... 73% 22.4M 11s
368000K .......... .......... .......... .......... .......... 73% 38.5M 11s
368050K .......... .......... .......... .......... .......... 73% 29.5M 11s
368100K .......... .......... .......... .......... .......... 73% 32.5M 11s
368150K .......... .......... .......... .......... .......... 73% 27.5M 11s
368200K .......... .......... .......... .......... .......... 73% 24.1M 11s
368250K .......... .......... .......... .......... .......... 73% 43.1M 11s
368300K .......... .......... .......... .......... .......... 73% 13.7M 11s
368350K .......... .......... .......... .......... .......... 73%  349M 11s
368400K .......... .......... .......... .......... .......... 73% 50.9M 11s
368450K .......... .......... .......... .......... .......... 73% 38.4M 11s
368500K .......... .......... .......... .......... .......... 73% 59.7M 11s
368550K .......... .......... .......... .......... .......... 73% 19.7M 11s
368600K .......... .......... .......... .......... .......... 73%  136M 11s
368650K .......... .......... .......... .......... .......... 73% 28.8M 11s
368700K .......... .......... .......... .......... .......... 73% 28.4M 11s
368750K .......... .......... .......... .......... .......... 73% 46.1M 11s
368800K .......... .......... .......... .......... .......... 73% 32.2M 11s
368850K .......... .......... .......... .......... .......... 73% 34.7M 11s
368900K .......... .......... .......... .......... .......... 73% 34.6M 11s
368950K .......... .......... .......... .......... .......... 73% 26.9M 11s
369000K .......... .......... .......... .......... .......... 73% 35.9M 10s
369050K .......... .......... .......... .......... .......... 73% 38.4M 10s
369100K .......... .......... .......... .......... .......... 73% 16.6M 10s
369150K .......... .......... .......... .......... .......... 73% 75.5M 10s
369200K .......... .......... .......... .......... .......... 73% 25.9M 10s
369250K .......... .......... .......... .......... .......... 73% 24.2M 10s
369300K .......... .......... .......... .......... .......... 73% 36.5M 10s
369350K .......... .......... .......... .......... .......... 73% 21.4M 10s
369400K .......... .......... .......... .......... .......... 73% 34.1M 10s
369450K .......... .......... .......... .......... .......... 73% 31.5M 10s
369500K .......... .......... .......... .......... .......... 73% 27.1M 10s
369550K .......... .......... .......... .......... .......... 73% 33.0M 10s
369600K .......... .......... .......... .......... .......... 73% 20.4M 10s
369650K .......... .......... .......... .......... .......... 73% 21.1M 10s
369700K .......... .......... .......... .......... .......... 73% 12.5M 10s
369750K .......... .......... .......... .......... .......... 73% 19.8M 10s
369800K .......... .......... .......... .......... .......... 73% 11.9M 10s
369850K .......... .......... .......... .......... .......... 73% 28.2M 10s
369900K .......... .......... .......... .......... .......... 73% 27.3M 10s
369950K .......... .......... .......... .......... .......... 73% 15.4M 10s
370000K .......... .......... .......... .......... .......... 73% 23.3M 10s
370050K .......... .......... .......... .......... .......... 73% 22.4M 10s
370100K .......... .......... .......... .......... .......... 73% 18.0M 10s
370150K .......... .......... .......... .......... .......... 73% 17.5M 10s
370200K .......... .......... .......... .......... .......... 73% 22.6M 10s
370250K .......... .......... .......... .......... .......... 73% 18.0M 10s
370300K .......... .......... .......... .......... .......... 73% 22.1M 10s
370350K .......... .......... .......... .......... .......... 73% 17.8M 10s
370400K .......... .......... .......... .......... .......... 73% 18.2M 10s
370450K .......... .......... .......... .......... .......... 73% 16.8M 10s
370500K .......... .......... .......... .......... .......... 73% 12.3M 10s
370550K .......... .......... .......... .......... .......... 73% 12.7M 10s
370600K .......... .......... .......... .......... .......... 73% 28.7M 10s
370650K .......... .......... .......... .......... .......... 73% 34.2M 10s
370700K .......... .......... .......... .......... .......... 73% 20.7M 10s
370750K .......... .......... .......... .......... .......... 73% 20.3M 10s
370800K .......... .......... .......... .......... .......... 73% 17.8M 10s
370850K .......... .......... .......... .......... .......... 73% 16.5M 10s
370900K .......... .......... .......... .......... .......... 73% 17.1M 10s
370950K .......... .......... .......... .......... .......... 73% 19.1M 10s
371000K .......... .......... .......... .......... .......... 73% 15.8M 10s
371050K .......... .......... .......... .......... .......... 73% 24.1M 10s
371100K .......... .......... .......... .......... .......... 73% 14.2M 10s
371150K .......... .......... .......... .......... .......... 73% 22.8M 10s
371200K .......... .......... .......... .......... .......... 73% 14.1M 10s
371250K .......... .......... .......... .......... .......... 73% 18.1M 10s
371300K .......... .......... .......... .......... .......... 73% 18.8M 10s
371350K .......... .......... .......... .......... .......... 73% 24.0M 10s
371400K .......... .......... .......... .......... .......... 73% 48.3M 10s
371450K .......... .......... .......... .......... .......... 73% 29.9M 10s
371500K .......... .......... .......... .......... .......... 73% 10.5M 10s
371550K .......... .......... .......... .......... .......... 73% 34.2M 10s
371600K .......... .......... .......... .......... .......... 73%  106M 10s
371650K .......... .......... .......... .......... .......... 73% 10.8M 10s
371700K .......... .......... .......... .......... .......... 73% 36.6M 10s
371750K .......... .......... .......... .......... .......... 73% 21.6M 10s
371800K .......... .......... .......... .......... .......... 73% 22.2M 10s
371850K .......... .......... .......... .......... .......... 73% 22.0M 10s
371900K .......... .......... .......... .......... .......... 73% 18.9M 10s
371950K .......... .......... .......... .......... .......... 73% 19.6M 10s
372000K .......... .......... .......... .......... .......... 73% 20.0M 10s
372050K .......... .......... .......... .......... .......... 73% 19.0M 10s
372100K .......... .......... .......... .......... .......... 73% 22.0M 10s
372150K .......... .......... .......... .......... .......... 73% 23.2M 10s
372200K .......... .......... .......... .......... .......... 73% 16.5M 10s
372250K .......... .......... .......... .......... .......... 73% 22.3M 10s
372300K .......... .......... .......... .......... .......... 73% 26.4M 10s
372350K .......... .......... .......... .......... .......... 73% 17.9M 10s
372400K .......... .......... .......... .......... .......... 73% 31.6M 10s
372450K .......... .......... .......... .......... .......... 73% 19.3M 10s
372500K .......... .......... .......... .......... .......... 73% 26.7M 10s
372550K .......... .......... .......... .......... .......... 73% 27.0M 10s
372600K .......... .......... .......... .......... .......... 73% 88.5M 10s
372650K .......... .......... .......... .......... .......... 74% 29.3M 10s
372700K .......... .......... .......... .......... .......... 74% 11.7M 10s
372750K .......... .......... .......... .......... .......... 74%  428M 10s
372800K .......... .......... .......... .......... .......... 74%  123M 10s
372850K .......... .......... .......... .......... .......... 74% 15.1M 10s
372900K .......... .......... .......... .......... .......... 74% 96.5M 10s
372950K .......... .......... .......... .......... .......... 74% 29.2M 10s
373000K .......... .......... .......... .......... .......... 74% 27.5M 10s
373050K .......... .......... .......... .......... .......... 74% 24.0M 10s
373100K .......... .......... .......... .......... .......... 74% 22.0M 10s
373150K .......... .......... .......... .......... .......... 74% 23.0M 10s
373200K .......... .......... .......... .......... .......... 74% 25.4M 10s
373250K .......... .......... .......... .......... .......... 74% 20.3M 10s
373300K .......... .......... .......... .......... .......... 74% 27.6M 10s
373350K .......... .......... .......... .......... .......... 74% 21.6M 10s
373400K .......... .......... .......... .......... .......... 74% 23.9M 10s
373450K .......... .......... .......... .......... .......... 74% 24.1M 10s
373500K .......... .......... .......... .......... .......... 74% 39.2M 10s
373550K .......... .......... .......... .......... .......... 74% 27.4M 10s
373600K .......... .......... .......... .......... .......... 74% 18.4M 10s
373650K .......... .......... .......... .......... .......... 74% 31.9M 10s
373700K .......... .......... .......... .......... .......... 74% 26.0M 10s
373750K .......... .......... .......... .......... .......... 74% 22.6M 10s
373800K .......... .......... .......... .......... .......... 74% 25.9M 10s
373850K .......... .......... .......... .......... .......... 74% 25.8M 10s
373900K .......... .......... .......... .......... .......... 74% 25.7M 10s
373950K .......... .......... .......... .......... .......... 74% 35.1M 10s
374000K .......... .......... .......... .......... .......... 74% 38.5M 10s
374050K .......... .......... .......... .......... .......... 74% 18.2M 10s
374100K .......... .......... .......... .......... .......... 74%  282M 10s
374150K .......... .......... .......... .......... .......... 74% 24.3M 10s
374200K .......... .......... .......... .......... .......... 74%  359M 10s
374250K .......... .......... .......... .......... .......... 74% 25.2M 10s
374300K .......... .......... .......... .......... .......... 74% 40.1M 10s
374350K .......... .......... .......... .......... .......... 74% 32.3M 10s
374400K .......... .......... .......... .......... .......... 74% 24.1M 10s
374450K .......... .......... .......... .......... .......... 74% 47.3M 10s
374500K .......... .......... .......... .......... .......... 74% 30.0M 10s
374550K .......... .......... .......... .......... .......... 74% 34.5M 10s
374600K .......... .......... .......... .......... .......... 74% 27.9M 10s
374650K .......... .......... .......... .......... .......... 74% 27.7M 10s
374700K .......... .......... .......... .......... .......... 74% 37.9M 10s
374750K .......... .......... .......... .......... .......... 74% 24.4M 10s
374800K .......... .......... .......... .......... .......... 74% 52.4M 10s
374850K .......... .......... .......... .......... .......... 74% 25.9M 10s
374900K .......... .......... .......... .......... .......... 74% 35.7M 10s
374950K .......... .......... .......... .......... .......... 74% 29.7M 10s
375000K .......... .......... .......... .......... .......... 74% 29.8M 10s
375050K .......... .......... .......... .......... .......... 74% 27.8M 10s
375100K .......... .......... .......... .......... .......... 74% 37.5M 10s
375150K .......... .......... .......... .......... .......... 74% 23.0M 10s
375200K .......... .......... .......... .......... .......... 74% 31.7M 10s
375250K .......... .......... .......... .......... .......... 74% 33.6M 10s
375300K .......... .......... .......... .......... .......... 74% 33.8M 10s
375350K .......... .......... .......... .......... .......... 74% 34.5M 10s
375400K .......... .......... .......... .......... .......... 74% 61.9M 10s
375450K .......... .......... .......... .......... .......... 74% 42.2M 10s
375500K .......... .......... .......... .......... .......... 74%  111M 10s
375550K .......... .......... .......... .......... .......... 74% 16.3M 10s
375600K .......... .......... .......... .......... .......... 74%  436M 10s
375650K .......... .......... .......... .......... .......... 74%  503M 10s
375700K .......... .......... .......... .......... .......... 74%  110M 10s
375750K .......... .......... .......... .......... .......... 74% 8.77M 10s
375800K .......... .......... .......... .......... .......... 74%  391M 10s
375850K .......... .......... .......... .......... .......... 74%  367M 10s
375900K .......... .......... .......... .......... .......... 74%  207M 10s
375950K .......... .......... .......... .......... .......... 74% 28.5M 10s
376000K .......... .......... .......... .......... .......... 74%  108M 10s
376050K .......... .......... .......... .......... .......... 74% 48.0M 10s
376100K .......... .......... .......... .......... .......... 74% 24.2M 10s
376150K .......... .......... .......... .......... .......... 74% 48.3M 10s
376200K .......... .......... .......... .......... .......... 74% 41.4M 10s
376250K .......... .......... .......... .......... .......... 74% 32.8M 10s
376300K .......... .......... .......... .......... .......... 74% 38.0M 10s
376350K .......... .......... .......... .......... .......... 74% 21.2M 10s
376400K .......... .......... .......... .......... .......... 74%  351M 10s
376450K .......... .......... .......... .......... .......... 74% 23.3M 10s
376500K .......... .......... .......... .......... .......... 74% 23.8M 10s
376550K .......... .......... .......... .......... .......... 74% 43.5M 10s
376600K .......... .......... .......... .......... .......... 74% 22.7M 10s
376650K .......... .......... .......... .......... .......... 74% 24.2M 10s
376700K .......... .......... .......... .......... .......... 74% 42.7M 10s
376750K .......... .......... .......... .......... .......... 74% 27.4M 10s
376800K .......... .......... .......... .......... .......... 74% 21.7M 10s
376850K .......... .......... .......... .......... .......... 74% 31.9M 10s
376900K .......... .......... .......... .......... .......... 74% 32.5M 10s
376950K .......... .......... .......... .......... .......... 74% 22.7M 10s
377000K .......... .......... .......... .......... .......... 74% 25.7M 10s
377050K .......... .......... .......... .......... .......... 74% 25.8M 10s
377100K .......... .......... .......... .......... .......... 74% 13.8M 10s
377150K .......... .......... .......... .......... .......... 74% 10.2M 10s
377200K .......... .......... .......... .......... .......... 74% 27.6M 10s
377250K .......... .......... .......... .......... .......... 74% 22.8M 10s
377300K .......... .......... .......... .......... .......... 74% 24.2M 10s
377350K .......... .......... .......... .......... .......... 74% 16.9M 10s
377400K .......... .......... .......... .......... .......... 74% 24.1M 10s
377450K .......... .......... .......... .......... .......... 74% 16.8M 10s
377500K .......... .......... .......... .......... .......... 74% 21.5M 10s
377550K .......... .......... .......... .......... .......... 74% 25.7M 10s
377600K .......... .......... .......... .......... .......... 74% 14.8M 10s
377650K .......... .......... .......... .......... .......... 74% 21.5M 10s
377700K .......... .......... .......... .......... .......... 75% 20.4M 10s
377750K .......... .......... .......... .......... .......... 75% 16.2M 10s
377800K .......... .......... .......... .......... .......... 75% 20.4M 10s
377850K .......... .......... .......... .......... .......... 75% 21.5M 10s
377900K .......... .......... .......... .......... .......... 75% 22.7M 10s
377950K .......... .......... .......... .......... .......... 75% 38.6M 10s
378000K .......... .......... .......... .......... .......... 75%  127M 10s
378050K .......... .......... .......... .......... .......... 75% 19.0M 10s
378100K .......... .......... .......... .......... .......... 75%  404M 10s
378150K .......... .......... .......... .......... .......... 75%  519M 10s
378200K .......... .......... .......... .......... .......... 75% 23.7M 10s
378250K .......... .......... .......... .......... .......... 75% 47.9M 10s
378300K .......... .......... .......... .......... .......... 75%  543M 10s
378350K .......... .......... .......... .......... .......... 75% 46.2M 10s
378400K .......... .......... .......... .......... .......... 75% 35.0M 10s
378450K .......... .......... .......... .......... .......... 75% 22.7M 10s
378500K .......... .......... .......... .......... .......... 75% 19.1M 10s
378550K .......... .......... .......... .......... .......... 75% 25.8M 10s
378600K .......... .......... .......... .......... .......... 75% 20.4M 10s
378650K .......... .......... .......... .......... .......... 75% 19.3M 10s
378700K .......... .......... .......... .......... .......... 75% 20.1M 10s
378750K .......... .......... .......... .......... .......... 75% 17.7M 10s
378800K .......... .......... .......... .......... .......... 75% 18.4M 10s
378850K .......... .......... .......... .......... .......... 75% 18.2M 10s
378900K .......... .......... .......... .......... .......... 75% 17.0M 10s
378950K .......... .......... .......... .......... .......... 75% 21.4M 10s
379000K .......... .......... .......... .......... .......... 75% 17.7M 10s
379050K .......... .......... .......... .......... .......... 75% 16.9M 10s
379100K .......... .......... .......... .......... .......... 75% 14.9M 10s
379150K .......... .......... .......... .......... .......... 75% 12.5M 10s
379200K .......... .......... .......... .......... .......... 75% 17.6M 10s
379250K .......... .......... .......... .......... .......... 75% 16.9M 10s
379300K .......... .......... .......... .......... .......... 75% 15.6M 10s
379350K .......... .......... .......... .......... .......... 75% 16.3M 10s
379400K .......... .......... .......... .......... .......... 75% 18.8M 10s
379450K .......... .......... .......... .......... .......... 75% 15.5M 10s
379500K .......... .......... .......... .......... .......... 75% 12.1M 10s
379550K .......... .......... .......... .......... .......... 75% 11.4M 10s
379600K .......... .......... .......... .......... .......... 75% 9.22M 10s
379650K .......... .......... .......... .......... .......... 75% 11.7M 10s
379700K .......... .......... .......... .......... .......... 75% 9.73M 10s
379750K .......... .......... .......... .......... .......... 75% 13.3M 10s
379800K .......... .......... .......... .......... .......... 75% 9.06M 10s
379850K .......... .......... .......... .......... .......... 75% 12.5M 10s
379900K .......... .......... .......... .......... .......... 75% 21.7M 10s
379950K .......... .......... .......... .......... .......... 75% 10.0M 10s
380000K .......... .......... .......... .......... .......... 75%  384M 10s
380050K .......... .......... .......... .......... .......... 75% 16.9M 10s
380100K .......... .......... .......... .......... .......... 75% 21.8M 10s
380150K .......... .......... .......... .......... .......... 75% 17.5M 9s
380200K .......... .......... .......... .......... .......... 75% 18.3M 9s
380250K .......... .......... .......... .......... .......... 75% 17.5M 9s
380300K .......... .......... .......... .......... .......... 75% 20.3M 9s
380350K .......... .......... .......... .......... .......... 75% 19.3M 9s
380400K .......... .......... .......... .......... .......... 75% 18.4M 9s
380450K .......... .......... .......... .......... .......... 75% 17.6M 9s
380500K .......... .......... .......... .......... .......... 75% 19.6M 9s
380550K .......... .......... .......... .......... .......... 75% 20.1M 9s
380600K .......... .......... .......... .......... .......... 75% 19.3M 9s
380650K .......... .......... .......... .......... .......... 75% 19.4M 9s
380700K .......... .......... .......... .......... .......... 75% 20.3M 9s
380750K .......... .......... .......... .......... .......... 75% 18.4M 9s
380800K .......... .......... .......... .......... .......... 75% 21.5M 9s
380850K .......... .......... .......... .......... .......... 75% 18.3M 9s
380900K .......... .......... .......... .......... .......... 75% 21.6M 9s
380950K .......... .......... .......... .......... .......... 75% 16.8M 9s
381000K .......... .......... .......... .......... .......... 75% 21.4M 9s
381050K .......... .......... .......... .......... .......... 75% 18.4M 9s
381100K .......... .......... .......... .......... .......... 75% 17.5M 9s
381150K .......... .......... .......... .......... .......... 75% 8.77M 9s
381200K .......... .......... .......... .......... .......... 75% 15.3M 9s
381250K .......... .......... .......... .......... .......... 75% 8.31M 9s
381300K .......... .......... .......... .......... .......... 75% 16.2M 9s
381350K .......... .......... .......... .......... .......... 75% 13.8M 9s
381400K .......... .......... .......... .......... .......... 75% 17.6M 9s
381450K .......... .......... .......... .......... .......... 75% 14.4M 9s
381500K .......... .......... .......... .......... .......... 75% 18.4M 9s
381550K .......... .......... .......... .......... .......... 75% 18.5M 9s
381600K .......... .......... .......... .......... .......... 75% 12.5M 9s
381650K .......... .......... .......... .......... .......... 75% 17.6M 9s
381700K .......... .......... .......... .......... .......... 75% 15.5M 9s
381750K .......... .......... .......... .......... .......... 75% 17.6M 9s
381800K .......... .......... .......... .......... .......... 75% 20.2M 9s
381850K .......... .......... .......... .......... .......... 75% 9.27M 9s
381900K .......... .......... .......... .......... .......... 75% 15.1M 9s
381950K .......... .......... .......... .......... .......... 75% 20.0M 9s
382000K .......... .......... .......... .......... .......... 75% 42.5M 9s
382050K .......... .......... .......... .......... .......... 75% 31.9M 9s
382100K .......... .......... .......... .......... .......... 75% 20.4M 9s
382150K .......... .......... .......... .......... .......... 75% 27.4M 9s
382200K .......... .......... .......... .......... .......... 75% 19.5M 9s
382250K .......... .......... .......... .......... .......... 75% 19.4M 9s
382300K .......... .......... .......... .......... .......... 75% 27.5M 9s
382350K .......... .......... .......... .......... .......... 75% 22.3M 9s
382400K .......... .......... .......... .......... .......... 75% 21.7M 9s
382450K .......... .......... .......... .......... .......... 75% 20.3M 9s
382500K .......... .......... .......... .......... .......... 75% 26.0M 9s
382550K .......... .......... .......... .......... .......... 75% 21.5M 9s
382600K .......... .......... .......... .......... .......... 75% 24.1M 9s
382650K .......... .......... .......... .......... .......... 75% 19.4M 9s
382700K .......... .......... .......... .......... .......... 76% 25.5M 9s
382750K .......... .......... .......... .......... .......... 76% 16.2M 9s
382800K .......... .......... .......... .......... .......... 76% 13.8M 9s
382850K .......... .......... .......... .......... .......... 76% 25.5M 9s
382900K .......... .......... .......... .......... .......... 76% 10.7M 9s
382950K .......... .......... .......... .......... .......... 76%  404M 9s
383000K .......... .......... .......... .......... .......... 76% 29.4M 9s
383050K .......... .......... .......... .......... .......... 76% 27.2M 9s
383100K .......... .......... .......... .......... .......... 76% 20.8M 9s
383150K .......... .......... .......... .......... .......... 76% 35.0M 9s
383200K .......... .......... .......... .......... .......... 76% 22.7M 9s
383250K .......... .......... .......... .......... .......... 76% 21.4M 9s
383300K .......... .......... .......... .......... .......... 76% 24.1M 9s
383350K .......... .......... .......... .......... .......... 76% 18.4M 9s
383400K .......... .......... .......... .......... .......... 76% 27.5M 9s
383450K .......... .......... .......... .......... .......... 76% 24.1M 9s
383500K .......... .......... .......... .......... .......... 76% 18.4M 9s
383550K .......... .......... .......... .......... .......... 76% 29.8M 9s
383600K .......... .......... .......... .......... .......... 76% 22.9M 9s
383650K .......... .......... .......... .......... .......... 76% 18.4M 9s
383700K .......... .......... .......... .......... .......... 76% 25.6M 9s
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383800K .......... .......... .......... .......... .......... 76% 25.8M 9s
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383900K .......... .......... .......... .......... .......... 76% 34.9M 9s
383950K .......... .......... .......... .......... .......... 76% 24.2M 9s
384000K .......... .......... .......... .......... .......... 76% 12.9M 9s
384050K .......... .......... .......... .......... .......... 76% 35.0M 9s
384100K .......... .......... .......... .......... .......... 76%  126M 9s
384150K .......... .......... .......... .......... .......... 76% 18.3M 9s
384200K .......... .......... .......... .......... .......... 76%  376M 9s
384250K .......... .......... .......... .......... .......... 76%  132M 9s
384300K .......... .......... .......... .......... .......... 76% 20.9M 9s
384350K .......... .......... .......... .......... .......... 76% 44.5M 9s
384400K .......... .......... .......... .......... .......... 76% 29.6M 9s
384450K .......... .......... .......... .......... .......... 76% 27.6M 9s
384500K .......... .......... .......... .......... .......... 76% 42.7M 9s
384550K .......... .......... .......... .......... .......... 76% 34.6M 9s
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384650K .......... .......... .......... .......... .......... 76% 37.8M 9s
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384750K .......... .......... .......... .......... .......... 76% 31.8M 9s
384800K .......... .......... .......... .......... .......... 76% 34.9M 9s
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384900K .......... .......... .......... .......... .......... 76% 31.7M 9s
384950K .......... .......... .......... .......... .......... 76% 27.3M 9s
385000K .......... .......... .......... .......... .......... 76% 42.2M 9s
385050K .......... .......... .......... .......... .......... 76% 38.9M 9s
385100K .......... .......... .......... .......... .......... 76% 31.7M 9s
385150K .......... .......... .......... .......... .......... 76% 29.5M 9s
385200K .......... .......... .......... .......... .......... 76% 31.9M 9s
385250K .......... .......... .......... .......... .......... 76% 26.9M 9s
385300K .......... .......... .......... .......... .......... 76% 29.3M 9s
385350K .......... .......... .......... .......... .......... 76% 34.2M 9s
385400K .......... .......... .......... .......... .......... 76% 27.3M 9s
385450K .......... .......... .......... .......... .......... 76% 19.1M 9s
385500K .......... .......... .......... .......... .......... 76% 8.68M 9s
385550K .......... .......... .......... .......... .......... 76%  112M 9s
385600K .......... .......... .......... .......... .......... 76% 14.3M 9s
385650K .......... .......... .......... .......... .......... 76% 32.4M 9s
385700K .......... .......... .......... .......... .......... 76% 13.8M 9s
385750K .......... .......... .......... .......... .......... 76% 23.8M 9s
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385850K .......... .......... .......... .......... .......... 76% 13.4M 9s
385900K .......... .......... .......... .......... .......... 76% 13.0M 9s
385950K .......... .......... .......... .......... .......... 76% 18.4M 9s
386000K .......... .......... .......... .......... .......... 76% 20.4M 9s
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386100K .......... .......... .......... .......... .......... 76% 15.4M 9s
386150K .......... .......... .......... .......... .......... 76% 17.7M 9s
386200K .......... .......... .......... .......... .......... 76% 16.8M 9s
386250K .......... .......... .......... .......... .......... 76% 21.3M 9s
386300K .......... .......... .......... .......... .......... 76% 17.8M 9s
386350K .......... .......... .......... .......... .......... 76% 16.2M 9s
386400K .......... .......... .......... .......... .......... 76% 27.6M 9s
386450K .......... .......... .......... .......... .......... 76% 17.7M 9s
386500K .......... .......... .......... .......... .......... 76% 21.4M 9s
386550K .......... .......... .......... .......... .......... 76% 24.1M 9s
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386650K .......... .......... .......... .......... .......... 76% 42.7M 9s
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386750K .......... .......... .......... .......... .......... 76% 14.0M 9s
386800K .......... .......... .......... .......... .......... 76%  407M 9s
386850K .......... .......... .......... .......... .......... 76% 28.8M 9s
386900K .......... .......... .......... .......... .......... 76%  296M 9s
386950K .......... .......... .......... .......... .......... 76% 24.5M 9s
387000K .......... .......... .......... .......... .......... 76% 24.9M 9s
387050K .......... .......... .......... .......... .......... 76% 49.1M 9s
387100K .......... .......... .......... .......... .......... 76% 25.2M 9s
387150K .......... .......... .......... .......... .......... 76% 29.3M 9s
387200K .......... .......... .......... .......... .......... 76% 30.6M 9s
387250K .......... .......... .......... .......... .......... 76% 29.2M 9s
387300K .......... .......... .......... .......... .......... 76% 34.1M 9s
387350K .......... .......... .......... .......... .......... 76% 24.4M 9s
387400K .......... .......... .......... .......... .......... 76% 29.3M 9s
387450K .......... .......... .......... .......... .......... 76% 30.6M 9s
387500K .......... .......... .......... .......... .......... 76% 29.1M 9s
387550K .......... .......... .......... .......... .......... 76% 42.2M 9s
387600K .......... .......... .......... .......... .......... 76% 25.3M 9s
387650K .......... .......... .......... .......... .......... 76% 26.2M 9s
387700K .......... .......... .......... .......... .......... 76% 32.0M 9s
387750K .......... .......... .......... .......... .......... 77% 29.8M 9s
387800K .......... .......... .......... .......... .......... 77% 34.5M 9s
387850K .......... .......... .......... .......... .......... 77% 26.1M 9s
387900K .......... .......... .......... .......... .......... 77% 35.0M 9s
387950K .......... .......... .......... .......... .......... 77% 25.5M 9s
388000K .......... .......... .......... .......... .......... 77% 38.8M 9s
388050K .......... .......... .......... .......... .......... 77% 27.3M 9s
388100K .......... .......... .......... .......... .......... 77% 35.2M 9s
388150K .......... .......... .......... .......... .......... 77% 30.1M 9s
388200K .......... .......... .......... .......... .......... 77% 10.9M 9s
388250K .......... .......... .......... .......... .......... 77%  440M 9s
388300K .......... .......... .......... .......... .......... 77% 12.7M 9s
388350K .......... .......... .......... .......... .......... 77%  384M 9s
388400K .......... .......... .......... .......... .......... 77%  410M 9s
388450K .......... .......... .......... .......... .......... 77% 13.3M 9s
388500K .......... .......... .......... .......... .......... 77%  181M 9s
388550K .......... .......... .......... .......... .......... 77% 95.9M 9s
388600K .......... .......... .......... .......... .......... 77% 30.3M 9s
388650K .......... .......... .......... .......... .......... 77% 38.5M 9s
388700K .......... .......... .......... .......... .......... 77% 29.5M 9s
388750K .......... .......... .......... .......... .......... 77% 34.6M 9s
388800K .......... .......... .......... .......... .......... 77% 33.8M 9s
388850K .......... .......... .......... .......... .......... 77% 29.3M 9s
388900K .......... .......... .......... .......... .......... 77% 28.6M 9s
388950K .......... .......... .......... .......... .......... 77% 25.4M 9s
389000K .......... .......... .......... .......... .......... 77% 46.4M 9s
389050K .......... .......... .......... .......... .......... 77% 29.5M 9s
389100K .......... .......... .......... .......... .......... 77% 32.6M 9s
389150K .......... .......... .......... .......... .......... 77% 25.5M 9s
389200K .......... .......... .......... .......... .......... 77% 32.6M 9s
389250K .......... .......... .......... .......... .......... 77% 29.3M 9s
389300K .......... .......... .......... .......... .......... 77% 42.8M 9s
389350K .......... .......... .......... .......... .......... 77% 24.5M 9s
389400K .......... .......... .......... .......... .......... 77% 38.6M 9s
389450K .......... .......... .......... .......... .......... 77% 29.7M 9s
389500K .......... .......... .......... .......... .......... 77% 42.1M 9s
389550K .......... .......... .......... .......... .......... 77% 29.7M 9s
389600K .......... .......... .......... .......... .......... 77% 38.4M 9s
389650K .......... .......... .......... .......... .......... 77% 27.9M 9s
389700K .......... .......... .......... .......... .......... 77% 32.2M 9s
389750K .......... .......... .......... .......... .......... 77% 41.8M 9s
389800K .......... .......... .......... .......... .......... 77% 49.0M 9s
389850K .......... .......... .......... .......... .......... 77% 31.8M 9s
389900K .......... .......... .......... .......... .......... 77% 14.0M 9s
389950K .......... .......... .......... .......... .......... 77%  300M 9s
390000K .......... .......... .......... .......... .......... 77%  367M 9s
390050K .......... .......... .......... .......... .......... 77%  220M 9s
390100K .......... .......... .......... .......... .......... 77% 14.9M 9s
390150K .......... .......... .......... .......... .......... 77%  410M 9s
390200K .......... .......... .......... .......... .......... 77% 32.1M 9s
390250K .......... .......... .......... .......... .......... 77% 56.4M 9s
390300K .......... .......... .......... .......... .......... 77% 46.9M 9s
390350K .......... .......... .......... .......... .......... 77% 81.9M 9s
390400K .......... .......... .......... .......... .......... 77% 42.3M 9s
390450K .......... .......... .......... .......... .......... 77% 35.2M 9s
390500K .......... .......... .......... .......... .......... 77% 48.1M 9s
390550K .......... .......... .......... .......... .......... 77% 38.5M 9s
390600K .......... .......... .......... .......... .......... 77% 37.8M 9s
390650K .......... .......... .......... .......... .......... 77% 39.1M 9s
390700K .......... .......... .......... .......... .......... 77% 32.0M 9s
390750K .......... .......... .......... .......... .......... 77% 54.9M 9s
390800K .......... .......... .......... .......... .......... 77% 62.3M 9s
390850K .......... .......... .......... .......... .......... 77% 35.5M 9s
390900K .......... .......... .......... .......... .......... 77% 38.8M 9s
390950K .......... .......... .......... .......... .......... 77% 42.6M 9s
391000K .......... .......... .......... .......... .......... 77% 38.6M 9s
391050K .......... .......... .......... .......... .......... 77% 38.5M 9s
391100K .......... .......... .......... .......... .......... 77% 27.2M 9s
391150K .......... .......... .......... .......... .......... 77% 55.0M 9s
391200K .......... .......... .......... .......... .......... 77% 38.5M 9s
391250K .......... .......... .......... .......... .......... 77% 43.6M 9s
391300K .......... .......... .......... .......... .......... 77% 34.8M 9s
391350K .......... .......... .......... .......... .......... 77% 29.8M 9s
391400K .......... .......... .......... .......... .......... 77% 42.2M 9s
391450K .......... .......... .......... .......... .......... 77% 27.6M 9s
391500K .......... .......... .......... .......... .......... 77% 48.0M 9s
391550K .......... .......... .......... .......... .......... 77% 48.6M 8s
391600K .......... .......... .......... .......... .......... 77% 32.0M 8s
391650K .......... .......... .......... .......... .......... 77% 38.8M 8s
391700K .......... .......... .......... .......... .......... 77% 22.8M 8s
391750K .......... .......... .......... .......... .......... 77% 38.6M 8s
391800K .......... .......... .......... .......... .......... 77% 18.0M 8s
391850K .......... .......... .......... .......... .......... 77%  315M 8s
391900K .......... .......... .......... .......... .......... 77% 38.2M 8s
391950K .......... .......... .......... .......... .......... 77% 43.2M 8s
392000K .......... .......... .......... .......... .......... 77% 54.6M 8s
392050K .......... .......... .......... .......... .......... 77% 54.4M 8s
392100K .......... .......... .......... .......... .......... 77% 40.4M 8s
392150K .......... .......... .......... .......... .......... 77% 38.0M 8s
392200K .......... .......... .......... .......... .......... 77% 27.6M 8s
392250K .......... .......... .......... .......... .......... 77% 29.8M 8s
392300K .......... .......... .......... .......... .......... 77% 47.4M 8s
392350K .......... .......... .......... .......... .......... 77% 32.6M 8s
392400K .......... .......... .......... .......... .......... 77% 38.3M 8s
392450K .......... .......... .......... .......... .......... 77% 38.5M 8s
392500K .......... .......... .......... .......... .......... 77% 38.6M 8s
392550K .......... .......... .......... .......... .......... 77% 35.0M 8s
392600K .......... .......... .......... .......... .......... 77% 32.2M 8s
392650K .......... .......... .......... .......... .......... 77% 38.4M 8s
392700K .......... .......... .......... .......... .......... 77% 35.1M 8s
392750K .......... .......... .......... .......... .......... 77% 47.1M 8s
392800K .......... .......... .......... .......... .......... 78% 39.3M 8s
392850K .......... .......... .......... .......... .......... 78% 27.4M 8s
392900K .......... .......... .......... .......... .......... 78% 54.3M 8s
392950K .......... .......... .......... .......... .......... 78% 22.7M 8s
393000K .......... .......... .......... .......... .......... 78% 53.2M 8s
393050K .......... .......... .......... .......... .......... 78% 39.8M 8s
393100K .......... .......... .......... .......... .......... 78% 29.9M 8s
393150K .......... .......... .......... .......... .......... 78% 42.5M 8s
393200K .......... .......... .......... .......... .......... 78% 35.1M 8s
393250K .......... .......... .......... .......... .......... 78% 29.9M 8s
393300K .......... .......... .......... .......... .......... 78% 42.9M 8s
393350K .......... .......... .......... .......... .......... 78% 53.4M 8s
393400K .......... .......... .......... .......... .......... 78% 39.0M 8s
393450K .......... .......... .......... .......... .......... 78% 63.7M 8s
393500K .......... .......... .......... .......... .......... 78% 21.3M 8s
393550K .......... .......... .......... .......... .......... 78%  370M 8s
393600K .......... .......... .......... .......... .......... 78%  373M 8s
393650K .......... .......... .......... .......... .......... 78% 33.8M 8s
393700K .......... .......... .......... .......... .......... 78% 22.5M 8s
393750K .......... .......... .......... .......... .......... 78%  332M 8s
393800K .......... .......... .......... .......... .......... 78% 88.3M 8s
393850K .......... .......... .......... .......... .......... 78%  373M 8s
393900K .......... .......... .......... .......... .......... 78% 51.7M 8s
393950K .......... .......... .......... .......... .......... 78% 58.1M 8s
394000K .......... .......... .......... .......... .......... 78% 48.5M 8s
394050K .......... .......... .......... .......... .......... 78% 42.9M 8s
394100K .......... .......... .......... .......... .......... 78% 22.4M 8s
394150K .......... .......... .......... .......... .......... 78%  428M 8s
394200K .......... .......... .......... .......... .......... 78% 29.7M 8s
394250K .......... .......... .......... .......... .......... 78% 32.0M 8s
394300K .......... .......... .......... .......... .......... 78% 48.0M 8s
394350K .......... .......... .......... .......... .......... 78% 27.3M 8s
394400K .......... .......... .......... .......... .......... 78% 43.7M 8s
394450K .......... .......... .......... .......... .......... 78% 34.7M 8s
394500K .......... .......... .......... .......... .......... 78% 29.8M 8s
394550K .......... .......... .......... .......... .......... 78% 36.6M 8s
394600K .......... .......... .......... .......... .......... 78% 40.4M 8s
394650K .......... .......... .......... .......... .......... 78% 27.6M 8s
394700K .......... .......... .......... .......... .......... 78% 31.6M 8s
394750K .......... .......... .......... .......... .......... 78% 25.8M 8s
394800K .......... .......... .......... .......... .......... 78% 27.7M 8s
394850K .......... .......... .......... .......... .......... 78% 31.6M 8s
394900K .......... .......... .......... .......... .......... 78% 26.0M 8s
394950K .......... .......... .......... .......... .......... 78% 25.7M 8s
395000K .......... .......... .......... .......... .......... 78% 35.1M 8s
395050K .......... .......... .......... .......... .......... 78% 24.2M 8s
395100K .......... .......... .......... .......... .......... 78% 18.4M 8s
395150K .......... .......... .......... .......... .......... 78% 27.4M 8s
395200K .......... .......... .......... .......... .......... 78% 11.4M 8s
395250K .......... .......... .......... .......... .......... 78% 16.6M 8s
395300K .......... .......... .......... .......... .......... 78% 10.6M 8s
395350K .......... .......... .......... .......... .......... 78% 11.7M 8s
395400K .......... .......... .......... .......... .......... 78% 12.9M 8s
395450K .......... .......... .......... .......... .......... 78% 10.8M 8s
395500K .......... .......... .......... .......... .......... 78% 10.8M 8s
395550K .......... .......... .......... .......... .......... 78% 12.5M 8s
395600K .......... .......... .......... .......... .......... 78% 6.23M 8s
395650K .......... .......... .......... .......... .......... 78% 9.67M 8s
395700K .......... .......... .......... .......... .......... 78% 8.40M 8s
395750K .......... .......... .......... .......... .......... 78% 3.85M 8s
395800K .......... .......... .......... .......... .......... 78% 7.74M 8s
395850K .......... .......... .......... .......... .......... 78% 12.0M 8s
395900K .......... .......... .......... .......... .......... 78% 29.5M 8s
395950K .......... .......... .......... .......... .......... 78% 46.0M 8s
396000K .......... .......... .......... .......... .......... 78% 14.0M 8s
396050K .......... .......... .......... .......... .......... 78% 17.8M 8s
396100K .......... .......... .......... .......... .......... 78% 15.0M 8s
396150K .......... .......... .......... .......... .......... 78% 19.3M 8s
396200K .......... .......... .......... .......... .......... 78% 17.5M 8s
396250K .......... .......... .......... .......... .......... 78% 21.5M 8s
396300K .......... .......... .......... .......... .......... 78% 16.8M 8s
396350K .......... .......... .......... .......... .......... 78% 18.5M 8s
396400K .......... .......... .......... .......... .......... 78% 18.4M 8s
396450K .......... .......... .......... .......... .......... 78% 18.5M 8s
396500K .......... .......... .......... .......... .......... 78% 18.4M 8s
396550K .......... .......... .......... .......... .......... 78% 14.9M 8s
396600K .......... .......... .......... .......... .......... 78% 19.1M 8s
396650K .......... .......... .......... .......... .......... 78% 17.6M 8s
396700K .......... .......... .......... .......... .......... 78% 13.8M 8s
396750K .......... .......... .......... .......... .......... 78% 20.7M 8s
396800K .......... .......... .......... .......... .......... 78% 42.9M 8s
396850K .......... .......... .......... .......... .......... 78% 52.8M 8s
396900K .......... .......... .......... .......... .......... 78% 43.0M 8s
396950K .......... .......... .......... .......... .......... 78% 44.8M 8s
397000K .......... .......... .......... .......... .......... 78% 25.8M 8s
397050K .......... .......... .......... .......... .......... 78% 10.3M 8s
397100K .......... .......... .......... .......... .......... 78%  373M 8s
397150K .......... .......... .......... .......... .......... 78% 15.4M 8s
397200K .......... .......... .......... .......... .......... 78%  209M 8s
397250K .......... .......... .......... .......... .......... 78% 22.9M 8s
397300K .......... .......... .......... .......... .......... 78% 15.7M 8s
397350K .......... .......... .......... .......... .......... 78% 21.7M 8s
397400K .......... .......... .......... .......... .......... 78% 21.4M 8s
397450K .......... .......... .......... .......... .......... 78% 16.8M 8s
397500K .......... .......... .......... .......... .......... 78% 14.4M 8s
397550K .......... .......... .......... .......... .......... 78% 15.5M 8s
397600K .......... .......... .......... .......... .......... 78% 14.9M 8s
397650K .......... .......... .......... .......... .......... 78% 14.4M 8s
397700K .......... .......... .......... .......... .......... 78% 19.3M 8s
397750K .......... .......... .......... .......... .......... 78% 16.8M 8s
397800K .......... .......... .......... .......... .......... 79% 24.1M 8s
397850K .......... .......... .......... .......... .......... 79% 12.9M 8s
397900K .......... .......... .......... .......... .......... 79% 14.9M 8s
397950K .......... .......... .......... .......... .......... 79% 8.04M 8s
398000K .......... .......... .......... .......... .......... 79% 13.4M 8s
398050K .......... .......... .......... .......... .......... 79% 17.7M 8s
398100K .......... .......... .......... .......... .......... 79% 16.8M 8s
398150K .......... .......... .......... .......... .......... 79% 20.4M 8s
398200K .......... .......... .......... .......... .......... 79% 12.1M 8s
398250K .......... .......... .......... .......... .......... 79% 18.4M 8s
398300K .......... .......... .......... .......... .......... 79% 19.3M 8s
398350K .......... .......... .......... .......... .......... 79% 13.8M 8s
398400K .......... .......... .......... .......... .......... 79% 13.4M 8s
398450K .......... .......... .......... .......... .......... 79% 16.8M 8s
398500K .......... .......... .......... .......... .......... 79% 20.4M 8s
398550K .......... .......... .......... .......... .......... 79% 20.4M 8s
398600K .......... .......... .......... .......... .......... 79% 13.8M 8s
398650K .......... .......... .......... .......... .......... 79% 18.4M 8s
398700K .......... .......... .......... .......... .......... 79% 31.3M 8s
398750K .......... .......... .......... .......... .......... 79% 26.0M 8s
398800K .......... .......... .......... .......... .......... 79% 21.6M 8s
398850K .......... .......... .......... .......... .......... 79% 14.3M 8s
398900K .......... .......... .......... .......... .......... 79%  381M 8s
398950K .......... .......... .......... .......... .......... 79% 18.5M 8s
399000K .......... .......... .......... .......... .......... 79%  319M 8s
399050K .......... .......... .......... .......... .......... 79% 27.7M 8s
399100K .......... .......... .......... .......... .......... 79% 42.9M 8s
399150K .......... .......... .......... .......... .......... 79% 35.1M 8s
399200K .......... .......... .......... .......... .......... 79% 20.3M 8s
399250K .......... .......... .......... .......... .......... 79% 32.1M 8s
399300K .......... .......... .......... .......... .......... 79% 20.3M 8s
399350K .......... .......... .......... .......... .......... 79% 27.7M 8s
399400K .......... .......... .......... .......... .......... 79% 29.7M 8s
399450K .......... .......... .......... .......... .......... 79% 29.6M 8s
399500K .......... .......... .......... .......... .......... 79% 29.2M 8s
399550K .......... .......... .......... .......... .......... 79% 26.2M 8s
399600K .......... .......... .......... .......... .......... 79% 24.2M 8s
399650K .......... .......... .......... .......... .......... 79% 27.6M 8s
399700K .......... .......... .......... .......... .......... 79% 25.7M 8s
399750K .......... .......... .......... .......... .......... 79% 24.1M 8s
399800K .......... .......... .......... .......... .......... 79% 37.1M 8s
399850K .......... .......... .......... .......... .......... 79% 18.8M 8s
399900K .......... .......... .......... .......... .......... 79% 29.7M 8s
399950K .......... .......... .......... .......... .......... 79% 32.0M 8s
400000K .......... .......... .......... .......... .......... 79% 27.2M 8s
400050K .......... .......... .......... .......... .......... 79% 43.0M 8s
400100K .......... .......... .......... .......... .......... 79% 42.7M 8s
400150K .......... .......... .......... .......... .......... 79% 39.3M 8s
400200K .......... .......... .......... .......... .......... 79% 34.0M 8s
400250K .......... .......... .......... .......... .......... 79% 83.6M 8s
400300K .......... .......... .......... .......... .......... 79% 14.5M 8s
400350K .......... .......... .......... .......... .......... 79% 54.0M 8s
400400K .......... .......... .......... .......... .......... 79% 64.5M 8s
400450K .......... .......... .......... .......... .......... 79% 30.4M 8s
400500K .......... .......... .......... .......... .......... 79%  397M 8s
400550K .......... .......... .......... .......... .......... 79% 25.6M 8s
400600K .......... .......... .......... .......... .......... 79% 43.9M 8s
400650K .......... .......... .......... .......... .......... 79% 48.3M 8s
400700K .......... .......... .......... .......... .......... 79% 34.9M 8s
400750K .......... .......... .......... .......... .......... 79% 32.0M 8s
400800K .......... .......... .......... .......... .......... 79% 48.4M 8s
400850K .......... .......... .......... .......... .......... 79% 34.9M 8s
400900K .......... .......... .......... .......... .......... 79% 27.6M 8s
400950K .......... .......... .......... .......... .......... 79% 41.3M 8s
401000K .......... .......... .......... .......... .......... 79% 49.3M 8s
401050K .......... .......... .......... .......... .......... 79% 35.3M 8s
401100K .......... .......... .......... .......... .......... 79% 27.5M 8s
401150K .......... .......... .......... .......... .......... 79% 47.1M 8s
401200K .......... .......... .......... .......... .......... 79% 42.9M 8s
401250K .......... .......... .......... .......... .......... 79% 27.9M 8s
401300K .......... .......... .......... .......... .......... 79% 48.0M 8s
401350K .......... .......... .......... .......... .......... 79% 35.0M 8s
401400K .......... .......... .......... .......... .......... 79% 6.07M 8s
401450K .......... .......... .......... .......... .......... 79% 26.1M 8s
401500K .......... .......... .......... .......... .......... 79% 46.8M 8s
401550K .......... .......... .......... .......... .......... 79% 48.2M 8s
401600K .......... .......... .......... .......... .......... 79% 32.0M 8s
401650K .......... .......... .......... .......... .......... 79% 49.3M 8s
401700K .......... .......... .......... .......... .......... 79% 48.2M 8s
401750K .......... .......... .......... .......... .......... 79% 35.2M 8s
401800K .......... .......... .......... .......... .......... 79% 42.1M 8s
401850K .......... .......... .......... .......... .......... 79% 11.2M 8s
401900K .......... .......... .......... .......... .......... 79%  182M 8s
401950K .......... .......... .......... .......... .......... 79%  367M 8s
402000K .......... .......... .......... .......... .......... 79% 37.6M 8s
402050K .......... .......... .......... .......... .......... 79% 43.4M 8s
402100K .......... .......... .......... .......... .......... 79%  400M 8s
402150K .......... .......... .......... .......... .......... 79% 42.0M 8s
402200K .......... .......... .......... .......... .......... 79% 20.8M 8s
402250K .......... .......... .......... .......... .......... 79% 27.4M 8s
402300K .......... .......... .......... .......... .......... 79% 89.3M 8s
402350K .......... .......... .......... .......... .......... 79% 38.9M 8s
402400K .......... .......... .......... .......... .......... 79% 32.4M 8s
402450K .......... .......... .......... .......... .......... 79% 24.1M 8s
402500K .......... .......... .......... .......... .......... 79% 42.6M 8s
402550K .......... .......... .......... .......... .......... 79% 38.0M 8s
402600K .......... .......... .......... .......... .......... 79% 25.7M 8s
402650K .......... .......... .......... .......... .......... 79% 38.5M 8s
402700K .......... .......... .......... .......... .......... 79% 27.2M 8s
402750K .......... .......... .......... .......... .......... 79% 30.0M 8s
402800K .......... .......... .......... .......... .......... 79% 27.8M 8s
402850K .......... .......... .......... .......... .......... 80% 34.5M 8s
402900K .......... .......... .......... .......... .......... 80% 39.0M 8s
402950K .......... .......... .......... .......... .......... 80% 31.8M 8s
403000K .......... .......... .......... .......... .......... 80% 42.6M 8s
403050K .......... .......... .......... .......... .......... 80% 43.5M 8s
403100K .......... .......... .......... .......... .......... 80% 24.2M 8s
403150K .......... .......... .......... .......... .......... 80% 35.1M 8s
403200K .......... .......... .......... .......... .......... 80% 38.3M 8s
403250K .......... .......... .......... .......... .......... 80% 29.9M 8s
403300K .......... .......... .......... .......... .......... 80% 38.7M 7s
403350K .......... .......... .......... .......... .......... 80% 29.5M 7s
403400K .......... .......... .......... .......... .......... 80% 48.5M 7s
403450K .......... .......... .......... .......... .......... 80% 27.5M 7s
403500K .......... .......... .......... .......... .......... 80% 31.7M 7s
403550K .......... .......... .......... .......... .......... 80% 26.0M 7s
403600K .......... .......... .......... .......... .......... 80% 20.4M 7s
403650K .......... .......... .......... .......... .......... 80%  356M 7s
403700K .......... .......... .......... .......... .......... 80% 20.1M 7s
403750K .......... .......... .......... .......... .......... 80%  196M 7s
403800K .......... .......... .......... .......... .......... 80% 32.0M 7s
403850K .......... .......... .......... .......... .......... 80% 28.8M 7s
403900K .......... .......... .......... .......... .......... 80% 33.1M 7s
403950K .......... .......... .......... .......... .......... 80% 29.4M 7s
404000K .......... .......... .......... .......... .......... 80% 32.3M 7s
404050K .......... .......... .......... .......... .......... 80% 32.5M 7s
404100K .......... .......... .......... .......... .......... 80% 29.6M 7s
404150K .......... .......... .......... .......... .......... 80% 38.6M 7s
404200K .......... .......... .......... .......... .......... 80% 22.3M 7s
404250K .......... .......... .......... .......... .......... 80% 39.6M 7s
404300K .......... .......... .......... .......... .......... 80% 22.7M 7s
404350K .......... .......... .......... .......... .......... 80% 22.5M 7s
404400K .......... .......... .......... .......... .......... 80% 39.1M 7s
404450K .......... .......... .......... .......... .......... 80% 25.5M 7s
404500K .......... .......... .......... .......... .......... 80% 27.9M 7s
404550K .......... .......... .......... .......... .......... 80% 38.6M 7s
404600K .......... .......... .......... .......... .......... 80% 27.7M 7s
404650K .......... .......... .......... .......... .......... 80% 25.7M 7s
404700K .......... .......... .......... .......... .......... 80% 25.8M 7s
404750K .......... .......... .......... .......... .......... 80% 35.2M 7s
404800K .......... .......... .......... .......... .......... 80% 27.6M 7s
404850K .......... .......... .......... .......... .......... 80% 25.7M 7s
404900K .......... .......... .......... .......... .......... 80% 17.6M 7s
404950K .......... .......... .......... .......... .......... 80% 17.6M 7s
405000K .......... .......... .......... .......... .......... 80% 21.5M 7s
405050K .......... .......... .......... .......... .......... 80% 32.1M 7s
405100K .......... .......... .......... .......... .......... 80% 20.3M 7s
405150K .......... .......... .......... .......... .......... 80% 25.5M 7s
405200K .......... .......... .......... .......... .......... 80% 21.7M 7s
405250K .......... .......... .......... .......... .......... 80% 18.1M 7s
405300K .......... .......... .......... .......... .......... 80%  474M 7s
405350K .......... .......... .......... .......... .......... 80% 25.2M 7s
405400K .......... .......... .......... .......... .......... 80% 91.6M 7s
405450K .......... .......... .......... .......... .......... 80% 22.1M 7s
405500K .......... .......... .......... .......... .......... 80% 27.2M 7s
405550K .......... .......... .......... .......... .......... 80% 43.6M 7s
405600K .......... .......... .......... .......... .......... 80% 29.7M 7s
405650K .......... .......... .......... .......... .......... 80% 27.6M 7s
405700K .......... .......... .......... .......... .......... 80% 21.4M 7s
405750K .......... .......... .......... .......... .......... 80% 22.8M 7s
405800K .......... .......... .......... .......... .......... 80% 29.7M 7s
405850K .......... .......... .......... .......... .......... 80% 21.4M 7s
405900K .......... .......... .......... .......... .......... 80% 42.5M 7s
405950K .......... .......... .......... .......... .......... 80% 20.5M 7s
406000K .......... .......... .......... .......... .......... 80% 29.5M 7s
406050K .......... .......... .......... .......... .......... 80% 24.3M 7s
406100K .......... .......... .......... .......... .......... 80% 24.2M 7s
406150K .......... .......... .......... .......... .......... 80% 34.6M 7s
406200K .......... .......... .......... .......... .......... 80% 17.7M 7s
406250K .......... .......... .......... .......... .......... 80% 37.9M 7s
406300K .......... .......... .......... .......... .......... 80% 21.7M 7s
406350K .......... .......... .......... .......... .......... 80% 25.7M 7s
406400K .......... .......... .......... .......... .......... 80% 17.5M 7s
406450K .......... .......... .......... .......... .......... 80% 14.4M 7s
406500K .......... .......... .......... .......... .......... 80% 14.2M 7s
406550K .......... .......... .......... .......... .......... 80% 34.2M 7s
406600K .......... .......... .......... .......... .......... 80% 38.7M 7s
406650K .......... .......... .......... .......... .......... 80% 21.9M 7s
406700K .......... .......... .......... .......... .......... 80% 19.4M 7s
406750K .......... .......... .......... .......... .......... 80% 17.4M 7s
406800K .......... .......... .......... .......... .......... 80% 16.2M 7s
406850K .......... .......... .......... .......... .......... 80% 17.7M 7s
406900K .......... .......... .......... .......... .......... 80% 16.0M 7s
406950K .......... .......... .......... .......... .......... 80% 17.0M 7s
407000K .......... .......... .......... .......... .......... 80% 15.5M 7s
407050K .......... .......... .......... .......... .......... 80% 22.7M 7s
407100K .......... .......... .......... .......... .......... 80% 12.9M 7s
407150K .......... .......... .......... .......... .......... 80% 22.8M 7s
407200K .......... .......... .......... .......... .......... 80% 13.8M 7s
407250K .......... .......... .......... .......... .......... 80% 7.76M 7s
407300K .......... .......... .......... .......... .......... 80% 10.4M 7s
407350K .......... .......... .......... .......... .......... 80% 10.3M 7s
407400K .......... .......... .......... .......... .......... 80% 11.4M 7s
407450K .......... .......... .......... .......... .......... 80% 13.8M 7s
407500K .......... .......... .......... .......... .......... 80% 10.2M 7s
407550K .......... .......... .......... .......... .......... 80% 12.9M 7s
407600K .......... .......... .......... .......... .......... 80% 11.7M 7s
407650K .......... .......... .......... .......... .......... 80% 12.8M 7s
407700K .......... .......... .......... .......... .......... 80% 10.1M 7s
407750K .......... .......... .......... .......... .......... 80% 21.4M 7s
407800K .......... .......... .......... .......... .......... 80% 14.2M 7s
407850K .......... .......... .......... .......... .......... 80% 20.8M 7s
407900K .......... .......... .......... .......... .......... 81% 61.6M 7s
407950K .......... .......... .......... .......... .......... 81% 18.2M 7s
408000K .......... .......... .......... .......... .......... 81% 14.7M 7s
408050K .......... .......... .......... .......... .......... 81% 56.6M 7s
408100K .......... .......... .......... .......... .......... 81% 13.7M 7s
408150K .......... .......... .......... .......... .......... 81% 37.9M 7s
408200K .......... .......... .......... .......... .......... 81% 31.1M 7s
408250K .......... .......... .......... .......... .......... 81% 30.2M 7s
408300K .......... .......... .......... .......... .......... 81% 24.0M 7s
408350K .......... .......... .......... .......... .......... 81% 14.5M 7s
408400K .......... .......... .......... .......... .......... 81% 25.2M 7s
408450K .......... .......... .......... .......... .......... 81% 14.8M 7s
408500K .......... .......... .......... .......... .......... 81% 20.3M 7s
408550K .......... .......... .......... .......... .......... 81% 23.4M 7s
408600K .......... .......... .......... .......... .......... 81% 17.3M 7s
408650K .......... .......... .......... .......... .......... 81% 16.0M 7s
408700K .......... .......... .......... .......... .......... 81% 21.3M 7s
408750K .......... .......... .......... .......... .......... 81% 20.2M 7s
408800K .......... .......... .......... .......... .......... 81% 21.1M 7s
408850K .......... .......... .......... .......... .......... 81% 16.0M 7s
408900K .......... .......... .......... .......... .......... 81% 9.24M 7s
408950K .......... .......... .......... .......... .......... 81% 24.9M 7s
409000K .......... .......... .......... .......... .......... 81% 9.63M 7s
409050K .......... .......... .......... .......... .......... 81% 16.0M 7s
409100K .......... .......... .......... .......... .......... 81% 11.6M 7s
409150K .......... .......... .......... .......... .......... 81% 11.6M 7s
409200K .......... .......... .......... .......... .......... 81% 11.7M 7s
409250K .......... .......... .......... .......... .......... 81% 11.7M 7s
409300K .......... .......... .......... .......... .......... 81% 11.4M 7s
409350K .......... .......... .......... .......... .......... 81% 10.7M 7s
409400K .......... .......... .......... .......... .......... 81% 14.3M 7s
409450K .......... .......... .......... .......... .......... 81% 12.9M 7s
409500K .......... .......... .......... .......... .......... 81% 12.5M 7s
409550K .......... .......... .......... .......... .......... 81% 14.9M 7s
409600K .......... .......... .......... .......... .......... 81% 16.8M 7s
409650K .......... .......... .......... .......... .......... 81% 13.3M 7s
409700K .......... .......... .......... .......... .......... 81% 17.6M 7s
409750K .......... .......... .......... .......... .......... 81% 19.4M 7s
409800K .......... .......... .......... .......... .......... 81% 13.4M 7s
409850K .......... .......... .......... .......... .......... 81% 10.8M 7s
409900K .......... .......... .......... .......... .......... 81% 14.3M 7s
409950K .......... .......... .......... .......... .......... 81% 12.0M 7s
410000K .......... .......... .......... .......... .......... 81% 13.3M 7s
410050K .......... .......... .......... .......... .......... 81% 16.1M 7s
410100K .......... .......... .......... .......... .......... 81% 14.8M 7s
410150K .......... .......... .......... .......... .......... 81% 16.6M 7s
410200K .......... .......... .......... .......... .......... 81% 14.7M 7s
410250K .......... .......... .......... .......... .......... 81% 10.0M 7s
410300K .......... .......... .......... .......... .......... 81% 14.4M 7s
410350K .......... .......... .......... .......... .......... 81% 12.1M 7s
410400K .......... .......... .......... .......... .......... 81% 34.8M 7s
410450K .......... .......... .......... .......... .......... 81% 32.1M 7s
410500K .......... .......... .......... .......... .......... 81% 27.9M 7s
410550K .......... .......... .......... .......... .......... 81%  474M 7s
410600K .......... .......... .......... .......... .......... 81% 30.4M 7s
410650K .......... .......... .......... .......... .......... 81% 53.9M 7s
410700K .......... .......... .......... .......... .......... 81% 26.9M 7s
410750K .......... .......... .......... .......... .......... 81% 41.5M 7s
410800K .......... .......... .......... .......... .......... 81% 38.4M 7s
410850K .......... .......... .......... .......... .......... 81% 31.0M 7s
410900K .......... .......... .......... .......... .......... 81% 51.6M 7s
410950K .......... .......... .......... .......... .......... 81% 37.2M 7s
411000K .......... .......... .......... .......... .......... 81% 27.7M 7s
411050K .......... .......... .......... .......... .......... 81% 42.8M 7s
411100K .......... .......... .......... .......... .......... 81% 29.4M 7s
411150K .......... .......... .......... .......... .......... 81% 55.0M 7s
411200K .......... .......... .......... .......... .......... 81% 32.0M 7s
411250K .......... .......... .......... .......... .......... 81% 53.8M 7s
411300K .......... .......... .......... .......... .......... 81% 39.1M 7s
411350K .......... .......... .......... .......... .......... 81% 25.6M 7s
411400K .......... .......... .......... .......... .......... 81% 48.2M 7s
411450K .......... .......... .......... .......... .......... 81% 42.1M 7s
411500K .......... .......... .......... .......... .......... 81% 29.8M 7s
411550K .......... .......... .......... .......... .......... 81% 46.5M 7s
411600K .......... .......... .......... .......... .......... 81% 42.5M 7s
411650K .......... .......... .......... .......... .......... 81% 41.1M 7s
411700K .......... .......... .......... .......... .......... 81% 25.6M 7s
411750K .......... .......... .......... .......... .......... 81% 41.3M 7s
411800K .......... .......... .......... .......... .......... 81% 41.9M 7s
411850K .......... .......... .......... .......... .......... 81% 38.6M 7s
411900K .......... .......... .......... .......... .......... 81% 38.4M 7s
411950K .......... .......... .......... .......... .......... 81% 37.2M 7s
412000K .......... .......... .......... .......... .......... 81% 17.3M 7s
412050K .......... .......... .......... .......... .......... 81% 48.2M 7s
412100K .......... .......... .......... .......... .......... 81% 76.3M 7s
412150K .......... .......... .......... .......... .......... 81%  488M 7s
412200K .......... .......... .......... .......... .......... 81% 30.5M 7s
412250K .......... .......... .......... .......... .......... 81%  123M 7s
412300K .......... .......... .......... .......... .......... 81% 33.4M 7s
412350K .......... .......... .......... .......... .......... 81% 69.4M 7s
412400K .......... .......... .......... .......... .......... 81% 70.2M 7s
412450K .......... .......... .......... .......... .......... 81% 29.6M 7s
412500K .......... .......... .......... .......... .......... 81% 38.4M 7s
412550K .......... .......... .......... .......... .......... 81% 29.6M 7s
412600K .......... .......... .......... .......... .......... 81% 34.3M 7s
412650K .......... .......... .......... .......... .......... 81% 42.6M 7s
412700K .......... .......... .......... .......... .......... 81% 21.2M 7s
412750K .......... .......... .......... .......... .......... 81% 38.0M 7s
412800K .......... .......... .......... .......... .......... 81% 31.3M 7s
412850K .......... .......... .......... .......... .......... 81% 36.7M 7s
412900K .......... .......... .......... .......... .......... 81% 21.2M 7s
412950K .......... .......... .......... .......... .......... 82% 21.6M 7s
413000K .......... .......... .......... .......... .......... 82% 42.7M 7s
413050K .......... .......... .......... .......... .......... 82% 43.1M 7s
413100K .......... .......... .......... .......... .......... 82% 19.0M 7s
413150K .......... .......... .......... .......... .......... 82% 24.5M 7s
413200K .......... .......... .......... .......... .......... 82% 38.1M 7s
413250K .......... .......... .......... .......... .......... 82% 32.1M 7s
413300K .......... .......... .......... .......... .......... 82% 29.4M 7s
413350K .......... .......... .......... .......... .......... 82% 27.2M 7s
413400K .......... .......... .......... .......... .......... 82% 41.3M 7s
413450K .......... .......... .......... .......... .......... 82% 24.3M 7s
413500K .......... .......... .......... .......... .......... 82% 37.6M 7s
413550K .......... .......... .......... .......... .......... 82% 45.1M 7s
413600K .......... .......... .......... .......... .......... 82% 40.5M 7s
413650K .......... .......... .......... .......... .......... 82% 63.5M 7s
413700K .......... .......... .......... .......... .......... 82% 64.2M 7s
413750K .......... .......... .......... .......... .......... 82% 52.9M 7s
413800K .......... .......... .......... .......... .......... 82% 23.4M 7s
413850K .......... .......... .......... .......... .......... 82%  370M 7s
413900K .......... .......... .......... .......... .......... 82% 39.7M 7s
413950K .......... .......... .......... .......... .......... 82% 96.3M 7s
414000K .......... .......... .......... .......... .......... 82% 40.1M 7s
414050K .......... .......... .......... .......... .......... 82% 54.9M 7s
414100K .......... .......... .......... .......... .......... 82% 80.8M 7s
414150K .......... .......... .......... .......... .......... 82% 32.0M 7s
414200K .......... .......... .......... .......... .......... 82% 38.5M 7s
414250K .......... .......... .......... .......... .......... 82% 42.9M 7s
414300K .......... .......... .......... .......... .......... 82% 42.4M 7s
414350K .......... .......... .......... .......... .......... 82% 35.1M 7s
414400K .......... .......... .......... .......... .......... 82% 38.4M 7s
414450K .......... .......... .......... .......... .......... 82% 37.8M 7s
414500K .......... .......... .......... .......... .......... 82% 48.0M 7s
414550K .......... .......... .......... .......... .......... 82% 38.6M 7s
414600K .......... .......... .......... .......... .......... 82% 32.2M 7s
414650K .......... .......... .......... .......... .......... 82% 54.2M 7s
414700K .......... .......... .......... .......... .......... 82% 38.5M 7s
414750K .......... .......... .......... .......... .......... 82% 39.1M 7s
414800K .......... .......... .......... .......... .......... 82% 42.5M 7s
414850K .......... .......... .......... .......... .......... 82% 39.1M 7s
414900K .......... .......... .......... .......... .......... 82% 42.1M 7s
414950K .......... .......... .......... .......... .......... 82% 39.3M 7s
415000K .......... .......... .......... .......... .......... 82% 46.8M 7s
415050K .......... .......... .......... .......... .......... 82% 35.5M 7s
415100K .......... .......... .......... .......... .......... 82% 35.0M 7s
415150K .......... .......... .......... .......... .......... 82% 48.3M 7s
415200K .......... .......... .......... .......... .......... 82% 35.0M 7s
415250K .......... .......... .......... .......... .......... 82% 42.9M 7s
415300K .......... .......... .......... .......... .......... 82% 34.7M 7s
415350K .......... .......... .......... .......... .......... 82% 47.3M 7s
415400K .......... .......... .......... .......... .......... 82% 40.8M 7s
415450K .......... .......... .......... .......... .......... 82% 36.9M 7s
415500K .......... .......... .......... .......... .......... 82% 49.3M 6s
415550K .......... .......... .......... .......... .......... 82% 42.7M 6s
415600K .......... .......... .......... .......... .......... 82% 47.1M 6s
415650K .......... .......... .......... .......... .......... 82% 38.2M 6s
415700K .......... .......... .......... .......... .......... 82% 8.53M 6s
415750K .......... .......... .......... .......... .......... 82%  351M 6s
415800K .......... .......... .......... .......... .......... 82%  397M 6s
415850K .......... .......... .......... .......... .......... 82%  410M 6s
415900K .......... .......... .......... .......... .......... 82% 21.5M 6s
415950K .......... .......... .......... .......... .......... 82%  313M 6s
416000K .......... .......... .......... .......... .......... 82%  470M 6s
416050K .......... .......... .......... .......... .......... 82% 34.3M 6s
416100K .......... .......... .......... .......... .......... 82% 24.8M 6s
416150K .......... .......... .......... .......... .......... 82%  233M 6s
416200K .......... .......... .......... .......... .......... 82% 67.4M 6s
416250K .......... .......... .......... .......... .......... 82% 23.4M 6s
416300K .......... .......... .......... .......... .......... 82% 23.3M 6s
416350K .......... .......... .......... .......... .......... 82% 20.4M 6s
416400K .......... .......... .......... .......... .......... 82% 34.7M 6s
416450K .......... .......... .......... .......... .......... 82% 21.0M 6s
416500K .......... .......... .......... .......... .......... 82% 29.3M 6s
416550K .......... .......... .......... .......... .......... 82% 22.8M 6s
416600K .......... .......... .......... .......... .......... 82% 23.9M 6s
416650K .......... .......... .......... .......... .......... 82% 27.5M 6s
416700K .......... .......... .......... .......... .......... 82% 22.7M 6s
416750K .......... .......... .......... .......... .......... 82% 25.8M 6s
416800K .......... .......... .......... .......... .......... 82% 24.2M 6s
416850K .......... .......... .......... .......... .......... 82% 19.4M 6s
416900K .......... .......... .......... .......... .......... 82% 42.8M 6s
416950K .......... .......... .......... .......... .......... 82% 19.3M 6s
417000K .......... .......... .......... .......... .......... 82% 21.4M 6s
417050K .......... .......... .......... .......... .......... 82% 14.9M 6s
417100K .......... .......... .......... .......... .......... 82% 11.7M 6s
417150K .......... .......... .......... .......... .......... 82% 22.6M 6s
417200K .......... .......... .......... .......... .......... 82% 24.2M 6s
417250K .......... .......... .......... .......... .......... 82% 21.7M 6s
417300K .......... .......... .......... .......... .......... 82% 17.2M 6s
417350K .......... .......... .......... .......... .......... 82% 17.9M 6s
417400K .......... .......... .......... .......... .......... 82%  100M 6s
417450K .......... .......... .......... .......... .......... 82% 17.5M 6s
417500K .......... .......... .......... .......... .......... 82% 20.2M 6s
417550K .......... .......... .......... .......... .......... 82% 18.3M 6s
417600K .......... .......... .......... .......... .......... 82% 16.8M 6s
417650K .......... .......... .......... .......... .......... 82% 21.3M 6s
417700K .......... .......... .......... .......... .......... 82% 15.0M 6s
417750K .......... .......... .......... .......... .......... 82% 20.4M 6s
417800K .......... .......... .......... .......... .......... 82% 20.4M 6s
417850K .......... .......... .......... .......... .......... 82% 20.3M 6s
417900K .......... .......... .......... .......... .......... 82% 20.2M 6s
417950K .......... .......... .......... .......... .......... 83% 16.9M 6s
418000K .......... .......... .......... .......... .......... 83% 16.1M 6s
418050K .......... .......... .......... .......... .......... 83% 20.4M 6s
418100K .......... .......... .......... .......... .......... 83% 13.8M 6s
418150K .......... .......... .......... .......... .......... 83% 14.6M 6s
418200K .......... .......... .......... .......... .......... 83% 18.7M 6s
418250K .......... .......... .......... .......... .......... 83% 39.2M 6s
418300K .......... .......... .......... .......... .......... 83% 24.1M 6s
418350K .......... .......... .......... .......... .......... 83% 20.2M 6s
418400K .......... .......... .......... .......... .......... 83% 19.4M 6s
418450K .......... .......... .......... .......... .......... 83% 16.4M 6s
418500K .......... .......... .......... .......... .......... 83% 19.9M 6s
418550K .......... .......... .......... .......... .......... 83% 24.3M 6s
418600K .......... .......... .......... .......... .......... 83% 18.5M 6s
418650K .......... .......... .......... .......... .......... 83% 22.8M 6s
418700K .......... .......... .......... .......... .......... 83% 20.1M 6s
418750K .......... .......... .......... .......... .......... 83% 25.8M 6s
418800K .......... .......... .......... .......... .......... 83% 19.9M 6s
418850K .......... .......... .......... .......... .......... 83% 21.4M 6s
418900K .......... .......... .......... .......... .......... 83% 24.1M 6s
418950K .......... .......... .......... .......... .......... 83% 19.3M 6s
419000K .......... .......... .......... .......... .......... 83% 32.1M 6s
419050K .......... .......... .......... .......... .......... 83% 25.4M 6s
419100K .......... .......... .......... .......... .......... 83% 13.3M 6s
419150K .......... .......... .......... .......... .......... 83%  407M 6s
419200K .......... .......... .......... .......... .......... 83% 16.2M 6s
419250K .......... .......... .......... .......... .......... 83% 44.6M 6s
419300K .......... .......... .......... .......... .......... 83% 34.9M 6s
419350K .......... .......... .......... .......... .......... 83% 20.0M 6s
419400K .......... .......... .......... .......... .......... 83% 30.4M 6s
419450K .......... .......... .......... .......... .......... 83% 27.2M 6s
419500K .......... .......... .......... .......... .......... 83% 25.9M 6s
419550K .......... .......... .......... .......... .......... 83% 38.3M 6s
419600K .......... .......... .......... .......... .......... 83% 23.0M 6s
419650K .......... .......... .......... .......... .......... 83% 31.5M 6s
419700K .......... .......... .......... .......... .......... 83% 22.4M 6s
419750K .......... .......... .......... .......... .......... 83% 32.0M 6s
419800K .......... .......... .......... .......... .......... 83% 27.2M 6s
419850K .......... .......... .......... .......... .......... 83% 27.6M 6s
419900K .......... .......... .......... .......... .......... 83% 32.2M 6s
419950K .......... .......... .......... .......... .......... 83% 27.5M 6s
420000K .......... .......... .......... .......... .......... 83% 27.6M 6s
420050K .......... .......... .......... .......... .......... 83% 42.7M 6s
420100K .......... .......... .......... .......... .......... 83% 24.0M 6s
420150K .......... .......... .......... .......... .......... 83% 27.6M 6s
420200K .......... .......... .......... .......... .......... 83% 29.6M 6s
420250K .......... .......... .......... .......... .......... 83% 29.3M 6s
420300K .......... .......... .......... .......... .......... 83% 35.6M 6s
420350K .......... .......... .......... .......... .......... 83% 19.3M 6s
420400K .......... .......... .......... .......... .......... 83% 15.4M 6s
420450K .......... .......... .......... .......... .......... 83% 12.8M 6s
420500K .......... .......... .......... .......... .......... 83%  452M 6s
420550K .......... .......... .......... .......... .......... 83%  414M 6s
420600K .......... .......... .......... .......... .......... 83% 20.8M 6s
420650K .......... .......... .......... .......... .......... 83% 45.5M 6s
420700K .......... .......... .......... .......... .......... 83% 25.7M 6s
420750K .......... .......... .......... .......... .......... 83% 34.7M 6s
420800K .......... .......... .......... .......... .......... 83% 43.7M 6s
420850K .......... .......... .......... .......... .......... 83% 22.7M 6s
420900K .......... .......... .......... .......... .......... 83% 34.9M 6s
420950K .......... .......... .......... .......... .......... 83% 25.7M 6s
421000K .......... .......... .......... .......... .......... 83% 42.8M 6s
421050K .......... .......... .......... .......... .......... 83% 38.5M 6s
421100K .......... .......... .......... .......... .......... 83% 27.6M 6s
421150K .......... .......... .......... .......... .......... 83% 32.2M 6s
421200K .......... .......... .......... .......... .......... 83% 32.0M 6s
421250K .......... .......... .......... .......... .......... 83% 33.0M 6s
421300K .......... .......... .......... .......... .......... 83% 33.7M 6s
421350K .......... .......... .......... .......... .......... 83% 24.0M 6s
421400K .......... .......... .......... .......... .......... 83% 38.0M 6s
421450K .......... .......... .......... .......... .......... 83% 25.8M 6s
421500K .......... .......... .......... .......... .......... 83% 37.0M 6s
421550K .......... .......... .......... .......... .......... 83% 21.2M 6s
421600K .......... .......... .......... .......... .......... 83% 37.3M 6s
421650K .......... .......... .......... .......... .......... 83% 24.8M 6s
421700K .......... .......... .......... .......... .......... 83% 25.6M 6s
421750K .......... .......... .......... .......... .......... 83% 26.7M 6s
421800K .......... .......... .......... .......... .......... 83% 26.6M 6s
421850K .......... .......... .......... .......... .......... 83% 16.4M 6s
421900K .......... .......... .......... .......... .......... 83%  444M 6s
421950K .......... .......... .......... .......... .......... 83% 23.8M 6s
422000K .......... .......... .......... .......... .......... 83%  111M 6s
422050K .......... .......... .......... .......... .......... 83% 23.2M 6s
422100K .......... .......... .......... .......... .......... 83% 88.5M 6s
422150K .......... .......... .......... .......... .......... 83% 38.4M 6s
422200K .......... .......... .......... .......... .......... 83% 25.2M 6s
422250K .......... .......... .......... .......... .......... 83% 38.3M 6s
422300K .......... .......... .......... .......... .......... 83% 42.0M 6s
422350K .......... .......... .......... .......... .......... 83% 24.4M 6s
422400K .......... .......... .......... .......... .......... 83% 34.8M 6s
422450K .......... .......... .......... .......... .......... 83% 24.0M 6s
422500K .......... .......... .......... .......... .......... 83% 37.1M 6s
422550K .......... .......... .......... .......... .......... 83% 34.5M 6s
422600K .......... .......... .......... .......... .......... 83% 26.9M 6s
422650K .......... .......... .......... .......... .......... 83% 32.0M 6s
422700K .......... .......... .......... .......... .......... 83% 41.9M 6s
422750K .......... .......... .......... .......... .......... 83% 29.9M 6s
422800K .......... .......... .......... .......... .......... 83% 34.8M 6s
422850K .......... .......... .......... .......... .......... 83% 37.9M 6s
422900K .......... .......... .......... .......... .......... 83% 33.1M 6s
422950K .......... .......... .......... .......... .......... 83% 29.8M 6s
423000K .......... .......... .......... .......... .......... 84% 43.7M 6s
423050K .......... .......... .......... .......... .......... 84% 31.7M 6s
423100K .......... .......... .......... .......... .......... 84% 30.1M 6s
423150K .......... .......... .......... .......... .......... 84% 46.9M 6s
423200K .......... .......... .......... .......... .......... 84% 30.8M 6s
423250K .......... .......... .......... .......... .......... 84% 36.7M 6s
423300K .......... .......... .......... .......... .......... 84% 63.0M 6s
423350K .......... .......... .......... .......... .......... 84% 21.8M 6s
423400K .......... .......... .......... .......... .......... 84%  452M 6s
423450K .......... .......... .......... .......... .......... 84% 49.9M 6s
423500K .......... .......... .......... .......... .......... 84% 57.4M 6s
423550K .......... .......... .......... .......... .......... 84%  498M 6s
423600K .......... .......... .......... .......... .......... 84% 70.0M 6s
423650K .......... .......... .......... .......... .......... 84% 54.0M 6s
423700K .......... .......... .......... .......... .......... 84% 54.8M 6s
423750K .......... .......... .......... .......... .......... 84% 80.3M 6s
423800K .......... .......... .......... .......... .......... 84% 46.1M 6s
423850K .......... .......... .......... .......... .......... 84% 41.0M 6s
423900K .......... .......... .......... .......... .......... 84% 51.5M 6s
423950K .......... .......... .......... .......... .......... 84% 37.3M 6s
424000K .......... .......... .......... .......... .......... 84% 46.1M 6s
424050K .......... .......... .......... .......... .......... 84% 37.9M 6s
424100K .......... .......... .......... .......... .......... 84% 53.5M 6s
424150K .......... .......... .......... .......... .......... 84% 47.5M 6s
424200K .......... .......... .......... .......... .......... 84% 31.9M 6s
424250K .......... .......... .......... .......... .......... 84% 52.8M 6s
424300K .......... .......... .......... .......... .......... 84% 54.4M 6s
424350K .......... .......... .......... .......... .......... 84% 37.3M 6s
424400K .......... .......... .......... .......... .......... 84% 41.5M 6s
424450K .......... .......... .......... .......... .......... 84% 39.0M 6s
424500K .......... .......... .......... .......... .......... 84% 54.6M 6s
424550K .......... .......... .......... .......... .......... 84% 42.2M 6s
424600K .......... .......... .......... .......... .......... 84% 38.5M 6s
424650K .......... .......... .......... .......... .......... 84% 48.7M 6s
424700K .......... .......... .......... .......... .......... 84% 42.6M 6s
424750K .......... .......... .......... .......... .......... 84% 32.6M 6s
424800K .......... .......... .......... .......... .......... 84% 55.3M 6s
424850K .......... .......... .......... .......... .......... 84% 34.4M 6s
424900K .......... .......... .......... .......... .......... 84% 52.6M 6s
424950K .......... .......... .......... .......... .......... 84% 45.7M 6s
425000K .......... .......... .......... .......... .......... 84% 36.1M 6s
425050K .......... .......... .......... .......... .......... 84% 36.3M 6s
425100K .......... .......... .......... .......... .......... 84% 42.2M 6s
425150K .......... .......... .......... .......... .......... 84% 43.7M 6s
425200K .......... .......... .......... .......... .......... 84% 32.8M 6s
425250K .......... .......... .......... .......... .......... 84% 37.5M 6s
425300K .......... .......... .......... .......... .......... 84% 14.4M 6s
425350K .......... .......... .......... .......... .......... 84% 15.1M 6s
425400K .......... .......... .......... .......... .......... 84%  397M 6s
425450K .......... .......... .......... .......... .......... 84%  400M 6s
425500K .......... .......... .......... .......... .......... 84% 18.5M 6s
425550K .......... .......... .......... .......... .......... 84%  112M 6s
425600K .......... .......... .......... .......... .......... 84% 32.3M 6s
425650K .......... .......... .......... .......... .......... 84% 29.3M 6s
425700K .......... .......... .......... .......... .......... 84% 27.4M 6s
425750K .......... .......... .......... .......... .......... 84% 35.0M 6s
425800K .......... .......... .......... .......... .......... 84% 21.4M 6s
425850K .......... .......... .......... .......... .......... 84% 21.0M 6s
425900K .......... .......... .......... .......... .......... 84% 25.6M 6s
425950K .......... .......... .......... .......... .......... 84% 25.7M 6s
426000K .......... .......... .......... .......... .......... 84% 22.8M 6s
426050K .......... .......... .......... .......... .......... 84% 43.0M 6s
426100K .......... .......... .......... .......... .......... 84% 18.5M 6s
426150K .......... .......... .......... .......... .......... 84% 27.7M 6s
426200K .......... .......... .......... .......... .......... 84% 25.5M 6s
426250K .......... .......... .......... .......... .......... 84% 24.1M 6s
426300K .......... .......... .......... .......... .......... 84% 22.8M 6s
426350K .......... .......... .......... .......... .......... 84% 20.4M 6s
426400K .......... .......... .......... .......... .......... 84% 24.1M 6s
426450K .......... .......... .......... .......... .......... 84% 9.82M 6s
426500K .......... .......... .......... .......... .......... 84% 12.2M 6s
426550K .......... .......... .......... .......... .......... 84%  461M 6s
426600K .......... .......... .......... .......... .......... 84% 16.3M 6s
426650K .......... .......... .......... .......... .......... 84% 29.0M 6s
426700K .......... .......... .......... .......... .......... 84% 20.3M 6s
426750K .......... .......... .......... .......... .......... 84% 22.7M 6s
426800K .......... .......... .......... .......... .......... 84% 24.1M 6s
426850K .......... .......... .......... .......... .......... 84% 20.3M 6s
426900K .......... .......... .......... .......... .......... 84% 25.6M 6s
426950K .......... .......... .......... .......... .......... 84% 19.4M 6s
427000K .......... .......... .......... .......... .......... 84% 31.7M 6s
427050K .......... .......... .......... .......... .......... 84% 21.5M 6s
427100K .......... .......... .......... .......... .......... 84% 19.4M 6s
427150K .......... .......... .......... .......... .......... 84% 22.8M 6s
427200K .......... .......... .......... .......... .......... 84% 27.4M 6s
427250K .......... .......... .......... .......... .......... 84% 22.4M 6s
427300K .......... .......... .......... .......... .......... 84% 22.1M 6s
427350K .......... .......... .......... .......... .......... 84% 23.5M 6s
427400K .......... .......... .......... .......... .......... 84% 17.2M 6s
427450K .......... .......... .......... .......... .......... 84% 11.4M 6s
427500K .......... .......... .......... .......... .......... 84% 20.2M 6s
427550K .......... .......... .......... .......... .......... 84% 9.04M 6s
427600K .......... .......... .......... .......... .......... 84%  461M 6s
427650K .......... .......... .......... .......... .......... 84% 20.7M 6s
427700K .......... .......... .......... .......... .......... 84% 29.0M 6s
427750K .......... .......... .......... .......... .......... 84% 22.8M 6s
427800K .......... .......... .......... .......... .......... 84% 19.3M 6s
427850K .......... .......... .......... .......... .......... 84% 13.9M 6s
427900K .......... .......... .......... .......... .......... 84% 18.5M 6s
427950K .......... .......... .......... .......... .......... 84% 21.4M 5s
428000K .......... .......... .......... .......... .......... 84% 18.0M 5s
428050K .......... .......... .......... .......... .......... 85% 22.7M 5s
428100K .......... .......... .......... .......... .......... 85% 15.5M 5s
428150K .......... .......... .......... .......... .......... 85% 17.6M 5s
428200K .......... .......... .......... .......... .......... 85% 13.4M 5s
428250K .......... .......... .......... .......... .......... 85% 17.6M 5s
428300K .......... .......... .......... .......... .......... 85% 20.4M 5s
428350K .......... .......... .......... .......... .......... 85% 12.1M 5s
428400K .......... .......... .......... .......... .......... 85% 12.6M 5s
428450K .......... .......... .......... .......... .......... 85% 81.1M 5s
428500K .......... .......... .......... .......... .......... 85% 19.4M 5s
428550K .......... .......... .......... .......... .......... 85% 16.4M 5s
428600K .......... .......... .......... .......... .......... 85% 13.1M 5s
428650K .......... .......... .......... .......... .......... 85% 14.3M 5s
428700K .......... .......... .......... .......... .......... 85% 13.4M 5s
428750K .......... .......... .......... .......... .......... 85% 13.8M 5s
428800K .......... .......... .......... .......... .......... 85% 13.8M 5s
428850K .......... .......... .......... .......... .......... 85% 16.8M 5s
428900K .......... .......... .......... .......... .......... 85% 13.9M 5s
428950K .......... .......... .......... .......... .......... 85% 12.9M 5s
429000K .......... .......... .......... .......... .......... 85% 15.5M 5s
429050K .......... .......... .......... .......... .......... 85% 19.4M 5s
429100K .......... .......... .......... .......... .......... 85% 14.9M 5s
429150K .......... .......... .......... .......... .......... 85% 22.6M 5s
429200K .......... .......... .......... .......... .......... 85% 10.7M 5s
429250K .......... .......... .......... .......... .......... 85% 16.4M 5s
429300K .......... .......... .......... .......... .......... 85% 58.5M 5s
429350K .......... .......... .......... .......... .......... 85% 11.0M 5s
429400K .......... .......... .......... .......... .......... 85% 18.4M 5s
429450K .......... .......... .......... .......... .......... 85% 13.8M 5s
429500K .......... .......... .......... .......... .......... 85% 17.6M 5s
429550K .......... .......... .......... .......... .......... 85% 16.3M 5s
429600K .......... .......... .......... .......... .......... 85% 11.8M 5s
429650K .......... .......... .......... .......... .......... 85% 14.7M 5s
429700K .......... .......... .......... .......... .......... 85% 12.9M 5s
429750K .......... .......... .......... .......... .......... 85% 11.8M 5s
429800K .......... .......... .......... .......... .......... 85% 16.2M 5s
429850K .......... .......... .......... .......... .......... 85% 8.83M 5s
429900K .......... .......... .......... .......... .......... 85% 11.0M 5s
429950K .......... .......... .......... .......... .......... 85% 14.6M 5s
430000K .......... .......... .......... .......... .......... 85% 16.1M 5s
430050K .......... .......... .......... .......... .......... 85% 18.1M 5s
430100K .......... .......... .......... .......... .......... 85% 28.3M 5s
430150K .......... .......... .......... .......... .......... 85% 24.2M 5s
430200K .......... .......... .......... .......... .......... 85% 20.3M 5s
430250K .......... .......... .......... .......... .......... 85% 27.5M 5s
430300K .......... .......... .......... .......... .......... 85% 24.1M 5s
430350K .......... .......... .......... .......... .......... 85% 27.3M 5s
430400K .......... .......... .......... .......... .......... 85% 21.6M 5s
430450K .......... .......... .......... .......... .......... 85% 22.9M 5s
430500K .......... .......... .......... .......... .......... 85% 42.9M 5s
430550K .......... .......... .......... .......... .......... 85% 21.4M 5s
430600K .......... .......... .......... .......... .......... 85% 21.5M 5s
430650K .......... .......... .......... .......... .......... 85% 24.2M 5s
430700K .......... .......... .......... .......... .......... 85% 24.1M 5s
430750K .......... .......... .......... .......... .......... 85% 38.7M 5s
430800K .......... .......... .......... .......... .......... 85% 22.3M 5s
430850K .......... .......... .......... .......... .......... 85% 23.1M 5s
430900K .......... .......... .......... .......... .......... 85% 25.5M 5s
430950K .......... .......... .......... .......... .......... 85% 24.4M 5s
431000K .......... .......... .......... .......... .......... 85% 41.8M 5s
431050K .......... .......... .......... .......... .......... 85% 17.2M 5s
431100K .......... .......... .......... .......... .......... 85% 26.8M 5s
431150K .......... .......... .......... .......... .......... 85% 53.7M 5s
431200K .......... .......... .......... .......... .......... 85%  339M 5s
431250K .......... .......... .......... .......... .......... 85% 20.5M 5s
431300K .......... .......... .......... .......... .......... 85% 31.9M 5s
431350K .......... .......... .......... .......... .......... 85% 84.5M 5s
431400K .......... .......... .......... .......... .......... 85% 19.8M 5s
431450K .......... .......... .......... .......... .......... 85% 25.6M 5s
431500K .......... .......... .......... .......... .......... 85% 22.8M 5s
431550K .......... .......... .......... .......... .......... 85% 27.6M 5s
431600K .......... .......... .......... .......... .......... 85% 20.4M 5s
431650K .......... .......... .......... .......... .......... 85% 22.8M 5s
431700K .......... .......... .......... .......... .......... 85% 24.0M 5s
431750K .......... .......... .......... .......... .......... 85% 21.5M 5s
431800K .......... .......... .......... .......... .......... 85% 22.9M 5s
431850K .......... .......... .......... .......... .......... 85% 18.7M 5s
431900K .......... .......... .......... .......... .......... 85% 29.7M 5s
431950K .......... .......... .......... .......... .......... 85% 25.3M 5s
432000K .......... .......... .......... .......... .......... 85% 22.2M 5s
432050K .......... .......... .......... .......... .......... 85% 22.7M 5s
432100K .......... .......... .......... .......... .......... 85% 22.7M 5s
432150K .......... .......... .......... .......... .......... 85% 24.2M 5s
432200K .......... .......... .......... .......... .......... 85% 21.4M 5s
432250K .......... .......... .......... .......... .......... 85% 27.5M 5s
432300K .......... .......... .......... .......... .......... 85% 10.9M 5s
432350K .......... .......... .......... .......... .......... 85%  110M 5s
432400K .......... .......... .......... .......... .......... 85% 41.6M 5s
432450K .......... .......... .......... .......... .......... 85% 14.9M 5s
432500K .......... .......... .......... .......... .......... 85% 25.7M 5s
432550K .......... .......... .......... .......... .......... 85% 35.5M 5s
432600K .......... .......... .......... .......... .......... 85% 14.3M 5s
432650K .......... .......... .......... .......... .......... 85% 22.4M 5s
432700K .......... .......... .......... .......... .......... 85% 19.5M 5s
432750K .......... .......... .......... .......... .......... 85% 19.3M 5s
432800K .......... .......... .......... .......... .......... 85% 20.3M 5s
432850K .......... .......... .......... .......... .......... 85% 14.9M 5s
432900K .......... .......... .......... .......... .......... 85% 15.5M 5s
432950K .......... .......... .......... .......... .......... 85% 13.8M 5s
433000K .......... .......... .......... .......... .......... 85% 16.0M 5s
433050K .......... .......... .......... .......... .......... 86% 16.3M 5s
433100K .......... .......... .......... .......... .......... 86% 13.1M 5s
433150K .......... .......... .......... .......... .......... 86% 17.0M 5s
433200K .......... .......... .......... .......... .......... 86% 13.9M 5s
433250K .......... .......... .......... .......... .......... 86% 17.4M 5s
433300K .......... .......... .......... .......... .......... 86% 9.96M 5s
433350K .......... .......... .......... .......... .......... 86% 10.4M 5s
433400K .......... .......... .......... .......... .......... 86% 35.6M 5s
433450K .......... .......... .......... .......... .......... 86% 23.4M 5s
433500K .......... .......... .......... .......... .......... 86% 28.3M 5s
433550K .......... .......... .......... .......... .......... 86% 23.6M 5s
433600K .......... .......... .......... .......... .......... 86% 24.8M 5s
433650K .......... .......... .......... .......... .......... 86% 29.5M 5s
433700K .......... .......... .......... .......... .......... 86% 23.5M 5s
433750K .......... .......... .......... .......... .......... 86% 26.9M 5s
433800K .......... .......... .......... .......... .......... 86% 25.8M 5s
433850K .......... .......... .......... .......... .......... 86% 27.6M 5s
433900K .......... .......... .......... .......... .......... 86% 29.6M 5s
433950K .......... .......... .......... .......... .......... 86% 21.4M 5s
434000K .......... .......... .......... .......... .......... 86% 24.2M 5s
434050K .......... .......... .......... .......... .......... 86% 25.2M 5s
434100K .......... .......... .......... .......... .......... 86% 19.8M 5s
434150K .......... .......... .......... .......... .......... 86% 45.6M 5s
434200K .......... .......... .......... .......... .......... 86% 19.8M 5s
434250K .......... .......... .......... .......... .......... 86% 11.7M 5s
434300K .......... .......... .......... .......... .......... 86% 47.8M 5s
434350K .......... .......... .......... .......... .......... 86% 14.4M 5s
434400K .......... .......... .......... .......... .......... 86% 17.4M 5s
434450K .......... .......... .......... .......... .......... 86% 13.2M 5s
434500K .......... .......... .......... .......... .......... 86% 21.1M 5s
434550K .......... .......... .......... .......... .......... 86% 20.2M 5s
434600K .......... .......... .......... .......... .......... 86% 16.8M 5s
434650K .......... .......... .......... .......... .......... 86% 23.0M 5s
434700K .......... .......... .......... .......... .......... 86% 17.6M 5s
434750K .......... .......... .......... .......... .......... 86% 22.4M 5s
434800K .......... .......... .......... .......... .......... 86% 21.8M 5s
434850K .......... .......... .......... .......... .......... 86% 21.4M 5s
434900K .......... .......... .......... .......... .......... 86% 21.5M 5s
434950K .......... .......... .......... .......... .......... 86% 17.6M 5s
435000K .......... .......... .......... .......... .......... 86% 20.4M 5s
435050K .......... .......... .......... .......... .......... 86% 28.8M 5s
435100K .......... .......... .......... .......... .......... 86% 23.1M 5s
435150K .......... .......... .......... .......... .......... 86% 15.2M 5s
435200K .......... .......... .......... .......... .......... 86%  356M 5s
435250K .......... .......... .......... .......... .......... 86% 27.6M 5s
435300K .......... .......... .......... .......... .......... 86% 47.8M 5s
435350K .......... .......... .......... .......... .......... 86% 25.8M 5s
435400K .......... .......... .......... .......... .......... 86% 26.5M 5s
435450K .......... .......... .......... .......... .......... 86% 20.4M 5s
435500K .......... .......... .......... .......... .......... 86% 27.6M 5s
435550K .......... .......... .......... .......... .......... 86% 25.5M 5s
435600K .......... .......... .......... .......... .......... 86% 22.7M 5s
435650K .......... .......... .......... .......... .......... 86% 27.6M 5s
435700K .......... .......... .......... .......... .......... 86% 24.1M 5s
435750K .......... .......... .......... .......... .......... 86% 22.7M 5s
435800K .......... .......... .......... .......... .......... 86% 26.0M 5s
435850K .......... .......... .......... .......... .......... 86% 22.7M 5s
435900K .......... .......... .......... .......... .......... 86% 22.7M 5s
435950K .......... .......... .......... .......... .......... 86% 23.9M 5s
436000K .......... .......... .......... .......... .......... 86% 27.8M 5s
436050K .......... .......... .......... .......... .......... 86% 26.9M 5s
436100K .......... .......... .......... .......... .......... 86% 17.9M 5s
436150K .......... .......... .......... .......... .......... 86% 22.5M 5s
436200K .......... .......... .......... .......... .......... 86% 11.1M 5s
436250K .......... .......... .......... .......... .......... 86% 22.9M 5s
436300K .......... .......... .......... .......... .......... 86% 27.6M 5s
436350K .......... .......... .......... .......... .......... 86% 25.8M 5s
436400K .......... .......... .......... .......... .......... 86% 18.8M 5s
436450K .......... .......... .......... .......... .......... 86%  160M 5s
436500K .......... .......... .......... .......... .......... 86% 28.0M 5s
436550K .......... .......... .......... .......... .......... 86% 29.0M 5s
436600K .......... .......... .......... .......... .......... 86% 25.7M 5s
436650K .......... .......... .......... .......... .......... 86% 38.6M 5s
436700K .......... .......... .......... .......... .......... 86% 20.3M 5s
436750K .......... .......... .......... .......... .......... 86% 48.3M 5s
436800K .......... .......... .......... .......... .......... 86% 29.4M 5s
436850K .......... .......... .......... .......... .......... 86% 25.9M 5s
436900K .......... .......... .......... .......... .......... 86% 27.7M 5s
436950K .......... .......... .......... .......... .......... 86% 29.5M 5s
437000K .......... .......... .......... .......... .......... 86% 32.6M 5s
437050K .......... .......... .......... .......... .......... 86% 21.4M 5s
437100K .......... .......... .......... .......... .......... 86% 43.0M 5s
437150K .......... .......... .......... .......... .......... 86% 24.1M 5s
437200K .......... .......... .......... .......... .......... 86% 25.8M 5s
437250K .......... .......... .......... .......... .......... 86% 27.6M 5s
437300K .......... .......... .......... .......... .......... 86% 41.7M 5s
437350K .......... .......... .......... .......... .......... 86% 22.6M 5s
437400K .......... .......... .......... .......... .......... 86% 25.0M 5s
437450K .......... .......... .......... .......... .......... 86% 26.2M 5s
437500K .......... .......... .......... .......... .......... 86% 23.8M 5s
437550K .......... .......... .......... .......... .......... 86% 30.1M 5s
437600K .......... .......... .......... .......... .......... 86% 24.1M 5s
437650K .......... .......... .......... .......... .......... 86% 28.4M 5s
437700K .......... .......... .......... .......... .......... 86% 17.4M 5s
437750K .......... .......... .......... .......... .......... 86% 27.9M 5s
437800K .......... .......... .......... .......... .......... 86% 11.5M 5s
437850K .......... .......... .......... .......... .......... 86%  414M 5s
437900K .......... .......... .......... .......... .......... 86% 44.5M 5s
437950K .......... .......... .......... .......... .......... 86% 25.5M 5s
438000K .......... .......... .......... .......... .......... 86% 22.0M 5s
438050K .......... .......... .......... .......... .......... 86% 44.6M 5s
438100K .......... .......... .......... .......... .......... 87% 21.3M 5s
438150K .......... .......... .......... .......... .......... 87% 26.7M 5s
438200K .......... .......... .......... .......... .......... 87% 25.5M 5s
438250K .......... .......... .......... .......... .......... 87% 15.3M 5s
438300K .......... .......... .......... .......... .......... 87% 42.1M 5s
438350K .......... .......... .......... .......... .......... 87% 17.9M 5s
438400K .......... .......... .......... .......... .......... 87% 25.1M 5s
438450K .......... .......... .......... .......... .......... 87% 20.8M 5s
438500K .......... .......... .......... .......... .......... 87% 20.3M 5s
438550K .......... .......... .......... .......... .......... 87% 22.3M 5s
438600K .......... .......... .......... .......... .......... 87% 23.9M 5s
438650K .......... .......... .......... .......... .......... 87% 20.2M 5s
438700K .......... .......... .......... .......... .......... 87% 24.7M 5s
438750K .......... .......... .......... .......... .......... 87% 25.3M 5s
438800K .......... .......... .......... .......... .......... 87% 23.9M 5s
438850K .......... .......... .......... .......... .......... 87% 12.1M 5s
438900K .......... .......... .......... .......... .......... 87% 11.8M 5s
438950K .......... .......... .......... .......... .......... 87% 9.67M 5s
439000K .......... .......... .......... .......... .......... 87% 37.9M 5s
439050K .......... .......... .......... .......... .......... 87% 39.1M 5s
439100K .......... .......... .......... .......... .......... 87% 51.1M 5s
439150K .......... .......... .......... .......... .......... 87% 21.6M 5s
439200K .......... .......... .......... .......... .......... 87% 18.8M 5s
439250K .......... .......... .......... .......... .......... 87% 29.7M 5s
439300K .......... .......... .......... .......... .......... 87% 25.7M 5s
439350K .......... .......... .......... .......... .......... 87% 21.2M 5s
439400K .......... .......... .......... .......... .......... 87% 21.5M 5s
439450K .......... .......... .......... .......... .......... 87% 25.8M 5s
439500K .......... .......... .......... .......... .......... 87% 22.9M 5s
439550K .......... .......... .......... .......... .......... 87% 23.8M 5s
439600K .......... .......... .......... .......... .......... 87% 21.8M 5s
439650K .......... .......... .......... .......... .......... 87% 16.6M 5s
439700K .......... .......... .......... .......... .......... 87% 19.5M 5s
439750K .......... .......... .......... .......... .......... 87% 17.6M 5s
439800K .......... .......... .......... .......... .......... 87% 20.3M 5s
439850K .......... .......... .......... .......... .......... 87% 18.4M 5s
439900K .......... .......... .......... .......... .......... 87% 14.3M 5s
439950K .......... .......... .......... .......... .......... 87% 12.1M 5s
440000K .......... .......... .......... .......... .......... 87% 15.5M 5s
440050K .......... .......... .......... .......... .......... 87% 18.5M 5s
440100K .......... .......... .......... .......... .......... 87% 14.9M 5s
440150K .......... .......... .......... .......... .......... 87% 15.4M 5s
440200K .......... .......... .......... .......... .......... 87% 16.0M 5s
440250K .......... .......... .......... .......... .......... 87% 18.6M 5s
440300K .......... .......... .......... .......... .......... 87% 16.5M 5s
440350K .......... .......... .......... .......... .......... 87% 38.1M 5s
440400K .......... .......... .......... .......... .......... 87% 29.5M 5s
440450K .......... .......... .......... .......... .......... 87% 19.1M 5s
440500K .......... .......... .......... .......... .......... 87% 23.9M 5s
440550K .......... .......... .......... .......... .......... 87% 23.3M 5s
440600K .......... .......... .......... .......... .......... 87% 27.7M 5s
440650K .......... .......... .......... .......... .......... 87% 18.5M 5s
440700K .......... .......... .......... .......... .......... 87%  328M 5s
440750K .......... .......... .......... .......... .......... 87% 42.6M 5s
440800K .......... .......... .......... .......... .......... 87% 18.0M 5s
440850K .......... .......... .......... .......... .......... 87%  379M 5s
440900K .......... .......... .......... .......... .......... 87% 29.0M 5s
440950K .......... .......... .......... .......... .......... 87% 29.0M 5s
441000K .......... .......... .......... .......... .......... 87% 21.5M 4s
441050K .......... .......... .......... .......... .......... 87% 18.2M 4s
441100K .......... .......... .......... .......... .......... 87% 23.4M 4s
441150K .......... .......... .......... .......... .......... 87% 22.3M 4s
441200K .......... .......... .......... .......... .......... 87% 25.4M 4s
441250K .......... .......... .......... .......... .......... 87% 20.0M 4s
441300K .......... .......... .......... .......... .......... 87% 18.8M 4s
441350K .......... .......... .......... .......... .......... 87% 16.7M 4s
441400K .......... .......... .......... .......... .......... 87% 15.2M 4s
441450K .......... .......... .......... .......... .......... 87% 25.6M 4s
441500K .......... .......... .......... .......... .......... 87% 17.4M 4s
441550K .......... .......... .......... .......... .......... 87% 22.1M 4s
441600K .......... .......... .......... .......... .......... 87% 16.6M 4s
441650K .......... .......... .......... .......... .......... 87% 23.6M 4s
441700K .......... .......... .......... .......... .......... 87% 19.0M 4s
441750K .......... .......... .......... .......... .......... 87% 18.1M 4s
441800K .......... .......... .......... .......... .......... 87% 23.2M 4s
441850K .......... .......... .......... .......... .......... 87% 27.8M 4s
441900K .......... .......... .......... .......... .......... 87% 25.6M 4s
441950K .......... .......... .......... .......... .......... 87% 21.5M 4s
442000K .......... .......... .......... .......... .......... 87% 37.2M 4s
442050K .......... .......... .......... .......... .......... 87% 9.88M 4s
442100K .......... .......... .......... .......... .......... 87%  391M 4s
442150K .......... .......... .......... .......... .......... 87% 48.4M 4s
442200K .......... .......... .......... .......... .......... 87% 13.8M 4s
442250K .......... .......... .......... .......... .......... 87% 97.5M 4s
442300K .......... .......... .......... .......... .......... 87% 29.2M 4s
442350K .......... .......... .......... .......... .......... 87% 20.8M 4s
442400K .......... .......... .......... .......... .......... 87% 34.2M 4s
442450K .......... .......... .......... .......... .......... 87% 14.5M 4s
442500K .......... .......... .......... .......... .......... 87%  503M 4s
442550K .......... .......... .......... .......... .......... 87% 32.9M 4s
442600K .......... .......... .......... .......... .......... 87% 24.5M 4s
442650K .......... .......... .......... .......... .......... 87% 37.2M 4s
442700K .......... .......... .......... .......... .......... 87% 27.5M 4s
442750K .......... .......... .......... .......... .......... 87% 28.9M 4s
442800K .......... .......... .......... .......... .......... 87% 41.5M 4s
442850K .......... .......... .......... .......... .......... 87% 22.6M 4s
442900K .......... .......... .......... .......... .......... 87% 38.0M 4s
442950K .......... .......... .......... .......... .......... 87% 25.6M 4s
443000K .......... .......... .......... .......... .......... 87% 32.8M 4s
443050K .......... .......... .......... .......... .......... 87% 38.4M 4s
443100K .......... .......... .......... .......... .......... 87% 34.6M 4s
443150K .......... .......... .......... .......... .......... 88% 29.9M 4s
443200K .......... .......... .......... .......... .......... 88% 28.8M 4s
443250K .......... .......... .......... .......... .......... 88% 33.4M 4s
443300K .......... .......... .......... .......... .......... 88% 34.9M 4s
443350K .......... .......... .......... .......... .......... 88% 31.1M 4s
443400K .......... .......... .......... .......... .......... 88% 35.1M 4s
443450K .......... .......... .......... .......... .......... 88% 29.8M 4s
443500K .......... .......... .......... .......... .......... 88% 34.0M 4s
443550K .......... .......... .......... .......... .......... 88% 22.5M 4s
443600K .......... .......... .......... .......... .......... 88% 48.6M 4s
443650K .......... .......... .......... .......... .......... 88% 33.5M 4s
443700K .......... .......... .......... .......... .......... 88% 25.9M 4s
443750K .......... .......... .......... .......... .......... 88% 22.0M 4s
443800K .......... .......... .......... .......... .......... 88% 34.5M 4s
443850K .......... .......... .......... .......... .......... 88% 29.4M 4s
443900K .......... .......... .......... .......... .......... 88% 15.0M 4s
443950K .......... .......... .......... .......... .......... 88% 31.6M 4s
444000K .......... .......... .......... .......... .......... 88%  448M 4s
444050K .......... .......... .......... .......... .......... 88% 18.6M 4s
444100K .......... .......... .......... .......... .......... 88%  129M 4s
444150K .......... .......... .......... .......... .......... 88% 16.9M 4s
444200K .......... .......... .......... .......... .......... 88% 26.2M 4s
444250K .......... .......... .......... .......... .......... 88% 22.7M 4s
444300K .......... .......... .......... .......... .......... 88% 25.8M 4s
444350K .......... .......... .......... .......... .......... 88% 16.7M 4s
444400K .......... .......... .......... .......... .......... 88% 29.4M 4s
444450K .......... .......... .......... .......... .......... 88% 17.6M 4s
444500K .......... .......... .......... .......... .......... 88% 21.3M 4s
444550K .......... .......... .......... .......... .......... 88% 21.0M 4s
444600K .......... .......... .......... .......... .......... 88% 19.0M 4s
444650K .......... .......... .......... .......... .......... 88% 24.8M 4s
444700K .......... .......... .......... .......... .......... 88% 16.2M 4s
444750K .......... .......... .......... .......... .......... 88% 25.1M 4s
444800K .......... .......... .......... .......... .......... 88% 22.2M 4s
444850K .......... .......... .......... .......... .......... 88% 19.9M 4s
444900K .......... .......... .......... .......... .......... 88% 26.8M 4s
444950K .......... .......... .......... .......... .......... 88% 16.0M 4s
445000K .......... .......... .......... .......... .......... 88% 30.5M 4s
445050K .......... .......... .......... .......... .......... 88% 11.1M 4s
445100K .......... .......... .......... .......... .......... 88%  341M 4s
445150K .......... .......... .......... .......... .......... 88%  245M 4s
445200K .......... .......... .......... .......... .......... 88% 11.3M 4s
445250K .......... .......... .......... .......... .......... 88% 25.6M 4s
445300K .......... .......... .......... .......... .......... 88%  448M 4s
445350K .......... .......... .......... .......... .......... 88% 18.5M 4s
445400K .......... .......... .......... .......... .......... 88% 25.6M 4s
445450K .......... .......... .......... .......... .......... 88% 27.7M 4s
445500K .......... .......... .......... .......... .......... 88% 35.1M 4s
445550K .......... .......... .......... .......... .......... 88% 29.7M 4s
445600K .......... .......... .......... .......... .......... 88% 25.7M 4s
445650K .......... .......... .......... .......... .......... 88% 35.1M 4s
445700K .......... .......... .......... .......... .......... 88% 24.0M 4s
445750K .......... .......... .......... .......... .......... 88% 21.6M 4s
445800K .......... .......... .......... .......... .......... 88% 39.3M 4s
445850K .......... .......... .......... .......... .......... 88% 19.3M 4s
445900K .......... .......... .......... .......... .......... 88% 24.1M 4s
445950K .......... .......... .......... .......... .......... 88% 25.7M 4s
446000K .......... .......... .......... .......... .......... 88% 24.0M 4s
446050K .......... .......... .......... .......... .......... 88% 33.7M 4s
446100K .......... .......... .......... .......... .......... 88% 20.0M 4s
446150K .......... .......... .......... .......... .......... 88% 27.4M 4s
446200K .......... .......... .......... .......... .......... 88% 25.5M 4s
446250K .......... .......... .......... .......... .......... 88% 23.6M 4s
446300K .......... .......... .......... .......... .......... 88% 19.3M 4s
446350K .......... .......... .......... .......... .......... 88% 13.8M 4s
446400K .......... .......... .......... .......... .......... 88% 11.0M 4s
446450K .......... .......... .......... .......... .......... 88% 10.8M 4s
446500K .......... .......... .......... .......... .......... 88% 12.9M 4s
446550K .......... .......... .......... .......... .......... 88% 27.5M 4s
446600K .......... .......... .......... .......... .......... 88% 21.4M 4s
446650K .......... .......... .......... .......... .......... 88% 50.1M 4s
446700K .......... .......... .......... .......... .......... 88% 22.7M 4s
446750K .......... .......... .......... .......... .......... 88% 31.7M 4s
446800K .......... .......... .......... .......... .......... 88% 25.1M 4s
446850K .......... .......... .......... .......... .......... 88% 29.5M 4s
446900K .......... .......... .......... .......... .......... 88% 41.0M 4s
446950K .......... .......... .......... .......... .......... 88% 20.9M 4s
447000K .......... .......... .......... .......... .......... 88% 20.8M 4s
447050K .......... .......... .......... .......... .......... 88% 48.1M 4s
447100K .......... .......... .......... .......... .......... 88% 31.6M 4s
447150K .......... .......... .......... .......... .......... 88% 22.6M 4s
447200K .......... .......... .......... .......... .......... 88% 22.1M 4s
447250K .......... .......... .......... .......... .......... 88% 48.9M 4s
447300K .......... .......... .......... .......... .......... 88% 20.9M 4s
447350K .......... .......... .......... .......... .......... 88% 24.4M 4s
447400K .......... .......... .......... .......... .......... 88% 21.8M 4s
447450K .......... .......... .......... .......... .......... 88% 18.6M 4s
447500K .......... .......... .......... .......... .......... 88% 15.5M 4s
447550K .......... .......... .......... .......... .......... 88% 22.4M 4s
447600K .......... .......... .......... .......... .......... 88% 19.2M 4s
447650K .......... .......... .......... .......... .......... 88% 18.3M 4s
447700K .......... .......... .......... .......... .......... 88% 15.5M 4s
447750K .......... .......... .......... .......... .......... 88% 19.0M 4s
447800K .......... .......... .......... .......... .......... 88% 16.1M 4s
447850K .......... .......... .......... .......... .......... 88% 9.87M 4s
447900K .......... .......... .......... .......... .......... 88% 13.9M 4s
447950K .......... .......... .......... .......... .......... 88% 8.09M 4s
448000K .......... .......... .......... .......... .......... 88% 8.92M 4s
448050K .......... .......... .......... .......... .......... 88% 12.8M 4s
448100K .......... .......... .......... .......... .......... 88% 10.5M 4s
448150K .......... .......... .......... .......... .......... 88% 9.52M 4s
448200K .......... .......... .......... .......... .......... 89% 11.6M 4s
448250K .......... .......... .......... .......... .......... 89% 9.38M 4s
448300K .......... .......... .......... .......... .......... 89% 12.9M 4s
448350K .......... .......... .......... .......... .......... 89% 10.7M 4s
448400K .......... .......... .......... .......... .......... 89% 16.6M 4s
448450K .......... .......... .......... .......... .......... 89% 15.6M 4s
448500K .......... .......... .......... .......... .......... 89% 27.6M 4s
448550K .......... .......... .......... .......... .......... 89% 29.7M 4s
448600K .......... .......... .......... .......... .......... 89% 38.4M 4s
448650K .......... .......... .......... .......... .......... 89% 20.2M 4s
448700K .......... .......... .......... .......... .......... 89%  356M 4s
448750K .......... .......... .......... .......... .......... 89% 43.6M 4s
448800K .......... .......... .......... .......... .......... 89% 27.3M 4s
448850K .......... .......... .......... .......... .......... 89% 43.1M 4s
448900K .......... .......... .......... .......... .......... 89% 22.7M 4s
448950K .......... .......... .......... .......... .......... 89% 41.4M 4s
449000K .......... .......... .......... .......... .......... 89% 41.3M 4s
449050K .......... .......... .......... .......... .......... 89% 26.9M 4s
449100K .......... .......... .......... .......... .......... 89% 23.9M 4s
449150K .......... .......... .......... .......... .......... 89% 37.6M 4s
449200K .......... .......... .......... .......... .......... 89% 27.3M 4s
449250K .......... .......... .......... .......... .......... 89% 38.3M 4s
449300K .......... .......... .......... .......... .......... 89% 35.1M 4s
449350K .......... .......... .......... .......... .......... 89% 29.2M 4s
449400K .......... .......... .......... .......... .......... 89% 30.2M 4s
449450K .......... .......... .......... .......... .......... 89% 27.5M 4s
449500K .......... .......... .......... .......... .......... 89% 36.7M 4s
449550K .......... .......... .......... .......... .......... 89% 38.2M 4s
449600K .......... .......... .......... .......... .......... 89% 27.0M 4s
449650K .......... .......... .......... .......... .......... 89% 30.9M 4s
449700K .......... .......... .......... .......... .......... 89% 29.8M 4s
449750K .......... .......... .......... .......... .......... 89% 31.5M 4s
449800K .......... .......... .......... .......... .......... 89% 31.0M 4s
449850K .......... .......... .......... .......... .......... 89% 32.1M 4s
449900K .......... .......... .......... .......... .......... 89% 24.1M 4s
449950K .......... .......... .......... .......... .......... 89% 25.6M 4s
450000K .......... .......... .......... .......... .......... 89% 25.7M 4s
450050K .......... .......... .......... .......... .......... 89% 22.6M 4s
450100K .......... .......... .......... .......... .......... 89% 11.5M 4s
450150K .......... .......... .......... .......... .......... 89% 16.1M 4s
450200K .......... .......... .......... .......... .......... 89% 13.6M 4s
450250K .......... .......... .......... .......... .......... 89% 17.5M 4s
450300K .......... .......... .......... .......... .......... 89% 17.6M 4s
450350K .......... .......... .......... .......... .......... 89% 16.1M 4s
450400K .......... .......... .......... .......... .......... 89% 19.1M 4s
450450K .......... .......... .......... .......... .......... 89% 18.5M 4s
450500K .......... .......... .......... .......... .......... 89% 22.2M 4s
450550K .......... .......... .......... .......... .......... 89% 25.5M 4s
450600K .......... .......... .......... .......... .......... 89% 29.7M 4s
450650K .......... .......... .......... .......... .......... 89% 38.3M 4s
450700K .......... .......... .......... .......... .......... 89% 38.4M 4s
450750K .......... .......... .......... .......... .......... 89% 18.3M 4s
450800K .......... .......... .......... .......... .......... 89%  105M 4s
450850K .......... .......... .......... .......... .......... 89% 40.2M 4s
450900K .......... .......... .......... .......... .......... 89% 76.5M 4s
450950K .......... .......... .......... .......... .......... 89% 80.2M 4s
451000K .......... .......... .......... .......... .......... 89% 38.1M 4s
451050K .......... .......... .......... .......... .......... 89% 48.5M 4s
451100K .......... .......... .......... .......... .......... 89% 31.6M 4s
451150K .......... .......... .......... .......... .......... 89% 42.1M 4s
451200K .......... .......... .......... .......... .......... 89% 38.8M 4s
451250K .......... .......... .......... .......... .......... 89% 39.0M 4s
451300K .......... .......... .......... .......... .......... 89% 42.4M 4s
451350K .......... .......... .......... .......... .......... 89% 32.4M 4s
451400K .......... .......... .......... .......... .......... 89% 48.2M 4s
451450K .......... .......... .......... .......... .......... 89% 29.8M 4s
451500K .......... .......... .......... .......... .......... 89% 42.3M 4s
451550K .......... .......... .......... .......... .......... 89% 48.2M 4s
451600K .......... .......... .......... .......... .......... 89% 32.7M 4s
451650K .......... .......... .......... .......... .......... 89% 41.6M 4s
451700K .......... .......... .......... .......... .......... 89% 36.9M 4s
451750K .......... .......... .......... .......... .......... 89% 48.1M 4s
451800K .......... .......... .......... .......... .......... 89% 51.1M 4s
451850K .......... .......... .......... .......... .......... 89% 34.4M 4s
451900K .......... .......... .......... .......... .......... 89% 48.1M 4s
451950K .......... .......... .......... .......... .......... 89% 32.5M 4s
452000K .......... .......... .......... .......... .......... 89% 42.7M 4s
452050K .......... .......... .......... .......... .......... 89% 48.2M 4s
452100K .......... .......... .......... .......... .......... 89% 27.6M 4s
452150K .......... .......... .......... .......... .......... 89% 42.9M 4s
452200K .......... .......... .......... .......... .......... 89% 54.1M 4s
452250K .......... .......... .......... .......... .......... 89% 39.1M 4s
452300K .......... .......... .......... .......... .......... 89% 38.4M 4s
452350K .......... .......... .......... .......... .......... 89% 38.1M 4s
452400K .......... .......... .......... .......... .......... 89% 42.8M 4s
452450K .......... .......... .......... .......... .......... 89% 38.3M 4s
452500K .......... .......... .......... .......... .......... 89% 18.0M 4s
452550K .......... .......... .......... .......... .......... 89%  404M 4s
452600K .......... .......... .......... .......... .......... 89% 44.1M 4s
452650K .......... .......... .......... .......... .......... 89%  421M 4s
452700K .......... .......... .......... .......... .......... 89%  373M 4s
452750K .......... .......... .......... .......... .......... 89% 19.2M 4s
452800K .......... .......... .......... .......... .......... 89% 69.8M 4s
452850K .......... .......... .......... .......... .......... 89% 78.8M 4s
452900K .......... .......... .......... .......... .......... 89% 53.2M 4s
452950K .......... .......... .......... .......... .......... 89% 48.2M 4s
453000K .......... .......... .......... .......... .......... 89% 24.7M 4s
453050K .......... .......... .......... .......... .......... 89% 32.5M 4s
453100K .......... .......... .......... .......... .......... 89% 19.2M 4s
453150K .......... .......... .......... .......... .......... 89% 27.5M 4s
453200K .......... .......... .......... .......... .......... 90% 18.7M 4s
453250K .......... .......... .......... .......... .......... 90% 27.0M 4s
453300K .......... .......... .......... .......... .......... 90% 19.5M 4s
453350K .......... .......... .......... .......... .......... 90% 21.2M 4s
453400K .......... .......... .......... .......... .......... 90% 15.7M 4s
453450K .......... .......... .......... .......... .......... 90% 27.4M 4s
453500K .......... .......... .......... .......... .......... 90% 21.9M 4s
453550K .......... .......... .......... .......... .......... 90% 27.1M 4s
453600K .......... .......... .......... .......... .......... 90% 17.4M 4s
453650K .......... .......... .......... .......... .......... 90% 26.9M 4s
453700K .......... .......... .......... .......... .......... 90% 17.5M 4s
453750K .......... .......... .......... .......... .......... 90% 25.6M 4s
453800K .......... .......... .......... .......... .......... 90% 34.5M 4s
453850K .......... .......... .......... .......... .......... 90% 32.5M 4s
453900K .......... .......... .......... .......... .......... 90% 19.2M 4s
453950K .......... .......... .......... .......... .......... 90% 26.7M 4s
454000K .......... .......... .......... .......... .......... 90% 61.6M 4s
454050K .......... .......... .......... .......... .......... 90% 20.9M 4s
454100K .......... .......... .......... .......... .......... 90% 38.8M 4s
454150K .......... .......... .......... .......... .......... 90% 38.9M 4s
454200K .......... .......... .......... .......... .......... 90% 14.7M 4s
454250K .......... .......... .......... .......... .......... 90%  379M 3s
454300K .......... .......... .......... .......... .......... 90% 33.7M 3s
454350K .......... .......... .......... .......... .......... 90% 61.8M 3s
454400K .......... .......... .......... .......... .......... 90% 81.9M 3s
454450K .......... .......... .......... .......... .......... 90% 26.1M 3s
454500K .......... .......... .......... .......... .......... 90% 45.4M 3s
454550K .......... .......... .......... .......... .......... 90% 31.4M 3s
454600K .......... .......... .......... .......... .......... 90% 24.6M 3s
454650K .......... .......... .......... .......... .......... 90% 22.2M 3s
454700K .......... .......... .......... .......... .......... 90% 24.1M 3s
454750K .......... .......... .......... .......... .......... 90% 24.0M 3s
454800K .......... .......... .......... .......... .......... 90% 27.6M 3s
454850K .......... .......... .......... .......... .......... 90% 24.0M 3s
454900K .......... .......... .......... .......... .......... 90% 23.9M 3s
454950K .......... .......... .......... .......... .......... 90% 22.9M 3s
455000K .......... .......... .......... .......... .......... 90% 29.7M 3s
455050K .......... .......... .......... .......... .......... 90% 24.1M 3s
455100K .......... .......... .......... .......... .......... 90% 22.8M 3s
455150K .......... .......... .......... .......... .......... 90% 22.6M 3s
455200K .......... .......... .......... .......... .......... 90% 23.8M 3s
455250K .......... .......... .......... .......... .......... 90% 26.0M 3s
455300K .......... .......... .......... .......... .......... 90% 24.1M 3s
455350K .......... .......... .......... .......... .......... 90% 22.5M 3s
455400K .......... .......... .......... .......... .......... 90% 24.3M 3s
455450K .......... .......... .......... .......... .......... 90% 22.6M 3s
455500K .......... .......... .......... .......... .......... 90% 18.6M 3s
455550K .......... .......... .......... .......... .......... 90% 47.9M 3s
455600K .......... .......... .......... .......... .......... 90% 22.6M 3s
455650K .......... .......... .......... .......... .......... 90% 21.7M 3s
455700K .......... .......... .......... .......... .......... 90% 14.6M 3s
455750K .......... .......... .......... .......... .......... 90% 22.5M 3s
455800K .......... .......... .......... .......... .......... 90% 34.3M 3s
455850K .......... .......... .......... .......... .......... 90% 18.2M 3s
455900K .......... .......... .......... .......... .......... 90%  126M 3s
455950K .......... .......... .......... .......... .......... 90% 7.99M 3s
456000K .......... .......... .......... .......... .......... 90%  183M 3s
456050K .......... .......... .......... .......... .......... 90% 67.2M 3s
456100K .......... .......... .......... .......... .......... 90% 14.9M 3s
456150K .......... .......... .......... .......... .......... 90% 22.4M 3s
456200K .......... .......... .......... .......... .......... 90% 20.4M 3s
456250K .......... .......... .......... .......... .......... 90% 19.9M 3s
456300K .......... .......... .......... .......... .......... 90% 25.2M 3s
456350K .......... .......... .......... .......... .......... 90% 16.8M 3s
456400K .......... .......... .......... .......... .......... 90% 24.4M 3s
456450K .......... .......... .......... .......... .......... 90% 16.8M 3s
456500K .......... .......... .......... .......... .......... 90% 23.9M 3s
456550K .......... .......... .......... .......... .......... 90% 25.6M 3s
456600K .......... .......... .......... .......... .......... 90% 13.1M 3s
456650K .......... .......... .......... .......... .......... 90% 13.1M 3s
456700K .......... .......... .......... .......... .......... 90% 10.8M 3s
456750K .......... .......... .......... .......... .......... 90% 18.9M 3s
456800K .......... .......... .......... .......... .......... 90% 24.2M 3s
456850K .......... .......... .......... .......... .......... 90% 20.0M 3s
456900K .......... .......... .......... .......... .......... 90% 17.9M 3s
456950K .......... .......... .......... .......... .......... 90% 36.3M 3s
457000K .......... .......... .......... .......... .......... 90% 25.5M 3s
457050K .......... .......... .......... .......... .......... 90% 49.1M 3s
457100K .......... .......... .......... .......... .......... 90% 23.6M 3s
457150K .......... .......... .......... .......... .......... 90% 31.8M 3s
457200K .......... .......... .......... .......... .......... 90% 27.3M 3s
457250K .......... .......... .......... .......... .......... 90% 34.4M 3s
457300K .......... .......... .......... .......... .......... 90% 28.7M 3s
457350K .......... .......... .......... .......... .......... 90% 27.4M 3s
457400K .......... .......... .......... .......... .......... 90% 31.2M 3s
457450K .......... .......... .......... .......... .......... 90% 23.8M 3s
457500K .......... .......... .......... .......... .......... 90% 42.6M 3s
457550K .......... .......... .......... .......... .......... 90% 24.6M 3s
457600K .......... .......... .......... .......... .......... 90% 22.6M 3s
457650K .......... .......... .......... .......... .......... 90% 54.3M 3s
457700K .......... .......... .......... .......... .......... 90% 22.7M 3s
457750K .......... .......... .......... .......... .......... 90% 38.8M 3s
457800K .......... .......... .......... .......... .......... 90% 24.3M 3s
457850K .......... .......... .......... .......... .......... 90% 25.7M 3s
457900K .......... .......... .......... .......... .......... 90% 42.9M 3s
457950K .......... .......... .......... .......... .......... 90% 42.2M 3s
458000K .......... .......... .......... .......... .......... 90% 48.3M 3s
458050K .......... .......... .......... .......... .......... 90% 38.3M 3s
458100K .......... .......... .......... .......... .......... 90% 24.9M 3s
458150K .......... .......... .......... .......... .......... 90% 74.1M 3s
458200K .......... .......... .......... .......... .......... 90%  106M 3s
458250K .......... .......... .......... .......... .......... 91% 49.5M 3s
458300K .......... .......... .......... .......... .......... 91% 96.7M 3s
458350K .......... .......... .......... .......... .......... 91% 62.4M 3s
458400K .......... .......... .......... .......... .......... 91% 76.7M 3s
458450K .......... .......... .......... .......... .......... 91%  291M 3s
458500K .......... .......... .......... .......... .......... 91% 36.3M 3s
458550K .......... .......... .......... .......... .......... 91% 47.8M 3s
458600K .......... .......... .......... .......... .......... 91% 31.7M 3s
458650K .......... .......... .......... .......... .......... 91% 35.5M 3s
458700K .......... .......... .......... .......... .......... 91% 52.1M 3s
458750K .......... .......... .......... .......... .......... 91% 35.9M 3s
458800K .......... .......... .......... .......... .......... 91% 51.7M 3s
458850K .......... .......... .......... .......... .......... 91% 31.4M 3s
458900K .......... .......... .......... .......... .......... 91% 38.2M 3s
458950K .......... .......... .......... .......... .......... 91% 30.3M 3s
459000K .......... .......... .......... .......... .......... 91% 48.0M 3s
459050K .......... .......... .......... .......... .......... 91% 51.8M 3s
459100K .......... .......... .......... .......... .......... 91% 29.8M 3s
459150K .......... .......... .......... .......... .......... 91% 46.2M 3s
459200K .......... .......... .......... .......... .......... 91% 42.1M 3s
459250K .......... .......... .......... .......... .......... 91% 33.8M 3s
459300K .......... .......... .......... .......... .......... 91% 43.5M 3s
459350K .......... .......... .......... .......... .......... 91% 40.5M 3s
459400K .......... .......... .......... .......... .......... 91% 42.1M 3s
459450K .......... .......... .......... .......... .......... 91% 32.3M 3s
459500K .......... .......... .......... .......... .......... 91% 27.5M 3s
459550K .......... .......... .......... .......... .......... 91% 34.7M 3s
459600K .......... .......... .......... .......... .......... 91% 50.6M 3s
459650K .......... .......... .......... .......... .......... 91% 34.4M 3s
459700K .......... .......... .......... .......... .......... 91% 34.2M 3s
459750K .......... .......... .......... .......... .......... 91% 38.2M 3s
459800K .......... .......... .......... .......... .......... 91% 22.3M 3s
459850K .......... .......... .......... .......... .......... 91% 27.1M 3s
459900K .......... .......... .......... .......... .......... 91% 46.4M 3s
459950K .......... .......... .......... .......... .......... 91% 15.4M 3s
460000K .......... .......... .......... .......... .......... 91%  549M 3s
460050K .......... .......... .......... .......... .......... 91% 30.0M 3s
460100K .......... .......... .......... .......... .......... 91% 77.6M 3s
460150K .......... .......... .......... .......... .......... 91% 43.0M 3s
460200K .......... .......... .......... .......... .......... 91% 21.6M 3s
460250K .......... .......... .......... .......... .......... 91%  107M 3s
460300K .......... .......... .......... .......... .......... 91% 37.6M 3s
460350K .......... .......... .......... .......... .......... 91%  142M 3s
460400K .......... .......... .......... .......... .......... 91% 46.1M 3s
460450K .......... .......... .......... .......... .......... 91% 33.2M 3s
460500K .......... .......... .......... .......... .......... 91% 40.9M 3s
460550K .......... .......... .......... .......... .......... 91% 39.5M 3s
460600K .......... .......... .......... .......... .......... 91% 23.2M 3s
460650K .......... .......... .......... .......... .......... 91% 37.9M 3s
460700K .......... .......... .......... .......... .......... 91% 43.1M 3s
460750K .......... .......... .......... .......... .......... 91% 42.6M 3s
460800K .......... .......... .......... .......... .......... 91% 29.4M 3s
460850K .......... .......... .......... .......... .......... 91% 37.3M 3s
460900K .......... .......... .......... .......... .......... 91% 29.5M 3s
460950K .......... .......... .......... .......... .......... 91% 26.7M 3s
461000K .......... .......... .......... .......... .......... 91% 34.8M 3s
461050K .......... .......... .......... .......... .......... 91% 41.0M 3s
461100K .......... .......... .......... .......... .......... 91% 23.2M 3s
461150K .......... .......... .......... .......... .......... 91% 41.8M 3s
461200K .......... .......... .......... .......... .......... 91% 32.0M 3s
461250K .......... .......... .......... .......... .......... 91% 40.4M 3s
461300K .......... .......... .......... .......... .......... 91% 35.0M 3s
461350K .......... .......... .......... .......... .......... 91% 31.3M 3s
461400K .......... .......... .......... .......... .......... 91% 38.4M 3s
461450K .......... .......... .......... .......... .......... 91% 37.5M 3s
461500K .......... .......... .......... .......... .......... 91% 28.3M 3s
461550K .......... .......... .......... .......... .......... 91% 41.9M 3s
461600K .......... .......... .......... .......... .......... 91% 31.7M 3s
461650K .......... .......... .......... .......... .......... 91% 88.3M 3s
461700K .......... .......... .......... .......... .......... 91% 14.5M 3s
461750K .......... .......... .......... .......... .......... 91%  549M 3s
461800K .......... .......... .......... .......... .......... 91% 35.0M 3s
461850K .......... .......... .......... .......... .......... 91%  394M 3s
461900K .......... .......... .......... .......... .......... 91% 29.1M 3s
461950K .......... .......... .......... .......... .......... 91% 75.5M 3s
462000K .......... .......... .......... .......... .......... 91%  376M 3s
462050K .......... .......... .......... .......... .......... 91% 53.9M 3s
462100K .......... .......... .......... .......... .......... 91%  220M 3s
462150K .......... .......... .......... .......... .......... 91% 46.7M 3s
462200K .......... .......... .......... .......... .......... 91% 30.7M 3s
462250K .......... .......... .......... .......... .......... 91% 35.1M 3s
462300K .......... .......... .......... .......... .......... 91% 41.9M 3s
462350K .......... .......... .......... .......... .......... 91% 47.2M 3s
462400K .......... .......... .......... .......... .......... 91% 41.6M 3s
462450K .......... .......... .......... .......... .......... 91% 46.2M 3s
462500K .......... .......... .......... .......... .......... 91% 52.9M 3s
462550K .......... .......... .......... .......... .......... 91% 54.5M 3s
462600K .......... .......... .......... .......... .......... 91% 23.7M 3s
462650K .......... .......... .......... .......... .......... 91% 48.1M 3s
462700K .......... .......... .......... .......... .......... 91% 53.2M 3s
462750K .......... .......... .......... .......... .......... 91% 36.9M 3s
462800K .......... .......... .......... .......... .......... 91% 51.2M 3s
462850K .......... .......... .......... .......... .......... 91% 46.2M 3s
462900K .......... .......... .......... .......... .......... 91% 47.4M 3s
462950K .......... .......... .......... .......... .......... 91% 42.6M 3s
463000K .......... .......... .......... .......... .......... 91% 34.4M 3s
463050K .......... .......... .......... .......... .......... 91% 54.0M 3s
463100K .......... .......... .......... .......... .......... 91% 33.5M 3s
463150K .......... .......... .......... .......... .......... 91% 41.3M 3s
463200K .......... .......... .......... .......... .......... 91% 47.9M 3s
463250K .......... .......... .......... .......... .......... 91% 53.6M 3s
463300K .......... .......... .......... .......... .......... 92% 31.7M 3s
463350K .......... .......... .......... .......... .......... 92% 46.0M 3s
463400K .......... .......... .......... .......... .......... 92% 34.0M 3s
463450K .......... .......... .......... .......... .......... 92% 37.1M 3s
463500K .......... .......... .......... .......... .......... 92% 47.9M 3s
463550K .......... .......... .......... .......... .......... 92% 30.1M 3s
463600K .......... .......... .......... .......... .......... 92% 47.6M 3s
463650K .......... .......... .......... .......... .......... 92% 52.6M 3s
463700K .......... .......... .......... .......... .......... 92% 61.3M 3s
463750K .......... .......... .......... .......... .......... 92% 47.8M 3s
463800K .......... .......... .......... .......... .......... 92% 63.3M 3s
463850K .......... .......... .......... .......... .......... 92% 53.2M 3s
463900K .......... .......... .......... .......... .......... 92% 16.8M 3s
463950K .......... .......... .......... .......... .......... 92%  394M 3s
464000K .......... .......... .......... .......... .......... 92% 53.3M 3s
464050K .......... .......... .......... .......... .......... 92%  421M 3s
464100K .......... .......... .......... .......... .......... 92% 32.0M 3s
464150K .......... .......... .......... .......... .......... 92% 38.4M 3s
464200K .......... .......... .......... .......... .......... 92%  397M 3s
464250K .......... .......... .......... .......... .......... 92%  488M 3s
464300K .......... .......... .......... .......... .......... 92% 22.0M 3s
464350K .......... .......... .......... .......... .......... 92%  208M 3s
464400K .......... .......... .......... .......... .......... 92% 27.3M 3s
464450K .......... .......... .......... .......... .......... 92% 45.8M 3s
464500K .......... .......... .......... .......... .......... 92% 40.4M 3s
464550K .......... .......... .......... .......... .......... 92% 35.7M 3s
464600K .......... .......... .......... .......... .......... 92% 27.4M 3s
464650K .......... .......... .......... .......... .......... 92% 48.2M 3s
464700K .......... .......... .......... .......... .......... 92% 34.7M 3s
464750K .......... .......... .......... .......... .......... 92% 37.2M 3s
464800K .......... .......... .......... .......... .......... 92% 47.0M 3s
464850K .......... .......... .......... .......... .......... 92% 33.0M 3s
464900K .......... .......... .......... .......... .......... 92% 41.0M 3s
464950K .......... .......... .......... .......... .......... 92% 27.4M 3s
465000K .......... .......... .......... .......... .......... 92% 40.6M 3s
465050K .......... .......... .......... .......... .......... 92% 33.5M 3s
465100K .......... .......... .......... .......... .......... 92% 32.1M 3s
465150K .......... .......... .......... .......... .......... 92% 40.0M 3s
465200K .......... .......... .......... .......... .......... 92% 41.2M 3s
465250K .......... .......... .......... .......... .......... 92% 28.4M 3s
465300K .......... .......... .......... .......... .......... 92% 41.2M 3s
465350K .......... .......... .......... .......... .......... 92% 31.0M 3s
465400K .......... .......... .......... .......... .......... 92% 41.3M 3s
465450K .......... .......... .......... .......... .......... 92% 31.0M 3s
465500K .......... .......... .......... .......... .......... 92% 28.9M 3s
465550K .......... .......... .......... .......... .......... 92% 47.9M 3s
465600K .......... .......... .......... .......... .......... 92% 27.7M 3s
465650K .......... .......... .......... .......... .......... 92% 21.0M 3s
465700K .......... .......... .......... .......... .......... 92% 10.8M 3s
465750K .......... .......... .......... .......... .......... 92% 10.0M 3s
465800K .......... .......... .......... .......... .......... 92% 41.1M 3s
465850K .......... .......... .......... .......... .......... 92% 22.4M 3s
465900K .......... .......... .......... .......... .......... 92% 25.6M 3s
465950K .......... .......... .......... .......... .......... 92% 14.2M 3s
466000K .......... .......... .......... .......... .......... 92% 20.0M 3s
466050K .......... .......... .......... .......... .......... 92% 22.4M 3s
466100K .......... .......... .......... .......... .......... 92% 17.5M 3s
466150K .......... .......... .......... .......... .......... 92% 17.2M 3s
466200K .......... .......... .......... .......... .......... 92% 20.2M 3s
466250K .......... .......... .......... .......... .......... 92% 17.3M 3s
466300K .......... .......... .......... .......... .......... 92% 22.6M 3s
466350K .......... .......... .......... .......... .......... 92% 20.8M 3s
466400K .......... .......... .......... .......... .......... 92% 17.5M 3s
466450K .......... .......... .......... .......... .......... 92% 13.2M 3s
466500K .......... .......... .......... .......... .......... 92% 11.7M 3s
466550K .......... .......... .......... .......... .......... 92% 12.0M 3s
466600K .......... .......... .......... .......... .......... 92% 14.6M 3s
466650K .......... .......... .......... .......... .......... 92% 13.2M 3s
466700K .......... .......... .......... .......... .......... 92% 20.2M 3s
466750K .......... .......... .......... .......... .......... 92% 13.6M 3s
466800K .......... .......... .......... .......... .......... 92%  384M 3s
466850K .......... .......... .......... .......... .......... 92% 19.2M 3s
466900K .......... .......... .......... .......... .......... 92% 47.6M 3s
466950K .......... .......... .......... .......... .......... 92% 30.4M 3s
467000K .......... .......... .......... .......... .......... 92% 31.5M 3s
467050K .......... .......... .......... .......... .......... 92% 37.0M 3s
467100K .......... .......... .......... .......... .......... 92% 25.8M 3s
467150K .......... .......... .......... .......... .......... 92% 41.4M 3s
467200K .......... .......... .......... .......... .......... 92% 29.3M 3s
467250K .......... .......... .......... .......... .......... 92% 38.5M 3s
467300K .......... .......... .......... .......... .......... 92% 35.2M 3s
467350K .......... .......... .......... .......... .......... 92% 30.5M 3s
467400K .......... .......... .......... .......... .......... 92% 34.3M 3s
467450K .......... .......... .......... .......... .......... 92% 25.2M 3s
467500K .......... .......... .......... .......... .......... 92% 48.3M 3s
467550K .......... .......... .......... .......... .......... 92% 31.1M 3s
467600K .......... .......... .......... .......... .......... 92% 29.2M 3s
467650K .......... .......... .......... .......... .......... 92% 42.3M 3s
467700K .......... .......... .......... .......... .......... 92% 24.8M 3s
467750K .......... .......... .......... .......... .......... 92% 33.1M 3s
467800K .......... .......... .......... .......... .......... 92% 37.5M 2s
467850K .......... .......... .......... .......... .......... 92% 34.9M 2s
467900K .......... .......... .......... .......... .......... 92% 38.3M 2s
467950K .......... .......... .......... .......... .......... 92% 27.1M 2s
468000K .......... .......... .......... .......... .......... 92% 48.2M 2s
468050K .......... .......... .......... .......... .......... 92% 44.0M 2s
468100K .......... .......... .......... .......... .......... 92% 38.5M 2s
468150K .......... .......... .......... .......... .......... 92%  174M 2s
468200K .......... .......... .......... .......... .......... 92% 34.5M 2s
468250K .......... .......... .......... .......... .......... 92% 95.4M 2s
468300K .......... .......... .......... .......... .......... 92% 16.8M 2s
468350K .......... .......... .......... .......... .......... 93%  381M 2s
468400K .......... .......... .......... .......... .......... 93%  474M 2s
468450K .......... .......... .......... .......... .......... 93% 10.7M 2s
468500K .......... .......... .......... .......... .......... 93%  414M 2s
468550K .......... .......... .......... .......... .......... 93%  436M 2s
468600K .......... .......... .......... .......... .......... 93% 65.1M 2s
468650K .......... .......... .......... .......... .......... 93% 25.4M 2s
468700K .......... .......... .......... .......... .......... 93%  470M 2s
468750K .......... .......... .......... .......... .......... 93% 22.1M 2s
468800K .......... .......... .......... .......... .......... 93%  191M 2s
468850K .......... .......... .......... .......... .......... 93% 25.4M 2s
468900K .......... .......... .......... .......... .......... 93% 31.9M 2s
468950K .......... .......... .......... .......... .......... 93% 23.4M 2s
469000K .......... .......... .......... .......... .......... 93% 34.3M 2s
469050K .......... .......... .......... .......... .......... 93% 28.7M 2s
469100K .......... .......... .......... .......... .......... 93% 25.8M 2s
469150K .......... .......... .......... .......... .......... 93% 46.8M 2s
469200K .......... .......... .......... .......... .......... 93% 21.8M 2s
469250K .......... .......... .......... .......... .......... 93% 41.0M 2s
469300K .......... .......... .......... .......... .......... 93% 28.6M 2s
469350K .......... .......... .......... .......... .......... 93% 29.2M 2s
469400K .......... .......... .......... .......... .......... 93% 31.8M 2s
469450K .......... .......... .......... .......... .......... 93% 28.3M 2s
469500K .......... .......... .......... .......... .......... 93% 27.5M 2s
469550K .......... .......... .......... .......... .......... 93% 37.5M 2s
469600K .......... .......... .......... .......... .......... 93% 22.6M 2s
469650K .......... .......... .......... .......... .......... 93% 37.7M 2s
469700K .......... .......... .......... .......... .......... 93% 25.4M 2s
469750K .......... .......... .......... .......... .......... 93% 40.6M 2s
469800K .......... .......... .......... .......... .......... 93% 27.0M 2s
469850K .......... .......... .......... .......... .......... 93% 25.2M 2s
469900K .......... .......... .......... .......... .......... 93% 27.2M 2s
469950K .......... .......... .......... .......... .......... 93% 21.2M 2s
470000K .......... .......... .......... .......... .......... 93% 13.9M 2s
470050K .......... .......... .......... .......... .......... 93%  421M 2s
470100K .......... .......... .......... .......... .......... 93% 17.6M 2s
470150K .......... .......... .......... .......... .......... 93%  474M 2s
470200K .......... .......... .......... .......... .......... 93% 30.9M 2s
470250K .......... .......... .......... .......... .......... 93% 19.4M 2s
470300K .......... .......... .......... .......... .......... 93% 30.0M 2s
470350K .......... .......... .......... .......... .......... 93% 40.3M 2s
470400K .......... .......... .......... .......... .......... 93% 24.0M 2s
470450K .......... .......... .......... .......... .......... 93% 18.1M 2s
470500K .......... .......... .......... .......... .......... 93% 28.8M 2s
470550K .......... .......... .......... .......... .......... 93% 27.2M 2s
470600K .......... .......... .......... .......... .......... 93% 19.1M 2s
470650K .......... .......... .......... .......... .......... 93% 26.8M 2s
470700K .......... .......... .......... .......... .......... 93% 19.0M 2s
470750K .......... .......... .......... .......... .......... 93% 23.9M 2s
470800K .......... .......... .......... .......... .......... 93% 23.0M 2s
470850K .......... .......... .......... .......... .......... 93% 23.8M 2s
470900K .......... .......... .......... .......... .......... 93% 22.0M 2s
470950K .......... .......... .......... .......... .......... 93% 19.8M 2s
471000K .......... .......... .......... .......... .......... 93% 25.4M 2s
471050K .......... .......... .......... .......... .......... 93% 24.6M 2s
471100K .......... .......... .......... .......... .......... 93% 18.3M 2s
471150K .......... .......... .......... .......... .......... 93% 17.4M 2s
471200K .......... .......... .......... .......... .......... 93% 25.3M 2s
471250K .......... .......... .......... .......... .......... 93%  127M 2s
471300K .......... .......... .......... .......... .......... 93% 19.1M 2s
471350K .......... .......... .......... .......... .......... 93% 16.2M 2s
471400K .......... .......... .......... .......... .......... 93% 84.0M 2s
471450K .......... .......... .......... .......... .......... 93% 15.0M 2s
471500K .......... .......... .......... .......... .......... 93%  130M 2s
471550K .......... .......... .......... .......... .......... 93% 27.7M 2s
471600K .......... .......... .......... .......... .......... 93% 25.9M 2s
471650K .......... .......... .......... .......... .......... 93% 29.9M 2s
471700K .......... .......... .......... .......... .......... 93% 27.5M 2s
471750K .......... .......... .......... .......... .......... 93% 29.4M 2s
471800K .......... .......... .......... .......... .......... 93% 25.3M 2s
471850K .......... .......... .......... .......... .......... 93% 25.5M 2s
471900K .......... .......... .......... .......... .......... 93% 22.3M 2s
471950K .......... .......... .......... .......... .......... 93% 22.5M 2s
472000K .......... .......... .......... .......... .......... 93% 34.2M 2s
472050K .......... .......... .......... .......... .......... 93% 26.3M 2s
472100K .......... .......... .......... .......... .......... 93% 23.5M 2s
472150K .......... .......... .......... .......... .......... 93% 23.9M 2s
472200K .......... .......... .......... .......... .......... 93% 25.0M 2s
472250K .......... .......... .......... .......... .......... 93% 22.2M 2s
472300K .......... .......... .......... .......... .......... 93% 42.6M 2s
472350K .......... .......... .......... .......... .......... 93% 23.9M 2s
472400K .......... .......... .......... .......... .......... 93% 26.8M 2s
472450K .......... .......... .......... .......... .......... 93% 23.4M 2s
472500K .......... .......... .......... .......... .......... 93% 23.4M 2s
472550K .......... .......... .......... .......... .......... 93% 31.3M 2s
472600K .......... .......... .......... .......... .......... 93% 21.5M 2s
472650K .......... .......... .......... .......... .......... 93%  180M 2s
472700K .......... .......... .......... .......... .......... 93% 10.9M 2s
472750K .......... .......... .......... .......... .......... 93% 32.0M 2s
472800K .......... .......... .......... .......... .......... 93%  133M 2s
472850K .......... .......... .......... .......... .......... 93% 23.1M 2s
472900K .......... .......... .......... .......... .......... 93% 27.1M 2s
472950K .......... .......... .......... .......... .......... 93%  100M 2s
473000K .......... .......... .......... .......... .......... 93% 26.5M 2s
473050K .......... .......... .......... .......... .......... 93% 25.5M 2s
473100K .......... .......... .......... .......... .......... 93% 20.4M 2s
473150K .......... .......... .......... .......... .......... 93% 26.9M 2s
473200K .......... .......... .......... .......... .......... 93% 21.0M 2s
473250K .......... .......... .......... .......... .......... 93% 27.4M 2s
473300K .......... .......... .......... .......... .......... 93% 26.9M 2s
473350K .......... .......... .......... .......... .......... 94% 22.0M 2s
473400K .......... .......... .......... .......... .......... 94% 22.8M 2s
473450K .......... .......... .......... .......... .......... 94% 19.0M 2s
473500K .......... .......... .......... .......... .......... 94% 25.7M 2s
473550K .......... .......... .......... .......... .......... 94% 23.4M 2s
473600K .......... .......... .......... .......... .......... 94% 21.2M 2s
473650K .......... .......... .......... .......... .......... 94% 21.8M 2s
473700K .......... .......... .......... .......... .......... 94% 20.9M 2s
473750K .......... .......... .......... .......... .......... 94% 18.7M 2s
473800K .......... .......... .......... .......... .......... 94% 23.8M 2s
473850K .......... .......... .......... .......... .......... 94% 24.3M 2s
473900K .......... .......... .......... .......... .......... 94% 9.74M 2s
473950K .......... .......... .......... .......... .......... 94%  319M 2s
474000K .......... .......... .......... .......... .......... 94% 29.3M 2s
474050K .......... .......... .......... .......... .......... 94% 70.7M 2s
474100K .......... .......... .......... .......... .......... 94% 17.3M 2s
474150K .......... .......... .......... .......... .......... 94% 44.1M 2s
474200K .......... .......... .......... .......... .......... 94% 37.8M 2s
474250K .......... .......... .......... .......... .......... 94% 27.0M 2s
474300K .......... .......... .......... .......... .......... 94% 25.0M 2s
474350K .......... .......... .......... .......... .......... 94% 34.1M 2s
474400K .......... .......... .......... .......... .......... 94% 23.9M 2s
474450K .......... .......... .......... .......... .......... 94% 26.7M 2s
474500K .......... .......... .......... .......... .......... 94% 23.7M 2s
474550K .......... .......... .......... .......... .......... 94% 25.2M 2s
474600K .......... .......... .......... .......... .......... 94% 22.2M 2s
474650K .......... .......... .......... .......... .......... 94% 23.9M 2s
474700K .......... .......... .......... .......... .......... 94% 25.4M 2s
474750K .......... .......... .......... .......... .......... 94% 27.2M 2s
474800K .......... .......... .......... .......... .......... 94% 10.1M 2s
474850K .......... .......... .......... .......... .......... 94% 16.4M 2s
474900K .......... .......... .......... .......... .......... 94% 37.9M 2s
474950K .......... .......... .......... .......... .......... 94% 17.0M 2s
475000K .......... .......... .......... .......... .......... 94% 28.9M 2s
475050K .......... .......... .......... .......... .......... 94% 35.5M 2s
475100K .......... .......... .......... .......... .......... 94% 10.6M 2s
475150K .......... .......... .......... .......... .......... 94%  483M 2s
475200K .......... .......... .......... .......... .......... 94%  356M 2s
475250K .......... .......... .......... .......... .......... 94% 17.5M 2s
475300K .......... .......... .......... .......... .......... 94% 21.1M 2s
475350K .......... .......... .......... .......... .......... 94% 16.9M 2s
475400K .......... .......... .......... .......... .......... 94% 29.8M 2s
475450K .......... .......... .......... .......... .......... 94% 25.0M 2s
475500K .......... .......... .......... .......... .......... 94% 29.1M 2s
475550K .......... .......... .......... .......... .......... 94% 21.2M 2s
475600K .......... .......... .......... .......... .......... 94% 19.9M 2s
475650K .......... .......... .......... .......... .......... 94% 26.6M 2s
475700K .......... .......... .......... .......... .......... 94% 20.2M 2s
475750K .......... .......... .......... .......... .......... 94% 18.8M 2s
475800K .......... .......... .......... .......... .......... 94% 23.1M 2s
475850K .......... .......... .......... .......... .......... 94% 17.1M 2s
475900K .......... .......... .......... .......... .......... 94% 24.1M 2s
475950K .......... .......... .......... .......... .......... 94% 23.6M 2s
476000K .......... .......... .......... .......... .......... 94% 15.5M 2s
476050K .......... .......... .......... .......... .......... 94% 31.6M 2s
476100K .......... .......... .......... .......... .......... 94% 16.1M 2s
476150K .......... .......... .......... .......... .......... 94% 24.2M 2s
476200K .......... .......... .......... .......... .......... 94% 17.6M 2s
476250K .......... .......... .......... .......... .......... 94% 24.0M 2s
476300K .......... .......... .......... .......... .......... 94% 20.4M 2s
476350K .......... .......... .......... .......... .......... 94% 19.5M 2s
476400K .......... .......... .......... .......... .......... 94% 21.3M 2s
476450K .......... .......... .......... .......... .......... 94% 31.8M 2s
476500K .......... .......... .......... .......... .......... 94% 17.3M 2s
476550K .......... .......... .......... .......... .......... 94%  271M 2s
476600K .......... .......... .......... .......... .......... 94% 13.2M 2s
476650K .......... .......... .......... .......... .......... 94%  407M 2s
476700K .......... .......... .......... .......... .......... 94% 22.7M 2s
476750K .......... .......... .......... .......... .......... 94% 32.0M 2s
476800K .......... .......... .......... .......... .......... 94% 29.6M 2s
476850K .......... .......... .......... .......... .......... 94% 27.2M 2s
476900K .......... .......... .......... .......... .......... 94% 27.6M 2s
476950K .......... .......... .......... .......... .......... 94% 25.6M 2s
477000K .......... .......... .......... .......... .......... 94% 35.2M 2s
477050K .......... .......... .......... .......... .......... 94% 24.1M 2s
477100K .......... .......... .......... .......... .......... 94% 25.5M 2s
477150K .......... .......... .......... .......... .......... 94% 39.1M 2s
477200K .......... .......... .......... .......... .......... 94% 25.6M 2s
477250K .......... .......... .......... .......... .......... 94% 27.4M 2s
477300K .......... .......... .......... .......... .......... 94% 26.0M 2s
477350K .......... .......... .......... .......... .......... 94% 34.6M 2s
477400K .......... .......... .......... .......... .......... 94% 25.9M 2s
477450K .......... .......... .......... .......... .......... 94% 29.7M 2s
477500K .......... .......... .......... .......... .......... 94% 35.2M 2s
477550K .......... .......... .......... .......... .......... 94% 27.4M 2s
477600K .......... .......... .......... .......... .......... 94% 22.6M 2s
477650K .......... .......... .......... .......... .......... 94% 49.2M 2s
477700K .......... .......... .......... .......... .......... 94% 92.3M 2s
477750K .......... .......... .......... .......... .......... 94% 49.2M 2s
477800K .......... .......... .......... .......... .......... 94% 76.2M 2s
477850K .......... .......... .......... .......... .......... 94% 15.7M 2s
477900K .......... .......... .......... .......... .......... 94%  555M 2s
477950K .......... .......... .......... .......... .......... 94%  115M 2s
478000K .......... .......... .......... .......... .......... 94% 83.2M 2s
478050K .......... .......... .......... .......... .......... 94% 70.9M 2s
478100K .......... .......... .......... .......... .......... 94% 67.4M 2s
478150K .......... .......... .......... .......... .......... 94%  124M 2s
478200K .......... .......... .......... .......... .......... 94% 54.5M 2s
478250K .......... .......... .......... .......... .......... 94% 74.8M 2s
478300K .......... .......... .......... .......... .......... 94%  241M 2s
478350K .......... .......... .......... .......... .......... 94% 55.1M 2s
478400K .......... .......... .......... .......... .......... 95% 47.4M 2s
478450K .......... .......... .......... .......... .......... 95% 43.2M 2s
478500K .......... .......... .......... .......... .......... 95% 34.9M 2s
478550K .......... .......... .......... .......... .......... 95% 54.7M 2s
478600K .......... .......... .......... .......... .......... 95% 25.5M 2s
478650K .......... .......... .......... .......... .......... 95% 43.8M 2s
478700K .......... .......... .......... .......... .......... 95% 47.3M 2s
478750K .......... .......... .......... .......... .......... 95% 53.8M 2s
478800K .......... .......... .......... .......... .......... 95% 35.9M 2s
478850K .......... .......... .......... .......... .......... 95% 47.0M 2s
478900K .......... .......... .......... .......... .......... 95% 49.2M 2s
478950K .......... .......... .......... .......... .......... 95% 38.6M 2s
479000K .......... .......... .......... .......... .......... 95% 55.3M 2s
479050K .......... .......... .......... .......... .......... 95% 48.0M 2s
479100K .......... .......... .......... .......... .......... 95% 38.6M 2s
479150K .......... .......... .......... .......... .......... 95% 54.6M 2s
479200K .......... .......... .......... .......... .......... 95% 42.1M 2s
479250K .......... .......... .......... .......... .......... 95% 54.6M 2s
479300K .......... .......... .......... .......... .......... 95% 43.4M 2s
479350K .......... .......... .......... .......... .......... 95% 42.7M 2s
479400K .......... .......... .......... .......... .......... 95% 48.2M 2s
479450K .......... .......... .......... .......... .......... 95% 29.6M 2s
479500K .......... .......... .......... .......... .......... 95% 55.2M 2s
479550K .......... .......... .......... .......... .......... 95% 53.7M 2s
479600K .......... .......... .......... .......... .......... 95% 43.6M 2s
479650K .......... .......... .......... .......... .......... 95% 55.0M 2s
479700K .......... .......... .......... .......... .......... 95% 42.9M 2s
479750K .......... .......... .......... .......... .......... 95% 38.6M 2s
479800K .......... .......... .......... .......... .......... 95% 52.7M 2s
479850K .......... .......... .......... .......... .......... 95% 36.0M 2s
479900K .......... .......... .......... .......... .......... 95% 95.9M 2s
479950K .......... .......... .......... .......... .......... 95% 17.3M 2s
480000K .......... .......... .......... .......... .......... 95% 77.6M 2s
480050K .......... .......... .......... .......... .......... 95%  456M 2s
480100K .......... .......... .......... .......... .......... 95%  370M 2s
480150K .......... .......... .......... .......... .......... 95% 40.5M 2s
480200K .......... .......... .......... .......... .......... 95% 56.3M 2s
480250K .......... .......... .......... .......... .......... 95%  384M 2s
480300K .......... .......... .......... .......... .......... 95% 37.9M 2s
480350K .......... .......... .......... .......... .......... 95% 28.3M 2s
480400K .......... .......... .......... .......... .......... 95%  503M 2s
480450K .......... .......... .......... .......... .......... 95%  156M 2s
480500K .......... .......... .......... .......... .......... 95% 33.0M 2s
480550K .......... .......... .......... .......... .......... 95% 59.9M 2s
480600K .......... .......... .......... .......... .......... 95% 27.7M 2s
480650K .......... .......... .......... .......... .......... 95% 22.7M 2s
480700K .......... .......... .......... .......... .......... 95% 27.6M 2s
480750K .......... .......... .......... .......... .......... 95% 32.7M 2s
480800K .......... .......... .......... .......... .......... 95% 26.8M 2s
480850K .......... .......... .......... .......... .......... 95% 22.7M 2s
480900K .......... .......... .......... .......... .......... 95% 21.7M 2s
480950K .......... .......... .......... .......... .......... 95% 43.0M 2s
481000K .......... .......... .......... .......... .......... 95% 25.8M 2s
481050K .......... .......... .......... .......... .......... 95% 29.7M 2s
481100K .......... .......... .......... .......... .......... 95% 27.4M 2s
481150K .......... .......... .......... .......... .......... 95% 21.6M 2s
481200K .......... .......... .......... .......... .......... 95% 25.8M 2s
481250K .......... .......... .......... .......... .......... 95% 42.1M 2s
481300K .......... .......... .......... .......... .......... 95% 27.8M 2s
481350K .......... .......... .......... .......... .......... 95% 25.8M 2s
481400K .......... .......... .......... .......... .......... 95% 29.6M 2s
481450K .......... .......... .......... .......... .......... 95% 27.7M 2s
481500K .......... .......... .......... .......... .......... 95% 29.8M 2s
481550K .......... .......... .......... .......... .......... 95% 31.9M 2s
481600K .......... .......... .......... .......... .......... 95% 21.6M 2s
481650K .......... .......... .......... .......... .......... 95% 32.3M 2s
481700K .......... .......... .......... .......... .......... 95% 24.0M 2s
481750K .......... .......... .......... .......... .......... 95% 30.0M 2s
481800K .......... .......... .......... .......... .......... 95% 22.7M 1s
481850K .......... .......... .......... .......... .......... 95% 16.4M 1s
481900K .......... .......... .......... .......... .......... 95%  479M 1s
481950K .......... .......... .......... .......... .......... 95% 32.0M 1s
482000K .......... .......... .......... .......... .......... 95% 33.1M 1s
482050K .......... .......... .......... .......... .......... 95% 71.2M 1s
482100K .......... .......... .......... .......... .......... 95% 54.0M 1s
482150K .......... .......... .......... .......... .......... 95%  109M 1s
482200K .......... .......... .......... .......... .......... 95% 29.5M 1s
482250K .......... .......... .......... .......... .......... 95% 47.7M 1s
482300K .......... .......... .......... .......... .......... 95% 29.9M 1s
482350K .......... .......... .......... .......... .......... 95% 27.5M 1s
482400K .......... .......... .......... .......... .......... 95% 37.9M 1s
482450K .......... .......... .......... .......... .......... 95% 25.9M 1s
482500K .......... .......... .......... .......... .......... 95% 35.0M 1s
482550K .......... .......... .......... .......... .......... 95% 42.2M 1s
482600K .......... .......... .......... .......... .......... 95% 25.4M 1s
482650K .......... .......... .......... .......... .......... 95% 36.0M 1s
482700K .......... .......... .......... .......... .......... 95% 29.7M 1s
482750K .......... .......... .......... .......... .......... 95% 29.6M 1s
482800K .......... .......... .......... .......... .......... 95% 42.2M 1s
482850K .......... .......... .......... .......... .......... 95% 25.9M 1s
482900K .......... .......... .......... .......... .......... 95% 42.6M 1s
482950K .......... .......... .......... .......... .......... 95% 27.5M 1s
483000K .......... .......... .......... .......... .......... 95% 35.2M 1s
483050K .......... .......... .......... .......... .......... 95% 32.1M 1s
483100K .......... .......... .......... .......... .......... 95% 32.0M 1s
483150K .......... .......... .......... .......... .......... 95% 29.7M 1s
483200K .......... .......... .......... .......... .......... 95% 35.1M 1s
483250K .......... .......... .......... .......... .......... 95% 54.1M 1s
483300K .......... .......... .......... .......... .......... 95% 24.4M 1s
483350K .......... .......... .......... .......... .......... 95% 16.8M 1s
483400K .......... .......... .......... .......... .......... 95% 24.3M 1s
483450K .......... .......... .......... .......... .......... 96% 25.7M 1s
483500K .......... .......... .......... .......... .......... 96% 14.5M 1s
483550K .......... .......... .......... .......... .......... 96%  436M 1s
483600K .......... .......... .......... .......... .......... 96%  136M 1s
483650K .......... .......... .......... .......... .......... 96% 18.5M 1s
483700K .......... .......... .......... .......... .......... 96%  130M 1s
483750K .......... .......... .......... .......... .......... 96% 18.3M 1s
483800K .......... .......... .......... .......... .......... 96%  128M 1s
483850K .......... .......... .......... .......... .......... 96% 27.3M 1s
483900K .......... .......... .......... .......... .......... 96% 27.4M 1s
483950K .......... .......... .......... .......... .......... 96% 27.9M 1s
484000K .......... .......... .......... .......... .......... 96% 22.8M 1s
484050K .......... .......... .......... .......... .......... 96% 43.0M 1s
484100K .......... .......... .......... .......... .......... 96% 22.2M 1s
484150K .......... .......... .......... .......... .......... 96% 26.4M 1s
484200K .......... .......... .......... .......... .......... 96% 23.6M 1s
484250K .......... .......... .......... .......... .......... 96% 38.1M 1s
484300K .......... .......... .......... .......... .......... 96% 27.2M 1s
484350K .......... .......... .......... .......... .......... 96% 23.8M 1s
484400K .......... .......... .......... .......... .......... 96% 42.7M 1s
484450K .......... .......... .......... .......... .......... 96% 27.0M 1s
484500K .......... .......... .......... .......... .......... 96% 27.1M 1s
484550K .......... .......... .......... .......... .......... 96% 46.5M 1s
484600K .......... .......... .......... .......... .......... 96% 25.2M 1s
484650K .......... .......... .......... .......... .......... 96% 29.4M 1s
484700K .......... .......... .......... .......... .......... 96% 30.6M 1s
484750K .......... .......... .......... .......... .......... 96% 27.5M 1s
484800K .......... .......... .......... .......... .......... 96% 25.5M 1s
484850K .......... .......... .......... .......... .......... 96% 25.9M 1s
484900K .......... .......... .......... .......... .......... 96%  124M 1s
484950K .......... .......... .......... .......... .......... 96% 9.19M 1s
485000K .......... .......... .......... .......... .......... 96%  488M 1s
485050K .......... .......... .......... .......... .......... 96%  474M 1s
485100K .......... .......... .......... .......... .......... 96% 18.3M 1s
485150K .......... .......... .......... .......... .......... 96% 27.9M 1s
485200K .......... .......... .......... .......... .......... 96%  138M 1s
485250K .......... .......... .......... .......... .......... 96% 16.3M 1s
485300K .......... .......... .......... .......... .......... 96% 21.5M 1s
485350K .......... .......... .......... .......... .......... 96% 29.3M 1s
485400K .......... .......... .......... .......... .......... 96% 32.0M 1s
485450K .......... .......... .......... .......... .......... 96% 24.5M 1s
485500K .......... .......... .......... .......... .......... 96% 26.9M 1s
485550K .......... .......... .......... .......... .......... 96% 31.0M 1s
485600K .......... .......... .......... .......... .......... 96% 27.0M 1s
485650K .......... .......... .......... .......... .......... 96% 10.3M 1s
485700K .......... .......... .......... .......... .......... 96% 18.3M 1s
485750K .......... .......... .......... .......... .......... 96% 37.5M 1s
485800K .......... .......... .......... .......... .......... 96% 23.9M 1s
485850K .......... .......... .......... .......... .......... 96% 29.0M 1s
485900K .......... .......... .......... .......... .......... 96% 26.7M 1s
485950K .......... .......... .......... .......... .......... 96% 21.3M 1s
486000K .......... .......... .......... .......... .......... 96% 18.8M 1s
486050K .......... .......... .......... .......... .......... 96% 29.2M 1s
486100K .......... .......... .......... .......... .......... 96% 15.4M 1s
486150K .......... .......... .......... .......... .......... 96% 34.7M 1s
486200K .......... .......... .......... .......... .......... 96% 76.8M 1s
486250K .......... .......... .......... .......... .......... 96% 42.1M 1s
486300K .......... .......... .......... .......... .......... 96% 47.2M 1s
486350K .......... .......... .......... .......... .......... 96% 62.2M 1s
486400K .......... .......... .......... .......... .......... 96% 14.3M 1s
486450K .......... .......... .......... .......... .......... 96%  364M 1s
486500K .......... .......... .......... .......... .......... 96%  432M 1s
486550K .......... .......... .......... .......... .......... 96% 16.3M 1s
486600K .......... .......... .......... .......... .......... 96% 50.9M 1s
486650K .......... .......... .......... .......... .......... 96% 20.6M 1s
486700K .......... .......... .......... .......... .......... 96%  202M 1s
486750K .......... .......... .......... .......... .......... 96% 29.7M 1s
486800K .......... .......... .......... .......... .......... 96% 19.3M 1s
486850K .......... .......... .......... .......... .......... 96% 28.7M 1s
486900K .......... .......... .......... .......... .......... 96% 23.7M 1s
486950K .......... .......... .......... .......... .......... 96% 16.5M 1s
487000K .......... .......... .......... .......... .......... 96% 23.9M 1s
487050K .......... .......... .......... .......... .......... 96% 18.9M 1s
487100K .......... .......... .......... .......... .......... 96% 23.7M 1s
487150K .......... .......... .......... .......... .......... 96% 25.7M 1s
487200K .......... .......... .......... .......... .......... 96% 18.8M 1s
487250K .......... .......... .......... .......... .......... 96% 23.6M 1s
487300K .......... .......... .......... .......... .......... 96% 24.0M 1s
487350K .......... .......... .......... .......... .......... 96% 19.0M 1s
487400K .......... .......... .......... .......... .......... 96% 27.2M 1s
487450K .......... .......... .......... .......... .......... 96% 22.2M 1s
487500K .......... .......... .......... .......... .......... 96% 18.4M 1s
487550K .......... .......... .......... .......... .......... 96% 27.5M 1s
487600K .......... .......... .......... .......... .......... 96% 8.19M 1s
487650K .......... .......... .......... .......... .......... 96%  432M 1s
487700K .......... .......... .......... .......... .......... 96% 13.6M 1s
487750K .......... .......... .......... .......... .......... 96% 17.6M 1s
487800K .......... .......... .......... .......... .......... 96% 13.9M 1s
487850K .......... .......... .......... .......... .......... 96% 14.5M 1s
487900K .......... .......... .......... .......... .......... 96% 17.3M 1s
487950K .......... .......... .......... .......... .......... 96% 16.2M 1s
488000K .......... .......... .......... .......... .......... 96% 15.3M 1s
488050K .......... .......... .......... .......... .......... 96% 15.5M 1s
488100K .......... .......... .......... .......... .......... 96% 16.4M 1s
488150K .......... .......... .......... .......... .......... 96% 20.3M 1s
488200K .......... .......... .......... .......... .......... 96% 15.8M 1s
488250K .......... .......... .......... .......... .......... 96% 16.7M 1s
488300K .......... .......... .......... .......... .......... 96% 22.6M 1s
488350K .......... .......... .......... .......... .......... 96% 14.6M 1s
488400K .......... .......... .......... .......... .......... 96% 21.1M 1s
488450K .......... .......... .......... .......... .......... 97% 20.3M 1s
488500K .......... .......... .......... .......... .......... 97% 10.9M 1s
488550K .......... .......... .......... .......... .......... 97% 18.5M 1s
488600K .......... .......... .......... .......... .......... 97%  193M 1s
488650K .......... .......... .......... .......... .......... 97% 16.7M 1s
488700K .......... .......... .......... .......... .......... 97% 19.5M 1s
488750K .......... .......... .......... .......... .......... 97% 25.0M 1s
488800K .......... .......... .......... .......... .......... 97% 19.1M 1s
488850K .......... .......... .......... .......... .......... 97% 19.0M 1s
488900K .......... .......... .......... .......... .......... 97% 22.5M 1s
488950K .......... .......... .......... .......... .......... 97% 16.5M 1s
489000K .......... .......... .......... .......... .......... 97% 23.6M 1s
489050K .......... .......... .......... .......... .......... 97% 21.1M 1s
489100K .......... .......... .......... .......... .......... 97% 21.6M 1s
489150K .......... .......... .......... .......... .......... 97% 21.2M 1s
489200K .......... .......... .......... .......... .......... 97% 15.4M 1s
489250K .......... .......... .......... .......... .......... 97% 23.9M 1s
489300K .......... .......... .......... .......... .......... 97% 23.9M 1s
489350K .......... .......... .......... .......... .......... 97% 22.3M 1s
489400K .......... .......... .......... .......... .......... 97% 28.9M 1s
489450K .......... .......... .......... .......... .......... 97% 18.5M 1s
489500K .......... .......... .......... .......... .......... 97% 20.2M 1s
489550K .......... .......... .......... .......... .......... 97% 11.4M 1s
489600K .......... .......... .......... .......... .......... 97% 55.4M 1s
489650K .......... .......... .......... .......... .......... 97%  440M 1s
489700K .......... .......... .......... .......... .......... 97% 15.0M 1s
489750K .......... .......... .......... .......... .......... 97% 27.0M 1s
489800K .......... .......... .......... .......... .......... 97% 19.1M 1s
489850K .......... .......... .......... .......... .......... 97% 39.3M 1s
489900K .......... .......... .......... .......... .......... 97% 35.1M 1s
489950K .......... .......... .......... .......... .......... 97% 25.9M 1s
490000K .......... .......... .......... .......... .......... 97% 27.1M 1s
490050K .......... .......... .......... .......... .......... 97% 26.0M 1s
490100K .......... .......... .......... .......... .......... 97% 25.6M 1s
490150K .......... .......... .......... .......... .......... 97% 43.4M 1s
490200K .......... .......... .......... .......... .......... 97% 24.1M 1s
490250K .......... .......... .......... .......... .......... 97% 25.8M 1s
490300K .......... .......... .......... .......... .......... 97% 31.7M 1s
490350K .......... .......... .......... .......... .......... 97% 24.3M 1s
490400K .......... .......... .......... .......... .......... 97% 29.7M 1s
490450K .......... .......... .......... .......... .......... 97% 19.3M 1s
490500K .......... .......... .......... .......... .......... 97% 38.4M 1s
490550K .......... .......... .......... .......... .......... 97% 26.8M 1s
490600K .......... .......... .......... .......... .......... 97% 22.4M 1s
490650K .......... .......... .......... .......... .......... 97% 23.2M 1s
490700K .......... .......... .......... .......... .......... 97% 19.8M 1s
490750K .......... .......... .......... .......... .......... 97% 25.1M 1s
490800K .......... .......... .......... .......... .......... 97% 46.2M 1s
490850K .......... .......... .......... .......... .......... 97% 29.0M 1s
490900K .......... .......... .......... .......... .......... 97% 15.8M 1s
490950K .......... .......... .......... .......... .......... 97% 31.8M 1s
491000K .......... .......... .......... .......... .......... 97% 55.9M 1s
491050K .......... .......... .......... .......... .......... 97% 61.8M 1s
491100K .......... .......... .......... .......... .......... 97% 39.2M 1s
491150K .......... .......... .......... .......... .......... 97% 23.8M 1s
491200K .......... .......... .......... .......... .......... 97% 48.2M 1s
491250K .......... .......... .......... .......... .......... 97% 29.3M 1s
491300K .......... .......... .......... .......... .......... 97% 34.0M 1s
491350K .......... .......... .......... .......... .......... 97% 28.9M 1s
491400K .......... .......... .......... .......... .......... 97% 40.8M 1s
491450K .......... .......... .......... .......... .......... 97% 25.3M 1s
491500K .......... .......... .......... .......... .......... 97% 27.2M 1s
491550K .......... .......... .......... .......... .......... 97% 33.2M 1s
491600K .......... .......... .......... .......... .......... 97% 31.2M 1s
491650K .......... .......... .......... .......... .......... 97% 21.3M 1s
491700K .......... .......... .......... .......... .......... 97% 29.3M 1s
491750K .......... .......... .......... .......... .......... 97% 30.8M 1s
491800K .......... .......... .......... .......... .......... 97% 28.1M 1s
491850K .......... .......... .......... .......... .......... 97% 18.0M 1s
491900K .......... .......... .......... .......... .......... 97% 21.8M 1s
491950K .......... .......... .......... .......... .......... 97% 31.8M 1s
492000K .......... .......... .......... .......... .......... 97% 19.3M 1s
492050K .......... .......... .......... .......... .......... 97% 27.1M 1s
492100K .......... .......... .......... .......... .......... 97% 21.7M 1s
492150K .......... .......... .......... .......... .......... 97% 26.6M 1s
492200K .......... .......... .......... .......... .......... 97% 14.8M 1s
492250K .......... .......... .......... .......... .......... 97% 14.0M 1s
492300K .......... .......... .......... .......... .......... 97% 13.2M 1s
492350K .......... .......... .......... .......... .......... 97% 12.8M 1s
492400K .......... .......... .......... .......... .......... 97% 14.0M 1s
492450K .......... .......... .......... .......... .......... 97% 13.2M 1s
492500K .......... .......... .......... .......... .......... 97% 14.7M 1s
492550K .......... .......... .......... .......... .......... 97% 15.7M 1s
492600K .......... .......... .......... .......... .......... 97% 11.6M 1s
492650K .......... .......... .......... .......... .......... 97% 16.7M 1s
492700K .......... .......... .......... .......... .......... 97% 13.0M 1s
492750K .......... .......... .......... .......... .......... 97% 15.4M 1s
492800K .......... .......... .......... .......... .......... 97% 15.3M 1s
492850K .......... .......... .......... .......... .......... 97% 24.1M 1s
492900K .......... .......... .......... .......... .......... 97% 22.6M 1s
492950K .......... .......... .......... .......... .......... 97% 23.5M 1s
493000K .......... .......... .......... .......... .......... 97% 12.9M 1s
493050K .......... .......... .......... .......... .......... 97%  115M 1s
493100K .......... .......... .......... .......... .......... 97% 11.3M 1s
493150K .......... .......... .......... .......... .......... 97% 77.6M 1s
493200K .......... .......... .......... .......... .......... 97% 21.6M 1s
493250K .......... .......... .......... .......... .......... 97% 16.6M 1s
493300K .......... .......... .......... .......... .......... 97% 21.2M 1s
493350K .......... .......... .......... .......... .......... 97% 18.8M 1s
493400K .......... .......... .......... .......... .......... 97% 16.1M 1s
493450K .......... .......... .......... .......... .......... 97% 18.2M 1s
493500K .......... .......... .......... .......... .......... 98% 19.2M 1s
493550K .......... .......... .......... .......... .......... 98% 25.1M 1s
493600K .......... .......... .......... .......... .......... 98% 19.7M 1s
493650K .......... .......... .......... .......... .......... 98% 21.4M 1s
493700K .......... .......... .......... .......... .......... 98% 15.7M 1s
493750K .......... .......... .......... .......... .......... 98% 22.2M 1s
493800K .......... .......... .......... .......... .......... 98% 25.2M 1s
493850K .......... .......... .......... .......... .......... 98% 16.5M 1s
493900K .......... .......... .......... .......... .......... 98% 25.2M 1s
493950K .......... .......... .......... .......... .......... 98% 29.5M 1s
494000K .......... .......... .......... .......... .......... 98% 22.6M 1s
494050K .......... .......... .......... .......... .......... 98% 24.7M 1s
494100K .......... .......... .......... .......... .......... 98% 15.7M 1s
494150K .......... .......... .......... .......... .......... 98% 68.7M 1s
494200K .......... .......... .......... .......... .......... 98% 15.8M 1s
494250K .......... .......... .......... .......... .......... 98% 13.5M 1s
494300K .......... .......... .......... .......... .......... 98% 54.9M 1s
494350K .......... .......... .......... .......... .......... 98% 19.5M 1s
494400K .......... .......... .......... .......... .......... 98% 23.5M 1s
494450K .......... .......... .......... .......... .......... 98% 22.2M 1s
494500K .......... .......... .......... .......... .......... 98% 21.6M 1s
494550K .......... .......... .......... .......... .......... 98% 16.7M 1s
494600K .......... .......... .......... .......... .......... 98% 18.2M 1s
494650K .......... .......... .......... .......... .......... 98% 23.7M 1s
494700K .......... .......... .......... .......... .......... 98% 17.5M 1s
494750K .......... .......... .......... .......... .......... 98% 25.6M 1s
494800K .......... .......... .......... .......... .......... 98% 26.9M 1s
494850K .......... .......... .......... .......... .......... 98% 19.1M 1s
494900K .......... .......... .......... .......... .......... 98% 25.5M 1s
494950K .......... .......... .......... .......... .......... 98% 16.1M 1s
495000K .......... .......... .......... .......... .......... 98% 25.9M 1s
495050K .......... .......... .......... .......... .......... 98% 23.9M 1s
495100K .......... .......... .......... .......... .......... 98% 75.1M 1s
495150K .......... .......... .......... .......... .......... 98% 33.7M 1s
495200K .......... .......... .......... .......... .......... 98% 76.1M 1s
495250K .......... .......... .......... .......... .......... 98% 42.5M 1s
495300K .......... .......... .......... .......... .......... 98% 73.3M 1s
495350K .......... .......... .......... .......... .......... 98% 16.8M 1s
495400K .......... .......... .......... .......... .......... 98% 60.3M 1s
495450K .......... .......... .......... .......... .......... 98% 19.3M 1s
495500K .......... .......... .......... .......... .......... 98% 41.8M 1s
495550K .......... .......... .......... .......... .......... 98% 23.4M 1s
495600K .......... .......... .......... .......... .......... 98% 41.5M 1s
495650K .......... .......... .......... .......... .......... 98% 56.0M 1s
495700K .......... .......... .......... .......... .......... 98% 15.6M 1s
495750K .......... .......... .......... .......... .......... 98% 19.0M 1s
495800K .......... .......... .......... .......... .......... 98% 23.8M 1s
495850K .......... .......... .......... .......... .......... 98% 18.0M 1s
495900K .......... .......... .......... .......... .......... 98% 19.8M 1s
495950K .......... .......... .......... .......... .......... 98% 23.4M 1s
496000K .......... .......... .......... .......... .......... 98% 20.1M 1s
496050K .......... .......... .......... .......... .......... 98% 22.6M 1s
496100K .......... .......... .......... .......... .......... 98% 18.0M 1s
496150K .......... .......... .......... .......... .......... 98% 22.5M 1s
496200K .......... .......... .......... .......... .......... 98% 14.9M 1s
496250K .......... .......... .......... .......... .......... 98% 31.9M 0s
496300K .......... .......... .......... .......... .......... 98% 18.9M 0s
496350K .......... .......... .......... .......... .......... 98% 17.2M 0s
496400K .......... .......... .......... .......... .......... 98% 9.14M 0s
496450K .......... .......... .......... .......... .......... 98% 38.3M 0s
496500K .......... .......... .......... .......... .......... 98%  470M 0s
496550K .......... .......... .......... .......... .......... 98% 11.6M 0s
496600K .......... .......... .......... .......... .......... 98%  452M 0s
496650K .......... .......... .......... .......... .......... 98% 40.6M 0s
496700K .......... .......... .......... .......... .......... 98% 26.3M 0s
496750K .......... .......... .......... .......... .......... 98% 18.3M 0s
496800K .......... .......... .......... .......... .......... 98% 26.3M 0s
496850K .......... .......... .......... .......... .......... 98% 16.5M 0s
496900K .......... .......... .......... .......... .......... 98% 25.3M 0s
496950K .......... .......... .......... .......... .......... 98% 22.5M 0s
497000K .......... .......... .......... .......... .......... 98% 25.3M 0s
497050K .......... .......... .......... .......... .......... 98% 21.3M 0s
497100K .......... .......... .......... .......... .......... 98% 18.1M 0s
497150K .......... .......... .......... .......... .......... 98% 24.0M 0s
497200K .......... .......... .......... .......... .......... 98% 18.2M 0s
497250K .......... .......... .......... .......... .......... 98% 18.9M 0s
497300K .......... .......... .......... .......... .......... 98% 29.2M 0s
497350K .......... .......... .......... .......... .......... 98% 24.8M 0s
497400K .......... .......... .......... .......... .......... 98% 21.2M 0s
497450K .......... .......... .......... .......... .......... 98% 15.3M 0s
497500K .......... .......... .......... .......... .......... 98% 12.3M 0s
497550K .......... .......... .......... .......... .......... 98% 22.6M 0s
497600K .......... .......... .......... .......... .......... 98% 22.6M 0s
497650K .......... .......... .......... .......... .......... 98% 15.2M 0s
497700K .......... .......... .......... .......... .......... 98% 48.1M 0s
497750K .......... .......... .......... .......... .......... 98% 38.8M 0s
497800K .......... .......... .......... .......... .......... 98% 24.5M 0s
497850K .......... .......... .......... .......... .......... 98% 31.2M 0s
497900K .......... .......... .......... .......... .......... 98% 23.9M 0s
497950K .......... .......... .......... .......... .......... 98% 28.0M 0s
498000K .......... .......... .......... .......... .......... 98% 28.1M 0s
498050K .......... .......... .......... .......... .......... 98% 23.7M 0s
498100K .......... .......... .......... .......... .......... 98% 20.9M 0s
498150K .......... .......... .......... .......... .......... 98% 29.6M 0s
498200K .......... .......... .......... .......... .......... 98% 17.4M 0s
498250K .......... .......... .......... .......... .......... 98% 33.5M 0s
498300K .......... .......... .......... .......... .......... 98% 18.8M 0s
498350K .......... .......... .......... .......... .......... 98% 16.9M 0s
498400K .......... .......... .......... .......... .......... 98% 21.5M 0s
498450K .......... .......... .......... .......... .......... 98% 17.1M 0s
498500K .......... .......... .......... .......... .......... 98% 21.1M 0s
498550K .......... .......... .......... .......... .......... 99% 16.6M 0s
498600K .......... .......... .......... .......... .......... 99% 15.4M 0s
498650K .......... .......... .......... .......... .......... 99% 7.42M 0s
498700K .......... .......... .......... .......... .......... 99% 13.7M 0s
498750K .......... .......... .......... .......... .......... 99% 11.3M 0s
498800K .......... .......... .......... .......... .......... 99% 11.7M 0s
498850K .......... .......... .......... .......... .......... 99% 8.93M 0s
498900K .......... .......... .......... .......... .......... 99% 11.3M 0s
498950K .......... .......... .......... .......... .......... 99% 9.87M 0s
499000K .......... .......... .......... .......... .......... 99% 11.0M 0s
499050K .......... .......... .......... .......... .......... 99% 10.6M 0s
499100K .......... .......... .......... .......... .......... 99% 16.1M 0s
499150K .......... .......... .......... .......... .......... 99% 15.3M 0s
499200K .......... .......... .......... .......... .......... 99% 25.7M 0s
499250K .......... .......... .......... .......... .......... 99% 21.6M 0s
499300K .......... .......... .......... .......... .......... 99% 27.1M 0s
499350K .......... .......... .......... .......... .......... 99% 25.5M 0s
499400K .......... .......... .......... .......... .......... 99% 20.2M 0s
499450K .......... .......... .......... .......... .......... 99% 21.9M 0s
499500K .......... .......... .......... .......... .......... 99% 18.4M 0s
499550K .......... .......... .......... .......... .......... 99% 29.1M 0s
499600K .......... .......... .......... .......... .......... 99% 17.5M 0s
499650K .......... .......... .......... .......... .......... 99% 28.9M 0s
499700K .......... .......... .......... .......... .......... 99% 18.2M 0s
499750K .......... .......... .......... .......... .......... 99% 26.9M 0s
499800K .......... .......... .......... .......... .......... 99% 18.9M 0s
499850K .......... .......... .......... .......... .......... 99% 22.5M 0s
499900K .......... .......... .......... .......... .......... 99% 25.4M 0s
499950K .......... .......... .......... .......... .......... 99% 22.7M 0s
500000K .......... .......... .......... .......... .......... 99% 19.7M 0s
500050K .......... .......... .......... .......... .......... 99% 22.6M 0s
500100K .......... .......... .......... .......... .......... 99% 25.2M 0s
500150K .......... .......... .......... .......... .......... 99% 46.3M 0s
500200K .......... .......... .......... .......... .......... 99% 21.4M 0s
500250K .......... .......... .......... .......... .......... 99% 10.7M 0s
500300K .......... .......... .......... .......... .......... 99%  465M 0s
500350K .......... .......... .......... .......... .......... 99%  456M 0s
500400K .......... .......... .......... .......... .......... 99% 30.3M 0s
500450K .......... .......... .......... .......... .......... 99% 18.5M 0s
500500K .......... .......... .......... .......... .......... 99% 20.3M 0s
500550K .......... .......... .......... .......... .......... 99% 15.2M 0s
500600K .......... .......... .......... .......... .......... 99%  163M 0s
500650K .......... .......... .......... .......... .......... 99% 37.7M 0s
500700K .......... .......... .......... .......... .......... 99% 20.9M 0s
500750K .......... .......... .......... .......... .......... 99% 23.5M 0s
500800K .......... .......... .......... .......... .......... 99% 34.5M 0s
500850K .......... .......... .......... .......... .......... 99% 25.2M 0s
500900K .......... .......... .......... .......... .......... 99% 26.7M 0s
500950K .......... .......... .......... .......... .......... 99% 22.2M 0s
501000K .......... .......... .......... .......... .......... 99% 24.1M 0s
501050K .......... .......... .......... .......... .......... 99% 31.5M 0s
501100K .......... .......... .......... .......... .......... 99% 22.9M 0s
501150K .......... .......... .......... .......... .......... 99% 31.8M 0s
501200K .......... .......... .......... .......... .......... 99% 28.6M 0s
501250K .......... .......... .......... .......... .......... 99% 28.0M 0s
501300K .......... .......... .......... .......... .......... 99% 41.1M 0s
501350K .......... .......... .......... .......... .......... 99% 23.6M 0s
501400K .......... .......... .......... .......... .......... 99% 25.4M 0s
501450K .......... .......... .......... .......... .......... 99% 25.2M 0s
501500K .......... .......... .......... .......... .......... 99% 31.5M 0s
501550K .......... .......... .......... .......... .......... 99% 28.6M 0s
501600K .......... .......... .......... .......... .......... 99% 38.3M 0s
501650K .......... .......... .......... .......... .......... 99% 42.2M 0s
501700K .......... .......... .......... .......... .......... 99% 76.3M 0s
501750K .......... .......... .......... .......... .......... 99% 14.5M 0s
501800K .......... .......... .......... .......... .......... 99% 61.9M 0s
501850K .......... .......... .......... .......... .......... 99%  410M 0s
501900K .......... .......... .......... .......... .......... 99% 89.9M 0s
501950K .......... .......... .......... .......... .......... 99%  444M 0s
502000K .......... .......... .......... .......... .......... 99% 28.8M 0s
502050K .......... .......... .......... .......... .......... 99%  410M 0s
502100K .......... .......... .......... .......... .......... 99% 33.1M 0s
502150K .......... .......... .......... .......... .......... 99% 33.6M 0s
502200K .......... .......... .......... .......... .......... 99% 43.2M 0s
502250K .......... .......... .......... .......... .......... 99% 31.9M 0s
502300K .......... .......... .......... .......... .......... 99% 30.9M 0s
502350K .......... .......... .......... .......... .......... 99% 34.2M 0s
502400K .......... .......... .......... .......... .......... 99% 27.0M 0s
502450K .......... .......... .......... .......... .......... 99% 38.0M 0s
502500K .......... .......... .......... .......... .......... 99% 33.7M 0s
502550K .......... .......... .......... .......... .......... 99% 31.4M 0s
502600K .......... .......... .......... .......... .......... 99% 44.9M 0s
502650K .......... .......... .......... .......... .......... 99% 37.0M 0s
502700K .......... .......... .......... .......... .......... 99% 29.6M 0s
502750K .......... .......... .......... .......... .......... 99% 42.8M 0s
502800K .......... .......... .......... .......... .......... 99% 45.1M 0s
502850K .......... .......... .......... .......... .......... 99% 29.1M 0s
502900K .......... .......... .......... .......... .......... 99% 31.9M 0s
502950K .......... .......... .......... .......... .......... 99% 31.2M 0s
503000K .......... .......... .......... .......... .......... 99% 34.6M 0s
503050K .......... .......... .......... .......... .......... 99% 42.1M 0s
503100K .......... .......... .......... .......... .......... 99% 27.5M 0s
503150K .......... .......... .......... .......... .......... 99% 37.2M 0s
503200K .......... .......... .......... .......... .......... 99% 33.8M 0s
503250K .......... .......... .......... .......... .......... 99% 25.8M 0s
503300K .......... .......... .......... .......... .......... 99% 23.5M 0s
503350K .......... .......... .......... .......... .......... 99% 13.3M 0s
503400K .......... .......... .......... .......... .......... 99% 18.8M 0s
503450K .......... .......... .......... .......... .......... 99% 37.7M 0s
503500K .......... .......... .......... .......... .......... 99% 13.8M 0s
503550K .......... .......... .......... .......... .......... 99% 31.3M 0s
503600K ...                                                   100%  180M=34s

2024-03-06 20:31:15 (14.4 MB/s) - ‘ESPbeta-macos-arm64.tgz’ saved [515690371/515690371]

+ tar -xf ESPbeta-macos-arm64.tgz
+ cd ESPbeta
+ rm -rf /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Slugs
++ uname -a
+ [[ Darwin VIGGEN.MIT.EDU 23.3.0 Darwin Kernel Version 23.3.0: Wed Dec 20 21:30:27 PST 2023; root:xnu-10002.81.5~7/RELEASE_ARM64_T8103 arm64 == *\D\a\r\w\i\n* ]]
+ ./setup.command
Custom icon assigned to '/Users/jenkins/Desktop/ESP125.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/esp_logo.png'.
Custom icon assigned to '/Users/jenkins/Desktop/runESP125.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/esp_logo.png'.
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/idle3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/pyftsubset'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/test_op4'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/ttx'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/wingproj'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/test_op2'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/pip3'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/test_bdf'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/aggregate_profile.pl'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/imageio_remove_bin'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/undill'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/bdf'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/run_om_test'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/f90nml'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/profile2mat.pl'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/webview'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/fonttools'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/openmdao'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/pyNastranGUI'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/f2py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/pip'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/pydoc3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/2to3-3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/imageio_download_bin'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/pip3.11'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/test_pynastrangui'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/numba'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/normalizer'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/virtualenv'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/reset_notebook'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/get_gprof'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/format_converter'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/qtpy'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/pyftmerge'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/python3.11-config'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/f06'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/get_objgraph'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/lib/python3.11/config-3.11-darwin/Makefile'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/lib/python3.11/config-3.11-darwin/python-config.py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/lib/pkgconfig/python-3.11-embed.pc'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/lib/pkgconfig/python-3.11.pc'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/lib/python3.11/_sysconfigdata__darwin_darwin.py'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/lib/python3.11/site-packages/mpi4py/mpi.cfg'
Patching 'bin/ompi_info'
Patching 'bin/orte-info'
Patching 'lib/libmpi.40.dylib'
Patching 'lib/libopen-pal.40.dylib'
Patching 'lib/openmpi/mca_io_romio321.so'
Patching 'lib/openmpi/mca_pmix_pmix3x.so'
Patching 'lib/pkgconfig/ompi-c.pc'
Patching 'lib/pkgconfig/ompi-cxx.pc'
Patching 'lib/pkgconfig/ompi-fort.pc'
Patching 'lib/pkgconfig/ompi.pc'
Patching 'lib/pkgconfig/orte.pc'
Patching 'lib/pkgconfig/pmix.pc'
Patching 'share/openmpi/mpic++-wrapper-data.txt'
Patching 'share/openmpi/mpicc-wrapper-data.txt'
Patching 'share/openmpi/mpifort-wrapper-data.txt'
Patching 'share/openmpi/ortecc-wrapper-data.txt'
+ rm -rf '/Users/jenkins/Desktop/*ESPbeta.command'
+ source /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=DARWIN64
++ ESP_ARCH=DARWIN64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad
++ ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad
++ export CASROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/OpenCASCADE-7.8.0
++ CASROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/OpenCASCADE-7.8.0
++ export CARARCH=.
++ CARARCH=.
++ export CASREV=7.8
++ CASREV=7.8
++ export PATH=.:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=.:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONINC=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/include/python3.11
++ PYTHONINC=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/include/python3.11
++ export 'PYTHONLIB=-L/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/lib -lpython3.11'
++ PYTHONLIB='-L/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/lib -lpython3.11'
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/lib:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/lib/python3.11/site-packages:/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/lib:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/lib/python3.11/site-packages:/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/udunits/udunits2.xml
++ export CAPS_GLYPH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ export 'SLUGS_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/SLUGS/Slugs.html'
++ SLUGS_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/SLUGS/Slugs.html'
++ export 'ESP_START=open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/ESP-localhost7681.html'
++ ESP_START='open -a /Applications/Safari.app;sleep 1;open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/ESP-localhost7681.html'
++ export 'WV_START=open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/wvClient/wv.html'
++ WV_START='open -a /Applications/Safari.app /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/wvClient/wv.html'
+ which python
/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/python
+ python --version
Python 3.11.6
+ export CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data
+ CSMDATA=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin
++ uname -a
+ [[ Darwin VIGGEN.MIT.EDU 23.3.0 Darwin Kernel Version 23.3.0: Wed Dec 20 21:30:27 PST 2023; root:xnu-10002.81.5~7/RELEASE_ARM64_T8103 arm64 == *\D\a\r\w\i\n* ]]
+ sed -i '' '/.*capsExamples.*/d' /Users/jenkins/workspace/ESP_bPreBuilt/Verification.sh
+ bash -ex /Users/jenkins/workspace/ESP_bPreBuilt/Verification.sh
+ expectSuccess 01 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/expressions.vfy", so verification is being skipped
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000152 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:169]]
        ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,0,999)"
ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set)
    --> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000158 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:176]]
        ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,14,999)"
ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set)
    --> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000164 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:183]]
        iend must not be less than ibeg when evaluating "slice(e3,4,-1)"
ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set)
    --> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (illegal_pmtr_index) in Branch Brch_000317 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:384]]
        index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000332 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:402]]
        index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000346 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:418]]
        row index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000360 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:434]]
        row index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000367 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:442]]
        row index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000374 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:450]]
        column index must be between 1 and 3
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000381 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:458]]
        column index must be between 1 and 3
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (UNKNOWN) in Branch Brch_001805 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:1914]]
        signal 1 thrown by user
    --> catching signal 1 (UNKNOWN)
ERROR:: (illegal_value) in Branch Brch_001813 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:1924]]
        vertex and base must be different
    --> catching signal -225 (illegal_value)
==> serveESP completed successfully with no verification data

real	0m1.920s
user	0m0.122s
sys	0m0.016s
+ set +x

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

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

real	0m0.229s
user	0m0.256s
sys	0m0.030s
+ set +x

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

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

real	0m1.129s
user	0m1.787s
sys	0m0.665s
+ set +x

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

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

real	0m0.287s
user	0m0.326s
sys	0m0.031s
+ set +x

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

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

real	0m0.348s
user	0m0.486s
sys	0m0.057s
+ set +x

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

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

real	0m0.325s
user	0m0.461s
sys	0m0.017s
+ set +x

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

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

real	0m1.630s
user	0m3.090s
sys	0m0.318s
+ set +x

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

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

real	0m12.073s
user	0m23.090s
sys	0m1.334s
+ set +x

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

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

real	0m0.309s
user	0m0.379s
sys	0m0.012s
+ set +x

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

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

real	0m13.801s
user	0m43.137s
sys	0m22.875s
+ set +x

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

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

real	0m0.207s
user	0m0.217s
sys	0m0.024s
+ set +x

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

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

real	0m0.378s
user	0m0.592s
sys	0m0.006s
+ set +x

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

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

real	0m0.150s
user	0m0.163s
sys	0m0.006s
+ set +x

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

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

real	0m0.267s
user	0m0.331s
sys	0m0.009s
+ set +x

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

+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP/testEGADS
+ make test
python --version
Python 3.11.6
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 0.996s

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

real	0m3.277s
user	0m5.293s
sys	0m0.089s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/pyESP/testCAPS
+ make test
python --version
Python 3.11.6
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 = 147
	Number of elements = 290
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 290
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 290
	Combined Number of elements = 572
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 572
	Combined Elemental Quad4 = 0

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

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

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

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

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

----------------------------------------------------------------------
Ran 100 tests in 7.874s

OK
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/
+ make test
python --version
Python 3.11.6
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.001   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      =      1086      2174
AFLR2 IG : Nodes, Faces      =      1087      2176
AFLR2 IG : Nodes, Faces      =      1321      2644
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1421      2844
AFLR2 IG : Nodes, Faces      =      1521      3044
AFLR2 IG : Nodes, Faces      =      1621      3244
AFLR2 IG : Nodes, Faces      =      1721      3444
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1821      3644
AFLR2 IG : Nodes, Faces      =      1921      3844
AFLR2 IG : Nodes, Faces      =      2021      4044
AFLR2 IG : Nodes, Faces      =      2121      4244
AFLR2 IG : Nodes, Faces      =      2221      4444
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.004   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4284      6324
AFLR2 GG : Nodes, Faces      =      6145     10046
AFLR2 GG : Nodes, Faces      =      7886     13528
AFLR2 GG : Nodes, Faces      =      9454     16664
AFLR2 GG : Nodes, Faces      =     10741     19238
AFLR2 GG : Nodes, Faces      =     11943     21642
AFLR2 GG : Nodes, Faces      =     13066     23888
AFLR2 GG : Nodes, Faces      =     14097     25950
AFLR2 GG : Nodes, Faces      =     15067     27890
AFLR2 GG : Nodes, Faces      =     15974     29704
AFLR2 GG : Nodes, Faces      =     16822     31400
AFLR2 GG : Nodes, Faces      =     17616     32988
AFLR2 GG : Nodes, Faces      =     18347     34450
AFLR2 GG : Nodes, Faces      =     19005     35766
AFLR2 GG : Nodes, Faces      =     19620     36996
AFLR2 GG : Nodes, Faces      =     20189     38134
AFLR2 GG : Nodes, Faces      =     20718     39192
AFLR2 GG : Nodes, Faces      =     21211     40178
AFLR2 GG : Nodes, Faces      =     21668     41092
AFLR2 GG : Nodes, Faces      =     22096     41948
AFLR2 GG : Nodes, Faces      =     22480     42716
AFLR2 GG : Nodes, Faces      =     22835     43426
AFLR2 GG : Nodes, Faces      =     23135     44026
AFLR2 GG : Nodes, Faces      =     23375     44506
AFLR2 GG : Nodes, Faces      =     23584     44924
AFLR2 GG : Nodes, Faces      =     23776     45308
AFLR2 GG : Nodes, Faces      =     23937     45630
AFLR2 GG : Nodes, Faces      =     24040     45836
AFLR2 GG : Nodes, Faces      =     24141     46038
AFLR2 GG : Nodes, Faces      =     24236     46228
AFLR2 GG : Nodes, Faces      =     24313     46382
AFLR2 GG : Nodes, Faces      =     24371     46498
AFLR2 GG : Nodes, Faces      =     24418     46592
AFLR2 GG : Nodes, Faces      =     24438     46632
AFLR2 GG : Nodes, Faces      =     24445     46646
AFLR2 GG : Nodes, Faces      =     24446     46648
 
AFLR2    : CPU Time          =     0.035   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     24446     46648
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 24446
Number of elements = 48892
Number of tris = 46648
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      =       850      1702
AFLR2 IG : Nodes, Faces      =       851      1704
AFLR2 IG : Nodes, Faces      =       892      1786
AFLR2 IG : Nodes, Faces      =      1301      2604
AFLR2 IG : Nodes, Faces      =      1338      2678
AFLR2 IG : Nodes, Faces      =      1401      2804
AFLR2 IG : Nodes, Faces      =      1501      3004
AFLR2 IG : Nodes, Faces      =      1601      3204
AFLR2 IG : Nodes, Faces      =      1701      3404
AFLR2 IG : Nodes, Faces      =      1784      3570
AFLR2 IG : Nodes, Faces      =      1801      3604
AFLR2 IG : Nodes, Faces      =      1901      3804
AFLR2 IG : Nodes, Faces      =      2001      4004
AFLR2 IG : Nodes, Faces      =      2101      4204
AFLR2 IG : Nodes, Faces      =      2201      4404
AFLR2 IG : Nodes, Faces      =      2224      4450
AFLR2 IG : Nodes, Faces      =      2228      4450
AFLR2 IG : Nodes, Faces      =      2224      2224
 
AFLR2    : CPU Time          =     0.004   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4125      6026
AFLR2 GG : Nodes, Faces      =      5678      9132
AFLR2 GG : Nodes, Faces      =      6935     11646
AFLR2 GG : Nodes, Faces      =      8014     13804
AFLR2 GG : Nodes, Faces      =      8951     15678
AFLR2 GG : Nodes, Faces      =      9771     17318
AFLR2 GG : Nodes, Faces      =     10475     18726
AFLR2 GG : Nodes, Faces      =     11059     19894
AFLR2 GG : Nodes, Faces      =     11570     20916
AFLR2 GG : Nodes, Faces      =     12009     21794
AFLR2 GG : Nodes, Faces      =     12391     22558
AFLR2 GG : Nodes, Faces      =     12726     23228
AFLR2 GG : Nodes, Faces      =     12997     23770
AFLR2 GG : Nodes, Faces      =     13221     24218
AFLR2 GG : Nodes, Faces      =     13414     24604
AFLR2 GG : Nodes, Faces      =     13547     24870
AFLR2 GG : Nodes, Faces      =     13643     25062
AFLR2 GG : Nodes, Faces      =     13711     25198
AFLR2 GG : Nodes, Faces      =     13758     25292
AFLR2 GG : Nodes, Faces      =     13790     25356
AFLR2 GG : Nodes, Faces      =     13806     25388
AFLR2 GG : Nodes, Faces      =     13809     25394
AFLR2 GG : Nodes, Faces      =     13810     25396
 
AFLR2    : CPU Time          =     0.018   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     13810     25396
 
AFLR2    : CPU Time          =     0.002   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 13810
Number of elements = 27620
Number of tris = 25396
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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      =      1086      2174
AFLR2 IG : Nodes, Faces      =      1087      2176
AFLR2 IG : Nodes, Faces      =      1321      2644
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1421      2844
AFLR2 IG : Nodes, Faces      =      1521      3044
AFLR2 IG : Nodes, Faces      =      1621      3244
AFLR2 IG : Nodes, Faces      =      1721      3444
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1821      3644
AFLR2 IG : Nodes, Faces      =      1921      3844
AFLR2 IG : Nodes, Faces      =      2021      4044
AFLR2 IG : Nodes, Faces      =      2121      4244
AFLR2 IG : Nodes, Faces      =      2221      4444
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.004   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4284      6324
AFLR2 GG : Nodes, Faces      =      6145     10046
AFLR2 GG : Nodes, Faces      =      7886     13528
AFLR2 GG : Nodes, Faces      =      9454     16664
AFLR2 GG : Nodes, Faces      =     10741     19238
AFLR2 GG : Nodes, Faces      =     11943     21642
AFLR2 GG : Nodes, Faces      =     13066     23888
AFLR2 GG : Nodes, Faces      =     14097     25950
AFLR2 GG : Nodes, Faces      =     15067     27890
AFLR2 GG : Nodes, Faces      =     15974     29704
AFLR2 GG : Nodes, Faces      =     16822     31400
AFLR2 GG : Nodes, Faces      =     17616     32988
AFLR2 GG : Nodes, Faces      =     18347     34450
AFLR2 GG : Nodes, Faces      =     19005     35766
AFLR2 GG : Nodes, Faces      =     19620     36996
AFLR2 GG : Nodes, Faces      =     20189     38134
AFLR2 GG : Nodes, Faces      =     20718     39192
AFLR2 GG : Nodes, Faces      =     21211     40178
AFLR2 GG : Nodes, Faces      =     21668     41092
AFLR2 GG : Nodes, Faces      =     22096     41948
AFLR2 GG : Nodes, Faces      =     22480     42716
AFLR2 GG : Nodes, Faces      =     22835     43426
AFLR2 GG : Nodes, Faces      =     23135     44026
AFLR2 GG : Nodes, Faces      =     23375     44506
AFLR2 GG : Nodes, Faces      =     23584     44924
AFLR2 GG : Nodes, Faces      =     23776     45308
AFLR2 GG : Nodes, Faces      =     23937     45630
AFLR2 GG : Nodes, Faces      =     24040     45836
AFLR2 GG : Nodes, Faces      =     24141     46038
AFLR2 GG : Nodes, Faces      =     24236     46228
AFLR2 GG : Nodes, Faces      =     24313     46382
AFLR2 GG : Nodes, Faces      =     24371     46498
AFLR2 GG : Nodes, Faces      =     24418     46592
AFLR2 GG : Nodes, Faces      =     24438     46632
AFLR2 GG : Nodes, Faces      =     24445     46646
AFLR2 GG : Nodes, Faces      =     24446     46648
 
AFLR2    : CPU Time          =     0.035   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     24446     46648
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 24446
Number of elements = 48892
Number of tris = 46648
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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      =       850      1702
AFLR2 IG : Nodes, Faces      =       851      1704
AFLR2 IG : Nodes, Faces      =       892      1786
AFLR2 IG : Nodes, Faces      =      1301      2604
AFLR2 IG : Nodes, Faces      =      1338      2678
AFLR2 IG : Nodes, Faces      =      1401      2804
AFLR2 IG : Nodes, Faces      =      1501      3004
AFLR2 IG : Nodes, Faces      =      1601      3204
AFLR2 IG : Nodes, Faces      =      1701      3404
AFLR2 IG : Nodes, Faces      =      1784      3570
AFLR2 IG : Nodes, Faces      =      1801      3604
AFLR2 IG : Nodes, Faces      =      1901      3804
AFLR2 IG : Nodes, Faces      =      2001      4004
AFLR2 IG : Nodes, Faces      =      2101      4204
AFLR2 IG : Nodes, Faces      =      2201      4404
AFLR2 IG : Nodes, Faces      =      2224      4450
AFLR2 IG : Nodes, Faces      =      2228      4450
AFLR2 IG : Nodes, Faces      =      2224      2224
 
AFLR2    : CPU Time          =     0.004   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4125      6026
AFLR2 GG : Nodes, Faces      =      5678      9132
AFLR2 GG : Nodes, Faces      =      6935     11646
AFLR2 GG : Nodes, Faces      =      8014     13804
AFLR2 GG : Nodes, Faces      =      8951     15678
AFLR2 GG : Nodes, Faces      =      9771     17318
AFLR2 GG : Nodes, Faces      =     10475     18726
AFLR2 GG : Nodes, Faces      =     11059     19894
AFLR2 GG : Nodes, Faces      =     11570     20916
AFLR2 GG : Nodes, Faces      =     12009     21794
AFLR2 GG : Nodes, Faces      =     12391     22558
AFLR2 GG : Nodes, Faces      =     12726     23228
AFLR2 GG : Nodes, Faces      =     12997     23770
AFLR2 GG : Nodes, Faces      =     13221     24218
AFLR2 GG : Nodes, Faces      =     13414     24604
AFLR2 GG : Nodes, Faces      =     13547     24870
AFLR2 GG : Nodes, Faces      =     13643     25062
AFLR2 GG : Nodes, Faces      =     13711     25198
AFLR2 GG : Nodes, Faces      =     13758     25292
AFLR2 GG : Nodes, Faces      =     13790     25356
AFLR2 GG : Nodes, Faces      =     13806     25388
AFLR2 GG : Nodes, Faces      =     13809     25394
AFLR2 GG : Nodes, Faces      =     13810     25396
 
AFLR2    : CPU Time          =     0.018   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     13810     25396
 
AFLR2    : CPU Time          =     0.002   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 13810
Number of elements = 27620
Number of tris = 25396
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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      =      1086      2174
AFLR2 IG : Nodes, Faces      =      1087      2176
AFLR2 IG : Nodes, Faces      =      1321      2644
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1421      2844
AFLR2 IG : Nodes, Faces      =      1521      3044
AFLR2 IG : Nodes, Faces      =      1621      3244
AFLR2 IG : Nodes, Faces      =      1721      3444
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1821      3644
AFLR2 IG : Nodes, Faces      =      1921      3844
AFLR2 IG : Nodes, Faces      =      2021      4044
AFLR2 IG : Nodes, Faces      =      2121      4244
AFLR2 IG : Nodes, Faces      =      2221      4444
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.004   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4284      6324
AFLR2 GG : Nodes, Faces      =      6145     10046
AFLR2 GG : Nodes, Faces      =      7886     13528
AFLR2 GG : Nodes, Faces      =      9454     16664
AFLR2 GG : Nodes, Faces      =     10741     19238
AFLR2 GG : Nodes, Faces      =     11943     21642
AFLR2 GG : Nodes, Faces      =     13066     23888
AFLR2 GG : Nodes, Faces      =     14097     25950
AFLR2 GG : Nodes, Faces      =     15067     27890
AFLR2 GG : Nodes, Faces      =     15974     29704
AFLR2 GG : Nodes, Faces      =     16822     31400
AFLR2 GG : Nodes, Faces      =     17616     32988
AFLR2 GG : Nodes, Faces      =     18347     34450
AFLR2 GG : Nodes, Faces      =     19005     35766
AFLR2 GG : Nodes, Faces      =     19620     36996
AFLR2 GG : Nodes, Faces      =     20189     38134
AFLR2 GG : Nodes, Faces      =     20718     39192
AFLR2 GG : Nodes, Faces      =     21211     40178
AFLR2 GG : Nodes, Faces      =     21668     41092
AFLR2 GG : Nodes, Faces      =     22096     41948
AFLR2 GG : Nodes, Faces      =     22480     42716
AFLR2 GG : Nodes, Faces      =     22835     43426
AFLR2 GG : Nodes, Faces      =     23135     44026
AFLR2 GG : Nodes, Faces      =     23375     44506
AFLR2 GG : Nodes, Faces      =     23584     44924
AFLR2 GG : Nodes, Faces      =     23776     45308
AFLR2 GG : Nodes, Faces      =     23937     45630
AFLR2 GG : Nodes, Faces      =     24040     45836
AFLR2 GG : Nodes, Faces      =     24141     46038
AFLR2 GG : Nodes, Faces      =     24236     46228
AFLR2 GG : Nodes, Faces      =     24313     46382
AFLR2 GG : Nodes, Faces      =     24371     46498
AFLR2 GG : Nodes, Faces      =     24418     46592
AFLR2 GG : Nodes, Faces      =     24438     46632
AFLR2 GG : Nodes, Faces      =     24445     46646
AFLR2 GG : Nodes, Faces      =     24446     46648
 
AFLR2    : CPU Time          =     0.035   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     24446     46648
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 24446
Number of elements = 48892
Number of tris = 46648
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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      =        38        78
AFLR2 IG : Nodes, Faces      =        39        80
AFLR2 IG : Nodes, Faces      =        40        82
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      =       106       164
AFLR2 GG : Nodes, Faces      =       120       192
AFLR2 GG : Nodes, Faces      =       132       216
AFLR2 GG : Nodes, Faces      =       143       238
AFLR2 GG : Nodes, Faces      =       154       260
AFLR2 GG : Nodes, Faces      =       165       282
AFLR2 GG : Nodes, Faces      =       174       300
AFLR2 GG : Nodes, Faces      =       181       314
AFLR2 GG : Nodes, Faces      =       183       318
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =       183       318
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 183
Number of elements = 366
Number of tris = 318
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       316       634
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =       344       344
AFLR2 GG : Nodes, Faces      =       680      1016
AFLR2 GG : Nodes, Faces      =      1009      1674
AFLR2 GG : Nodes, Faces      =      1333      2322
AFLR2 GG : Nodes, Faces      =      1650      2956
AFLR2 GG : Nodes, Faces      =      1957      3570
AFLR2 GG : Nodes, Faces      =      2258      4172
AFLR2 GG : Nodes, Faces      =      2548      4752
AFLR2 GG : Nodes, Faces      =      2831      5318
AFLR2 GG : Nodes, Faces      =      3102      5860
AFLR2 GG : Nodes, Faces      =      3364      6384
AFLR2 GG : Nodes, Faces      =      3614      6884
AFLR2 GG : Nodes, Faces      =      3830      7316
AFLR2 GG : Nodes, Faces      =      4037      7730
AFLR2 GG : Nodes, Faces      =      4229      8114
AFLR2 GG : Nodes, Faces      =      4415      8486
AFLR2 GG : Nodes, Faces      =      4594      8844
AFLR2 GG : Nodes, Faces      =      4763      9182
AFLR2 GG : Nodes, Faces      =      4926      9508
AFLR2 GG : Nodes, Faces      =      5086      9828
AFLR2 GG : Nodes, Faces      =      5239     10134
AFLR2 GG : Nodes, Faces      =      5385     10426
AFLR2 GG : Nodes, Faces      =      5529     10714
AFLR2 GG : Nodes, Faces      =      5669     10994
AFLR2 GG : Nodes, Faces      =      5812     11280
AFLR2 GG : Nodes, Faces      =      5943     11542
AFLR2 GG : Nodes, Faces      =      6070     11796
AFLR2 GG : Nodes, Faces      =      6189     12034
AFLR2 GG : Nodes, Faces      =      6307     12270
AFLR2 GG : Nodes, Faces      =      6415     12486
AFLR2 GG : Nodes, Faces      =      6510     12676
AFLR2 GG : Nodes, Faces      =      6595     12846
AFLR2 GG : Nodes, Faces      =      6665     12986
AFLR2 GG : Nodes, Faces      =      6727     13110
AFLR2 GG : Nodes, Faces      =      6772     13200
AFLR2 GG : Nodes, Faces      =      6806     13268
AFLR2 GG : Nodes, Faces      =      6831     13318
AFLR2 GG : Nodes, Faces      =      6850     13356
AFLR2 GG : Nodes, Faces      =      6864     13384
AFLR2 GG : Nodes, Faces      =      6872     13400
AFLR2 GG : Nodes, Faces      =      6875     13406
AFLR2 GG : Nodes, Faces      =      6876     13408
 
AFLR2    : CPU Time          =     0.007   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      6876     13408
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 6876
Number of elements = 13752
Number of tris = 13408
Number of quad = 0

Writing TECPLOT file: pyCAPS_aflr2_Tri.dat ....
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      =       316       634
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       681      1018
AFLR2 GGp: Nodes, Faces      =      1013      1682
AFLR2 GGp: Nodes, Faces      =      1339      2334
AFLR2 GGp: Nodes, Faces      =      1652      2960
AFLR2 GGp: Nodes, Faces      =      1957      3570
AFLR2 GGp: Nodes, Faces      =      2252      4160
AFLR2 GGp: Nodes, Faces      =      2526      4708
AFLR2 GGp: Nodes, Faces      =      2809      5274
AFLR2 GGp: Nodes, Faces      =      3083      5822
AFLR2 GGp: Nodes, Faces      =      3327      6310
AFLR2 GGp: Nodes, Faces      =      3564      6784
AFLR2 GGp: Nodes, Faces      =      3788      7232
AFLR2 GGp: Nodes, Faces      =      3995      7646
AFLR2 GGp: Nodes, Faces      =      4194      8044
AFLR2 GGp: Nodes, Faces      =      4394      8444
AFLR2 GGp: Nodes, Faces      =      4585      8826
AFLR2 GGp: Nodes, Faces      =      4772      9200
AFLR2 GGp: Nodes, Faces      =      4943      9542
AFLR2 GGp: Nodes, Faces      =      5129      9914
AFLR2 GGp: Nodes, Faces      =      5293     10242
AFLR2 GGp: Nodes, Faces      =      5447     10550
AFLR2 GGp: Nodes, Faces      =      5594     10844
AFLR2 GGp: Nodes, Faces      =      5716     11088
AFLR2 GGp: Nodes, Faces      =      5830     11316
AFLR2 GGp: Nodes, Faces      =      5909     11474
AFLR2 GGp: Nodes, Faces      =      5964     11584
AFLR2 GGp: Nodes, Faces      =      6006     11668
AFLR2 GGp: Nodes, Faces      =      6025     11706
AFLR2 GGp: Nodes, Faces      =      6034     11724
 
AFLR2    : CPU Time          =     0.010   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      6034     11724
AFLR2 QI : Nodes, Faces      =      6033       454
AFLR2 QI : Nodes, Faces      =      6033      5634
AFLR2 QI : Nodes, Faces      =      6033     11722
AFLR2 QI : Nodes, Faces      =      6032       462
AFLR2 QI : Nodes, Faces      =      6032      5629
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       456
AFLR2 QI : Nodes, Faces      =      6032      5632
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       474
AFLR2 QI : Nodes, Faces      =      6032      5623
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6031       486
AFLR2 QI : Nodes, Faces      =      6031      5616
AFLR2 QI : Nodes, Faces      =      6031       488
AFLR2 QI : Nodes, Faces      =      6031      5616
 
AFLR2    : CPU Time          =     0.005   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 6031
Number of elements = 6448
Number of tris = 488
Number of quad = 5616

Writing TECPLOT file: pyCAPS_aflr2_Quad.dat ....
Finished writing TECPLOT file

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)!
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       316       634
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       681      1018
AFLR2 GGp: Nodes, Faces      =      1013      1682
AFLR2 GGp: Nodes, Faces      =      1339      2334
AFLR2 GGp: Nodes, Faces      =      1652      2960
AFLR2 GGp: Nodes, Faces      =      1957      3570
AFLR2 GGp: Nodes, Faces      =      2252      4160
AFLR2 GGp: Nodes, Faces      =      2526      4708
AFLR2 GGp: Nodes, Faces      =      2809      5274
AFLR2 GGp: Nodes, Faces      =      3083      5822
AFLR2 GGp: Nodes, Faces      =      3327      6310
AFLR2 GGp: Nodes, Faces      =      3564      6784
AFLR2 GGp: Nodes, Faces      =      3788      7232
AFLR2 GGp: Nodes, Faces      =      3995      7646
AFLR2 GGp: Nodes, Faces      =      4194      8044
AFLR2 GGp: Nodes, Faces      =      4394      8444
AFLR2 GGp: Nodes, Faces      =      4585      8826
AFLR2 GGp: Nodes, Faces      =      4772      9200
AFLR2 GGp: Nodes, Faces      =      4943      9542
AFLR2 GGp: Nodes, Faces      =      5129      9914
AFLR2 GGp: Nodes, Faces      =      5293     10242
AFLR2 GGp: Nodes, Faces      =      5447     10550
AFLR2 GGp: Nodes, Faces      =      5594     10844
AFLR2 GGp: Nodes, Faces      =      5716     11088
AFLR2 GGp: Nodes, Faces      =      5830     11316
AFLR2 GGp: Nodes, Faces      =      5909     11474
AFLR2 GGp: Nodes, Faces      =      5964     11584
AFLR2 GGp: Nodes, Faces      =      6006     11668
AFLR2 GGp: Nodes, Faces      =      6025     11706
AFLR2 GGp: Nodes, Faces      =      6034     11724
 
AFLR2    : CPU Time          =     0.010   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      6034     11724
AFLR2 QI : Nodes, Faces      =      6033       454
AFLR2 QI : Nodes, Faces      =      6033      5634
AFLR2 QI : Nodes, Faces      =      6033     11722
AFLR2 QI : Nodes, Faces      =      6032       462
AFLR2 QI : Nodes, Faces      =      6032      5629
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       456
AFLR2 QI : Nodes, Faces      =      6032      5632
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       474
AFLR2 QI : Nodes, Faces      =      6032      5623
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6031       486
AFLR2 QI : Nodes, Faces      =      6031      5616
AFLR2 QI : Nodes, Faces      =      6031       488
AFLR2 QI : Nodes, Faces      =      6031      5616
 
AFLR2    : CPU Time          =     0.005   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 6031
Number of elements = 6448
Number of tris = 488
Number of quad = 5616

Writing TECPLOT file: pyCAPS_aflr2_Test.dat ....
Finished writing TECPLOT file

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)!
ok
test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 1191
	Number of elements       = 6258
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4926
	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          = 6247
	Number of elements       = 34665
	Number of triangles      = 4438
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 30227
	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          = 13624
	Number of elements       = 76441
	Number of triangles      = 8142
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 68299
	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          = 42012
	Number of elements       = 238767
	Number of triangles      = 19898
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 218869
	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          = 4303
	Number of elements       = 23832
	Number of triangles      = 3020
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 20812
	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          = 11065
	Number of elements       = 61168
	Number of triangles      = 8630
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 52538
	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          = 10501
	Number of elements       = 58839
	Number of triangles      = 6368
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 52471
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file

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          = 88943
	Number of elements       = 499970
	Number of triangles      = 51828
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 448142
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing AFLR3 file ....
Finished writing AFLR3 file

ok
test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 17719
	Number of elements       = 100939
	Number of triangles      = 8324
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 92615
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 2560
	Number of elements       = 13640
	Number of triangles      = 2760
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 10880
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 3643
	Number of elements       = 19753
	Number of triangles      = 3396
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 16357
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 5497
	Number of elements       = 30553
	Number of triangles      = 3658
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 26895
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 4709
	Number of elements       = 26067
	Number of triangles      = 3328
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 22739
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 5505
	Number of elements       = 30555
	Number of triangles      = 3758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 26797
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 2258
	Number of elements       = 12120
	Number of triangles      = 2220
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 9900
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 3320
	Number of elements       = 17943
	Number of triangles      = 3108
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 14835
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 4387
	Number of elements       = 23813
	Number of triangles      = 3994
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 19819
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 5459
	Number of elements       = 29714
	Number of triangles      = 4882
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 24832
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 6538
	Number of elements       = 35638
	Number of triangles      = 5772
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 29866
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 7610
	Number of elements       = 41543
	Number of triangles      = 6662
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 34881
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 19842
	Number of elements       = 110111
	Number of triangles      = 15544
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 94567
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 29703
	Number of elements       = 171754
	Number of triangles      = 7670
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 164084
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 22531
	Number of elements       = 130381
	Number of triangles      = 6118
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 124263
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
 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          = 29703
	Number of elements       = 171754
	Number of triangles      = 7670
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 164084
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
 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          = 22531
	Number of elements       = 130381
	Number of triangles      = 6118
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 124263
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
 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          = 29703
	Number of elements       = 171754
	Number of triangles      = 7670
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 164084
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: test.dat ....
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          = 22531
	Number of elements       = 130381
	Number of triangles      = 6118
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 124263
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: test.dat ....
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          = 29703
	Number of elements       = 171754
	Number of triangles      = 7670
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 164084
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: test.dat ....
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          = 22531
	Number of elements       = 130381
	Number of triangles      = 6118
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 124263
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: test.dat ....
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          = 4983
	Number of elements       = 27605
	Number of triangles      = 3464
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 24141
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
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          = 6477
	Number of elements       = 36245
	Number of triangles      = 4050
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 32195
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
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          = 40466
	Number of elements       = 233749
	Number of triangles      = 12424
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 221325
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: test.dat ....
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          = 44743
	Number of elements       = 259184
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 246778
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: test.dat ....
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          = 40466
	Number of elements       = 233731
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 221325
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: test.dat ....
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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to 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 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
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:61202)
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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
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
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:61202)
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:61202)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
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:61202)
 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:61202)
 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:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 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:61202)
 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:61202)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
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:61202)
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
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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
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 = 1
Number of node elements          = 1
Number of line 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 node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 44
----------------------------
Total number of nodes    = 47
Total number of elements = 45
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

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

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

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

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

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

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

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


Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Done running Astros!
ok
test_Plate (test_astros.TestAstros.test_Plate) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes    = 25
Total number of elements = 16
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - Mach
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 3
	Objective name - C_A
	Objective name - C_N
	Objective name - C_Y
	Done getting CFD functional
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.383913  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:33:30) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:33:31) 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
   (20:33:32) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:33:34) 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
   (20:33:34) Linearizing cut-cells
   (20:33:34) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:33:34) Computing gradients
   (20:33:42) ... 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
   (20:33:43) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:33:44) 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
   (20:33:44) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:33:45) 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
   (20:33:46) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:33:47) 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
   (20:33:47) Linearizing cut-cells
   (20:33:47) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:33:47) Computing gradients
   (20:33:55) ... 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
   (20:33:56) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:33:57) 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
   (20:33:57) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:33:58) 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
   (20:33:59) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:00) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (20:34:00) Linearizing cut-cells
   (20:34:00) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:34:00) Computing gradients
   (20:34:04) ... 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
   (20:34:04) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:05) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_m
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:34:06) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:07) 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
   (20:34:07) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:08) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (20:34:08) Linearizing cut-cells
   (20:34:08) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:34:08) Computing gradients
   (20:34:12) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:34:13) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:14) 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
   (20:34:14) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:15) 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
   (20:34:16) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:17) 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
   (20:34:17) Linearizing cut-cells
   (20:34:17) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:34:17) Computing gradients
   (20:34:21) ... 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
   (20:34:21) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:22) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_M_x
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:34:23) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:24) 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
   (20:34:24) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:25) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (20:34:25) Linearizing cut-cells
   (20:34:25) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:34:25) Computing gradients
   (20:34:29) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:34:30) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:31) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
	Number of design variables - 1
	Objective name - C_M_y
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:34:31) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:32) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:34:33) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:34) 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
   (20:34:34) Linearizing cut-cells
   (20:34:34) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:34:34) Computing gradients
   (20:34:38) ... 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
   (20:34:38) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:39) 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
   (20:34:40) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:41) 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
   (20:34:41) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:42) 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
   (20:34:42) Linearizing cut-cells
   (20:34:42) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:34:42) Computing gradients
   (20:34:46) ... 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
   (20:34:47) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:48) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
ok
test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1

Getting CFD design variables.......
	Number of design variables - 2
	Design Variable name - Mach
	Design Variable name - area
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 3
	Objective name - C_A
	Objective name - C_N
	Objective name - C_Y
	Done getting CFD functional
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.383913  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:34:49) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:50) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:34:51) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:34:52) 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:                    2
   o Number of simultaneous cutter jobs:   2
   (20:34:52) Linearizing cut-cells
   (20:34:55) ... done
   o Number of simultaneous xsensit jobs:  2
   (20:34:55) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (20:35:03) ... 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
   (20:35:03) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:35:04) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
ok
test_Output (test_cbaero.TestCBAERO.test_Output) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = Wing1, index = 1
	Name = trailingEdge, index = 2

Writing FAST file ....
Finished writing FAST file

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

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
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:61202)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 9
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = nodeBody, index = 8
	Name = farfield, index = 9
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 174257000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 174257000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
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
 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 174257000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 174257000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
ok
test_bullet (test_egadsTess.TestEGADS.test_bullet) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = bullet, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_cone (test_egadsTess.TestEGADS.test_cone) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cone, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_cylinder (test_egadsTess.TestEGADS.test_cylinder) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_invalid_Mesh_Lenght_Scale (test_egadsTess.TestEGADS.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
ok
test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
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:61202)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
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:61202)
 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:61202)
 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:61202)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202)
 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:61202)
 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:61202)
 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:61202)
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:61202)
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:61202)
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
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_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
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
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    = 7802
Number of elements = 15600
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 15600
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5906
Number of elements = 11808
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 545
Number of elements = 1086
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1086
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14253
Total number of elements = 28494
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 - 14253, elements - 28494
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.085198
Creating surface mesh ...
Surface mesh seconds:  0.011377
Recovering boundaries...
Boundary recovery seconds:  0.049649
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.016841
Recovering Delaunayness...
Delaunay recovery seconds:  0.030436
Refining mesh...
  18999 insertions, added 13806 points, 712098 tetrahedra in queue.
  6326 insertions, added 2564 points, 586841 tetrahedra in queue.
  8433 insertions, added 1779 points, 64950 tetrahedra in queue.
Refinement seconds:  0.95311
Smoothing vertices...
Mesh smoothing seconds:  0.804609
Improving mesh...
Mesh improvement seconds:  0.022906

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

Output seconds:  0.003992
Total running seconds:  1.97841

Statistics:

  Input points: 14253
  Input facets: 28494
  Input segments: 42741
  Input holes: 2
  Input regions: 0

  Mesh points: 33071
  Mesh tetrahedra: 159280
  Mesh faces: 332807
  Mesh faces on exterior boundary: 28494
  Mesh faces on input facets: 28494
  Mesh edges on input segments: 42741
  Steiner points inside domain: 18818

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    = 7802
Number of elements = 15600
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 15600
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5906
Number of elements = 11808
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 545
Number of elements = 1086
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1086
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14253
Total number of elements = 28494
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 - 14253, elements - 28494
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.085438
Creating surface mesh ...
Surface mesh seconds:  0.011426
Recovering boundaries...
Boundary recovery seconds:  0.050052
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.016727
Recovering Delaunayness...
Delaunay recovery seconds:  0.030416
Refining mesh...
  18999 insertions, added 13806 points, 712098 tetrahedra in queue.
  6326 insertions, added 2564 points, 586841 tetrahedra in queue.
  8433 insertions, added 1779 points, 64950 tetrahedra in queue.
Refinement seconds:  0.956232
Smoothing vertices...
Mesh smoothing seconds:  0.817184
Improving mesh...
Mesh improvement seconds:  0.022974

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

Output seconds:  0.00414
Total running seconds:  1.99488

Statistics:

  Input points: 14253
  Input facets: 28494
  Input segments: 42741
  Input holes: 2
  Input regions: 0

  Mesh points: 33071
  Mesh tetrahedra: 159280
  Mesh faces: 332807
  Mesh faces on exterior boundary: 28494
  Mesh faces on input facets: 28494
  Mesh edges on input segments: 42741
  Steiner points inside domain: 18818

Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)

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

Writing MAPBC file ....
Finished writing MAPBC file


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

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)

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

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 5100, elements - 10188
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 - 5100, elements - 10188
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 - 14253, elements - 28494
Getting volume mesh

Generating volume mesh using TetGen.....

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

Writing MAPBC file ....
Finished writing MAPBC file

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

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

Writing MAPBC file ....
Finished writing MAPBC file

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

Writing MAPBC file ....
Finished writing MAPBC file

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

Writing MAPBC file ....
Finished writing MAPBC file

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

Writing MAPBC file ....
Finished writing MAPBC file

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4048
	Number of elements = 8092
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 8092
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6217
	Combined Number of elements = 12425
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12424
	Combined Elemental Quad4 = 0

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

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 3908
	Number of elements = 7812
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 7812
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6077
	Combined Number of elements = 12145
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12144
	Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4048
	Number of elements = 8092
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 8092
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6217
	Combined Number of elements = 12425
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12424
	Combined Elemental Quad4 = 0

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

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4048
	Number of elements = 8092
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 8092
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6217
	Combined Number of elements = 12425
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12424
	Combined Elemental Quad4 = 0

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

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 3908
	Number of elements = 7812
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 7812
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6077
	Combined Number of elements = 12145
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12144
	Combined Elemental Quad4 = 0

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

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 3908
	Number of elements = 7812
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 7812
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6077
	Combined Number of elements = 12145
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12144
	Combined Elemental Quad4 = 0

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
ok
test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable'
test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable'
test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable'
test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable'
test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable'
test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable'
test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable'
test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable'
test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable'
test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable'
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 1017
	Number of elements       = 5484
	Number of triangles      = 918
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4566
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 320
	Number of elements       = 1559
	Number of triangles      = 496
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1063
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 951
	Number of elements       = 5079
	Number of triangles      = 874
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4205
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 17432
	Number of elements       = 100418
	Number of triangles      = 5240
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 95178
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

Writing SU2 file ....
Finished writing SU2 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 (8.0.0) "

Writing SU2 file ....
Finished writing SU2 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 (8.0.0) "

Writing SU2 file ....
Finished writing SU2 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 (8.0.0) "
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          = 1017
	Number of elements       = 5484
	Number of triangles      = 918
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4566
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 393
	Number of elements       = 1929
	Number of triangles      = 612
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1317
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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          = 304
	Number of elements       = 1461
	Number of triangles      = 468
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 993
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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 Sense   Edges
EGADS    :      1     Yes     1   1 4 -3 -2
EGADS    :      2     Yes     1   3 7 -6 -5
EGADS    :      3     Yes     1   6 9 -1 -8
EGADS    :      4     Yes     1   -4 -9 -7
EGADS    :      5     Yes     1   -10 2 11 -12
EGADS    :      6     Yes     1   -11 5 13 -14
EGADS    :      7     Yes     1   -13 8 10 -15
EGADS    :      8     Yes     1   12 14 15
EGADS    :      9     Yes     1   16 19 -18 -17
EGADS    :     10     Yes     1   18 22 -21 -20
EGADS    :     11     Yes     1   21 24 -16 -23
EGADS    :     12     Yes     1   -19 -24 -22
EGADS    :     13     Yes     1   -25 17 26 -27
EGADS    :     14     Yes     1   -26 20 28 -29
EGADS    :     15     Yes     1   -28 23 25 -30
EGADS    :     16     Yes     1   27 29 30
EGADS    :     17     Yes     1   -31 -32 33 34
EGADS    :     18     Yes     1   -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=     12406
AFLR43   : Nodes             =      6209
 
 
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 16.32.49
AFLR3    : Version Date   07/26/23 @ 12:32AM
AFLR3    : Compile OS     Darwin 22.6.0 arm64
AFLR3    : Compile Date   08/01/23 @ 11:39PM
AFLR3    : Copyright 1994-2021, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =      6209         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          =     0.008   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =      6209         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =      1244      7682
AFLR3 IG : Nodes, Elements   =      2488     16247
AFLR3 IG : Nodes, Elements   =      3732     24929
AFLR3 IG : Nodes, Elements   =      4976     33969
AFLR3 IG : Nodes, Elements   =      6216     42984
AFLR3 IG : Nodes, Elements   =      6216     42922
AFLR3 IG : Nodes, Elements   =      6216     42927
AFLR3 IG : Nodes, Elements   =      6216     42922
AFLR3 IG : Nodes, Elements   =      6216     42927
AFLR3 IG : Nodes, Elements   =      6216     42920
AFLR3 IG : Nodes, Elements   =      6216     42921
AFLR3 IG : Nodes, Elements   =      6209     25546
AFLR3 IG : Nodes, Elements   =      6209     25566
AFLR3 IG : Nodes, Elements   =      6209     20496
AFLR3 IG : Nodes, Elements   =      6209     18359
 
AFLR3    : CPU Time          =     0.105   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =      6209     18359
AFLR3 GG : Nodes, Elements   =      9074     27175
AFLR3 GG : Nodes, Elements   =      9074     39170
AFLR3 GG : Nodes, Elements   =      9074     36224
AFLR3 GG : Nodes, Elements   =      9074     34723
AFLR3 GG : Nodes, Elements   =     11644     42749
AFLR3 GG : Nodes, Elements   =     11644     54099
AFLR3 GG : Nodes, Elements   =     11644     50812
AFLR3 GG : Nodes, Elements   =     11644     49921
AFLR3 GG : Nodes, Elements   =     14441     58599
AFLR3 GG : Nodes, Elements   =     14441     70844
AFLR3 GG : Nodes, Elements   =     14441     67333
AFLR3 GG : Nodes, Elements   =     14441     66422
AFLR3 GG : Nodes, Elements   =     17481     75734
AFLR3 GG : Nodes, Elements   =     17481     88956
AFLR3 GG : Nodes, Elements   =     17481     85215
AFLR3 GG : Nodes, Elements   =     17481     84368
AFLR3 GG : Nodes, Elements   =     20614     93923
AFLR3 GG : Nodes, Elements   =     20614    107375
AFLR3 GG : Nodes, Elements   =     20614    103694
AFLR3 GG : Nodes, Elements   =     20614    102890
AFLR3 GG : Nodes, Elements   =     23924    112944
AFLR3 GG : Nodes, Elements   =     23924    127128
AFLR3 GG : Nodes, Elements   =     23924    123349
AFLR3 GG : Nodes, Elements   =     23924    122508
AFLR3 GG : Nodes, Elements   =     27322    132858
AFLR3 GG : Nodes, Elements   =     27322    147287
AFLR3 GG : Nodes, Elements   =     27322    143409
AFLR3 GG : Nodes, Elements   =     27322    142563
AFLR3 GG : Nodes, Elements   =     30785    153086
AFLR3 GG : Nodes, Elements   =     30785    167947
AFLR3 GG : Nodes, Elements   =     30785    163988
AFLR3 GG : Nodes, Elements   =     30785    163155
AFLR3 GG : Nodes, Elements   =     34330    173904
AFLR3 GG : Nodes, Elements   =     34330    188899
AFLR3 GG : Nodes, Elements   =     34330    184950
AFLR3 GG : Nodes, Elements   =     34330    184198
AFLR3 GG : Nodes, Elements   =     37875    194909
AFLR3 GG : Nodes, Elements   =     37875    209837
AFLR3 GG : Nodes, Elements   =     37875    205939
AFLR3 GG : Nodes, Elements   =     37875    205185
AFLR3 GG : Nodes, Elements   =     41383    215750
AFLR3 GG : Nodes, Elements   =     41383    230824
AFLR3 GG : Nodes, Elements   =     41383    226838
AFLR3 GG : Nodes, Elements   =     41383    226055
AFLR3 GG : Nodes, Elements   =     44758    236221
AFLR3 GG : Nodes, Elements   =     44758    250507
AFLR3 GG : Nodes, Elements   =     44758    246858
AFLR3 GG : Nodes, Elements   =     44758    246174
AFLR3 GG : Nodes, Elements   =     47993    255921
AFLR3 GG : Nodes, Elements   =     47993    269685
AFLR3 GG : Nodes, Elements   =     47993    266082
AFLR3 GG : Nodes, Elements   =     47993    265470
AFLR3 GG : Nodes, Elements   =     51138    274926
AFLR3 GG : Nodes, Elements   =     51138    288260
AFLR3 GG : Nodes, Elements   =     51138    284900
AFLR3 GG : Nodes, Elements   =     51138    284259
AFLR3 GG : Nodes, Elements   =     54127    293245
AFLR3 GG : Nodes, Elements   =     54127    305708
AFLR3 GG : Nodes, Elements   =     54127    302622
AFLR3 GG : Nodes, Elements   =     54127    302089
AFLR3 GG : Nodes, Elements   =     56876    310344
AFLR3 GG : Nodes, Elements   =     56876    321960
AFLR3 GG : Nodes, Elements   =     56876    319008
AFLR3 GG : Nodes, Elements   =     56876    318534
AFLR3 GG : Nodes, Elements   =     59490    326385
AFLR3 GG : Nodes, Elements   =     59490    337219
AFLR3 GG : Nodes, Elements   =     59490    334507
AFLR3 GG : Nodes, Elements   =     59490    334143
AFLR3 GG : Nodes, Elements   =     61763    340968
AFLR3 GG : Nodes, Elements   =     61763    350625
AFLR3 GG : Nodes, Elements   =     61763    348113
AFLR3 GG : Nodes, Elements   =     61763    347806
AFLR3 GG : Nodes, Elements   =     63781    353860
AFLR3 GG : Nodes, Elements   =     63781    362343
AFLR3 GG : Nodes, Elements   =     63781    360110
AFLR3 GG : Nodes, Elements   =     63781    359835
AFLR3 GG : Nodes, Elements   =     65434    364796
AFLR3 GG : Nodes, Elements   =     65434    371861
AFLR3 GG : Nodes, Elements   =     65434    369981
AFLR3 GG : Nodes, Elements   =     65434    369781
AFLR3 GG : Nodes, Elements   =     66679    373516
AFLR3 GG : Nodes, Elements   =     66679    378838
AFLR3 GG : Nodes, Elements   =     66679    377349
AFLR3 GG : Nodes, Elements   =     66679    377207
AFLR3 GG : Nodes, Elements   =     67556    379838
AFLR3 GG : Nodes, Elements   =     67556    383674
AFLR3 GG : Nodes, Elements   =     67556    382612
AFLR3 GG : Nodes, Elements   =     67556    382516
AFLR3 GG : Nodes, Elements   =     68132    384245
AFLR3 GG : Nodes, Elements   =     68132    386717
AFLR3 GG : Nodes, Elements   =     68132    386001
AFLR3 GG : Nodes, Elements   =     68132    385950
AFLR3 GG : Nodes, Elements   =     68454    386917
AFLR3 GG : Nodes, Elements   =     68454    388272
AFLR3 GG : Nodes, Elements   =     68454    387885
AFLR3 GG : Nodes, Elements   =     68454    387856
AFLR3 GG : Nodes, Elements   =     68603    388303
AFLR3 GG : Nodes, Elements   =     68603    388994
AFLR3 GG : Nodes, Elements   =     68603    388755
AFLR3 GG : Nodes, Elements   =     68603    388747
AFLR3 GG : Nodes, Elements   =     68663    388927
AFLR3 GG : Nodes, Elements   =     68663    389173
AFLR3 GG : Nodes, Elements   =     68663    389089
AFLR3 GG : Nodes, Elements   =     68663    389081
AFLR3 GG : Nodes, Elements   =     68678    389127
AFLR3 GG : Nodes, Elements   =     68678    389189
AFLR3 GG : Nodes, Elements   =     68678    389164
AFLR3 GG : Nodes, Elements   =     68678    389168
AFLR3 GG : Nodes, Elements   =     68680    389174
AFLR3 GG : Nodes, Elements   =     68680    389185
AFLR3 GG : Nodes, Elements   =     68680    389182
AFLR3 GG : Nodes, Elements   =     68701    389245
AFLR3 GG : Nodes, Elements   =     68701    389327
AFLR3 GG : Nodes, Elements   =     68701    389297
AFLR3 GG : Nodes, Elements   =     68701    389298
AFLR3 GG : Nodes, Elements   =     68710    389325
AFLR3 GG : Nodes, Elements   =     68710    389355
AFLR3 GG : Nodes, Elements   =     68710    389347
AFLR3 GG : Nodes, Elements   =     68715    389362
AFLR3 GG : Nodes, Elements   =     68715    389378
AFLR3 GG : Nodes, Elements   =     68715    389373
AFLR3 GG : Nodes, Elements   =     68715    389374
AFLR3 GG : Nodes, Elements   =     68716    389377
AFLR3 GG : Nodes, Elements   =     68716    389381
AFLR3 GG : Nodes, Elements   =     68716    389380
 
AFLR3    : CPU Time          =     1.862   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =     68716    389380
AFLR3 QI : Nodes, Elements   =     67278    381216
AFLR3 QI : Nodes, Elements   =     67023    379752
AFLR3 QI : Nodes, Elements   =     67008    379668
AFLR3 QI : Nodes, Elements   =     67006    379656
AFLR3 QI : Nodes, Elements   =     67006    383317
AFLR3 QI : Nodes, Elements   =     67006    379427
AFLR3 QI : Nodes, Elements   =     67006    379059
AFLR3 QI : Nodes, Elements   =     67006    379440
AFLR3 QI : Nodes, Elements   =     67006    378845
AFLR3 QI : Nodes, Elements   =     67006    378651
AFLR3 QI : Nodes, Elements   =     67006    378930
AFLR3 QI : Nodes, Elements   =     67006    378627
AFLR3 QI : Nodes, Elements   =     67006    378531
AFLR3 QI : Nodes, Elements   =     67006    378787
AFLR3 QI : Nodes, Elements   =     67006    378530
AFLR3 QI : Nodes, Elements   =     67006    378477
AFLR3 QI : Nodes, Elements   =     67006    378727
AFLR3 QI : Nodes, Elements   =     67006    378484
AFLR3 QI : Nodes, Elements   =     67006    378447
AFLR3 QI : Nodes, Elements   =     67009    378461
AFLR3 QI : Nodes, Elements   =     67009    378706
AFLR3 QI : Nodes, Elements   =     67009    378476
AFLR3 QI : Nodes, Elements   =     67009    378460
AFLR3 QI : Nodes, Elements   =     67009    378698
AFLR3 QI : Nodes, Elements   =     67009    378474
AFLR3 QI : Nodes, Elements   =     67009    378437
 
AFLR3    : CPU Time          =     0.594   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =     67009    378437
AFLR3 QRG: Nodes, Elements   =     67032    378558
AFLR3 QRG: Nodes, Elements   =     67031    378553
AFLR3 QRG: Nodes, Elements   =     67037    378584
AFLR3 QRG: Nodes, Elements   =     67046    378631
AFLR3 QRG: Nodes, Elements   =     67044    378622
 
AFLR3    : CPU Time          =     0.023   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    378622
UG3      : Min, Max Ang      =     1.144     173.8
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        55
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.11e+06

UG3      : No. Tet Elems     =    378622
UG3      : Min Vol           =  6.04e-10
UG3      : Average Vol       =      5.57
UG3      : Total-Tet-Vol     =  2.11e+06
UG3      : No. Vol<TOL       =         0

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

UG3      : No. Tet Elems     =    378622
UG3      : Min, Max Q        =    0.0662         1
UG3      : Average Q         =      0.89
UG3      : No. Q<       0.1  =        20
UG3      : No. Q<      0.01  =         0

OVERALL  : CPU Time          =     2.770   seconds

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    378622
UG3      : Min, Max Ang      =     1.144     173.8
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        55
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.11e+06

UG3      : No. Tet Elems     =    378622
UG3      : Min Vol           =  6.04e-10
UG3      : Average Vol       =      5.57
UG3      : Total-Tet-Vol     =  2.11e+06
UG3      : No. Vol<TOL       =         0

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

UG3      : No. Tet Elems     =    378622
UG3      : Min, Max Q        =     0.171         1
UG3      : Average Q         =     0.853
UG3      : No. Q<       0.1  =         0
UG3      : No. Q<      0.01  =         0

UG3      : CPU Time          =     0.000   seconds

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

EGADS    : CREATE EGADS TESS FROM AFLR3 DATA

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

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

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

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

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

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

EGADS    : EGADS TESS CREATED

EGADS    : CHECK TESS FACE NODE MAP

EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 9
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 10
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 16
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 17
EGADS    : CHECKING NODE MAP FOR BODY 2 FACE 18
Volume mesh:
	Number of nodes          = 67044
	Number of elements       = 391028
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 378622
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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          = 67044
	Number of elements       = 391028
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 378622
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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 (8.0.0) "
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 (8.0.0) "
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!
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          = 67044
	Number of elements       = 391028
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 378622
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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 (8.0.0) "
 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 (8.0.0) "
 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          = 67044
	Number of elements       = 391028
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 378622
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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 (8.0.0) "
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 (8.0.0) "
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 (8.0.0) "
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)
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of node elements          = 0
Number of line elements          = 0
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)
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of node elements          = 0
Number of line elements          = 0
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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - 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 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

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

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

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

Getting FEA 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:61202)
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)
 174257000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 174257000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 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 node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 2 (of 7)
Number of nodes    = 298
Number of elements = 592
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 592
Number of quadrilateral elements = 0
Body 3 (of 7)
Number of nodes    = 488
Number of elements = 972
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 972
Number of quadrilateral elements = 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
Body 4 (of 7)
Number of nodes    = 2048
Number of elements = 4096
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 4096
Number of quadrilateral elements = 0
Body 5 (of 7)
Number of nodes    = 152
Number of elements = 300
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 300
Number of quadrilateral elements = 0
Body 6 (of 7)
Number of nodes    = 624
Number of elements = 1248
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1248
Number of quadrilateral elements = 0
Body 7 (of 7)
Number of nodes    = 489
Number of elements = 974
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 974
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4197
Total number of elements = 8374
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 298, elements - 592
Body 3 number of surface: nodes - 488, elements - 972
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 489, elements - 974
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.001941
Creating surface mesh ...
Surface mesh seconds:  5e-05
Recovering boundaries...
Boundary recovery seconds:  0.00077
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  2.8e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.0007
Refining mesh...
Refinement seconds:  0.000571
Smoothing vertices...
Mesh smoothing seconds:  0.002449
Improving mesh...
Mesh improvement seconds:  4.4e-05

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

Output seconds:  1.5e-05
Total running seconds:  0.006592

Statistics:

  Input points: 98
  Input facets: 192
  Input segments: 288
  Input holes: 0
  Input regions: 0

  Mesh points: 100
  Mesh tetrahedra: 232
  Mesh faces: 560
  Mesh faces on exterior boundary: 192
  Mesh faces on input facets: 192
  Mesh edges on input segments: 288
  Steiner points inside domain: 2

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 = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.010501
Creating surface mesh ...
Surface mesh seconds:  0.000157
Recovering boundaries...
Boundary recovery seconds:  0.001558
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.00016
Recovering Delaunayness...
Delaunay recovery seconds:  0.003079
Refining mesh...
Refinement seconds:  0.013376
Smoothing vertices...
Mesh smoothing seconds:  0.016146
Improving mesh...
Mesh improvement seconds:  0.000186

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

Output seconds:  3e-05
Total running seconds:  0.045224

Statistics:

  Input points: 298
  Input facets: 592
  Input segments: 888
  Input holes: 0
  Input regions: 0

  Mesh points: 355
  Mesh tetrahedra: 1106
  Mesh faces: 2508
  Mesh faces on exterior boundary: 592
  Mesh faces on input facets: 592
  Mesh edges on input segments: 888
  Steiner points inside domain: 57

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 = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.044895
Creating surface mesh ...
Surface mesh seconds:  0.000232
Recovering boundaries...
Boundary recovery seconds:  0.004677
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000329
Recovering Delaunayness...
Delaunay recovery seconds:  0.010308
Refining mesh...
  650 insertions, added 162 points, 7185 tetrahedra in queue.
  216 insertions, added 10 points, 5924 tetrahedra in queue.
  288 insertions, added 6 points, 2911 tetrahedra in queue.
  384 insertions, added 10 points, 126 tetrahedra in queue.
Refinement seconds:  0.108796
Smoothing vertices...
Mesh smoothing seconds:  0.037516
Improving mesh...
Mesh improvement seconds:  0.000442

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

Output seconds:  4.9e-05
Total running seconds:  0.207274

Statistics:

  Input points: 488
  Input facets: 972
  Input segments: 1458
  Input holes: 0
  Input regions: 0

  Mesh points: 687
  Mesh tetrahedra: 2744
  Mesh faces: 5974
  Mesh faces on exterior boundary: 972
  Mesh faces on input facets: 972
  Mesh edges on input segments: 1458
  Steiner points inside domain: 199

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 = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.324421
Creating surface mesh ...
Surface mesh seconds:  0.001087
Recovering boundaries...
Boundary recovery seconds:  0.004603
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.001198
Recovering Delaunayness...
Delaunay recovery seconds:  0.092668
Refining mesh...
Refinement seconds:  0.215075
Smoothing vertices...
Mesh smoothing seconds:  0.154082
Improving mesh...
Mesh improvement seconds:  0.001881

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

Output seconds:  0.000198
Total running seconds:  0.795282

Statistics:

  Input points: 2048
  Input facets: 4096
  Input segments: 6144
  Input holes: 0
  Input regions: 0

  Mesh points: 2901
  Mesh tetrahedra: 11307
  Mesh faces: 24662
  Mesh faces on exterior boundary: 4096
  Mesh faces on input facets: 4096
  Mesh edges on input segments: 6144
  Steiner points inside domain: 853

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 = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.000209
Creating surface mesh ...
Surface mesh seconds:  8.2e-05
Recovering boundaries...
Boundary recovery seconds:  0.000188
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  4.9e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.000276
Refining mesh...
Refinement seconds:  0.001711
Smoothing vertices...
Mesh smoothing seconds:  0.001372
Improving mesh...
Mesh improvement seconds:  9.5e-05

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

Output seconds:  2e-05
Total running seconds:  0.004024

Statistics:

  Input points: 152
  Input facets: 300
  Input segments: 450
  Input holes: 0
  Input regions: 0

  Mesh points: 193
  Mesh tetrahedra: 636
  Mesh faces: 1422
  Mesh faces on exterior boundary: 300
  Mesh faces on input facets: 300
  Mesh edges on input segments: 450
  Steiner points inside domain: 41

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 = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.03826
Creating surface mesh ...
Surface mesh seconds:  0.0003
Recovering boundaries...
Boundary recovery seconds:  0.003386
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000363
Recovering Delaunayness...
Delaunay recovery seconds:  0.005086
Refining mesh...
  831 insertions, added 215 points, 6026 tetrahedra in queue.
  276 insertions, added 15 points, 1148 tetrahedra in queue.
Refinement seconds:  0.048456
Smoothing vertices...
Mesh smoothing seconds:  0.036948
Improving mesh...
Mesh improvement seconds:  0.000542

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

Output seconds:  6.7e-05
Total running seconds:  0.133444

Statistics:

  Input points: 624
  Input facets: 1248
  Input segments: 1872
  Input holes: 0
  Input regions: 0

  Mesh points: 854
  Mesh tetrahedra: 3220
  Mesh faces: 7064
  Mesh faces on exterior boundary: 1248
  Mesh faces on input facets: 1248
  Mesh edges on input segments: 1872
  Steiner points inside domain: 230

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 = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.033789
Creating surface mesh ...
Surface mesh seconds:  0.000226
Recovering boundaries...
Boundary recovery seconds:  0.002564
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000226
Recovering Delaunayness...
Delaunay recovery seconds:  0.024792
Refining mesh...
Refinement seconds:  0.033301
Smoothing vertices...
Mesh smoothing seconds:  0.019116
Improving mesh...
Mesh improvement seconds:  0.000406

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

Output seconds:  4.9e-05
Total running seconds:  0.1145

Statistics:

  Input points: 489
  Input facets: 974
  Input segments: 1461
  Input holes: 0
  Input regions: 0

  Mesh points: 670
  Mesh tetrahedra: 2479
  Mesh faces: 5445
  Mesh faces on exterior boundary: 974
  Mesh faces on input facets: 974
  Mesh edges on input segments: 1461
  Steiner points inside domain: 181

Done meshing using TetGen!

Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file


Writing AFLR3 file ....
Finished writing AFLR3 file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 298, elements - 592
Body 3 number of surface: nodes - 488, elements - 972
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 489, elements - 974
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.001932
Creating surface mesh ...
Surface mesh seconds:  5.3e-05
Recovering boundaries...
Boundary recovery seconds:  0.000764
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  2.8e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.000697
Refining mesh...
Refinement seconds:  0.000268
Smoothing vertices...
Mesh smoothing seconds:  0.002394
Improving mesh...
Mesh improvement seconds:  0.000217

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

Output seconds:  1.5e-05
Total running seconds:  0.006393

Statistics:

  Input points: 98
  Input facets: 192
  Input segments: 288
  Input holes: 0
  Input regions: 1

  Mesh points: 100
  Mesh tetrahedra: 232
  Mesh faces: 560
  Mesh faces on exterior boundary: 192
  Mesh faces on input facets: 192
  Mesh edges on input segments: 288
  Steiner points inside domain: 2


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.010454
Creating surface mesh ...
Surface mesh seconds:  0.000155
Recovering boundaries...
Boundary recovery seconds:  0.001548
Removing exterior tetrahedra ...
Warning:  The 1-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds:  0.000158
Recovering Delaunayness...
Delaunay recovery seconds:  0.003049
Refining mesh...
Refinement seconds:  0.013362
Smoothing vertices...
Mesh smoothing seconds:  0.016139
Improving mesh...
Mesh improvement seconds:  0.000186

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

Output seconds:  2.9e-05
Total running seconds:  0.045107

Statistics:

  Input points: 298
  Input facets: 592
  Input segments: 888
  Input holes: 0
  Input regions: 2

  Mesh points: 355
  Mesh tetrahedra: 1106
  Mesh faces: 2508
  Mesh faces on exterior boundary: 592
  Mesh faces on input facets: 592
  Mesh edges on input segments: 888
  Steiner points inside domain: 57


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.044887
Creating surface mesh ...
Surface mesh seconds:  0.000253
Recovering boundaries...
Boundary recovery seconds:  0.004672
Removing exterior tetrahedra ...
Warning:  The 1-th region point lies outside the convex hull.
Warning:  The 2-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds:  0.000349
Recovering Delaunayness...
Delaunay recovery seconds:  0.010349
Refining mesh...
  650 insertions, added 162 points, 7185 tetrahedra in queue.
  216 insertions, added 10 points, 5924 tetrahedra in queue.
  288 insertions, added 6 points, 2911 tetrahedra in queue.
  384 insertions, added 10 points, 126 tetrahedra in queue.
Refinement seconds:  0.108725
Smoothing vertices...
Mesh smoothing seconds:  0.037484
Improving mesh...
Mesh improvement seconds:  0.00044

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

Output seconds:  4.8e-05
Total running seconds:  0.207241

Statistics:

  Input points: 488
  Input facets: 972
  Input segments: 1458
  Input holes: 0
  Input regions: 3

  Mesh points: 687
  Mesh tetrahedra: 2744
  Mesh faces: 5974
  Mesh faces on exterior boundary: 972
  Mesh faces on input facets: 972
  Mesh edges on input segments: 1458
  Steiner points inside domain: 199


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.324463
Creating surface mesh ...
Surface mesh seconds:  0.001025
Recovering boundaries...
Boundary recovery seconds:  0.00462
Removing exterior tetrahedra ...
Warning:  The 1-th region point lies outside the convex hull.
Warning:  The 2-th region point lies outside the convex hull.
Warning:  The 3-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds:  0.001206
Recovering Delaunayness...
Delaunay recovery seconds:  0.092697
Refining mesh...
Refinement seconds:  0.21622
Smoothing vertices...
Mesh smoothing seconds:  0.153962
Improving mesh...
Mesh improvement seconds:  0.001878

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

Output seconds:  0.000193
Total running seconds:  0.796333

Statistics:

  Input points: 2048
  Input facets: 4096
  Input segments: 6144
  Input holes: 0
  Input regions: 4

  Mesh points: 2901
  Mesh tetrahedra: 11307
  Mesh faces: 24662
  Mesh faces on exterior boundary: 4096
  Mesh faces on input facets: 4096
  Mesh edges on input segments: 6144
  Steiner points inside domain: 853


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.000218
Creating surface mesh ...
Surface mesh seconds:  8.1e-05
Recovering boundaries...
Boundary recovery seconds:  0.000186
Removing exterior tetrahedra ...
Warning:  The 1-th region point lies outside the convex hull.
Warning:  The 2-th region point lies outside the convex hull.
Warning:  The 3-th region point lies outside the convex hull.
Warning:  The 4-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds:  5.4e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.000277
Refining mesh...
Refinement seconds:  0.001587
Smoothing vertices...
Mesh smoothing seconds:  0.001365
Improving mesh...
Mesh improvement seconds:  9.5e-05

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

Output seconds:  2.1e-05
Total running seconds:  0.003906

Statistics:

  Input points: 152
  Input facets: 300
  Input segments: 450
  Input holes: 0
  Input regions: 5

  Mesh points: 193
  Mesh tetrahedra: 636
  Mesh faces: 1422
  Mesh faces on exterior boundary: 300
  Mesh faces on input facets: 300
  Mesh edges on input segments: 450
  Steiner points inside domain: 41


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.03831
Creating surface mesh ...
Surface mesh seconds:  0.000292
Recovering boundaries...
Boundary recovery seconds:  0.003484
Removing exterior tetrahedra ...
Warning:  The 1-th region point lies outside the convex hull.
Warning:  The 2-th region point lies outside the convex hull.
Warning:  The 3-th region point lies outside the convex hull.
Warning:  The 4-th region point lies outside the convex hull.
Warning:  The 5-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds:  0.000391
Recovering Delaunayness...
Delaunay recovery seconds:  0.005017
Refining mesh...
  831 insertions, added 215 points, 6026 tetrahedra in queue.
  276 insertions, added 15 points, 1148 tetrahedra in queue.
Refinement seconds:  0.045841
Smoothing vertices...
Mesh smoothing seconds:  0.036677
Improving mesh...
Mesh improvement seconds:  0.000595

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

Output seconds:  6.3e-05
Total running seconds:  0.130698

Statistics:

  Input points: 624
  Input facets: 1248
  Input segments: 1872
  Input holes: 0
  Input regions: 6

  Mesh points: 854
  Mesh tetrahedra: 3220
  Mesh faces: 7064
  Mesh faces on exterior boundary: 1248
  Mesh faces on input facets: 1248
  Mesh edges on input segments: 1872
  Steiner points inside domain: 230


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.033766
Creating surface mesh ...
Surface mesh seconds:  0.000253
Recovering boundaries...
Boundary recovery seconds:  0.002573
Removing exterior tetrahedra ...
Warning:  The 1-th region point lies outside the convex hull.
Warning:  The 2-th region point lies outside the convex hull.
Warning:  The 3-th region point lies outside the convex hull.
Warning:  The 4-th region point lies outside the convex hull.
Warning:  The 5-th region point lies outside the convex hull.
Warning:  The 6-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds:  0.000249
Recovering Delaunayness...
Delaunay recovery seconds:  0.024844
Refining mesh...
Refinement seconds:  0.030476
Smoothing vertices...
Mesh smoothing seconds:  0.019903
Improving mesh...
Mesh improvement seconds:  0.000413

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

Output seconds:  4.8e-05
Total running seconds:  0.11256

Statistics:

  Input points: 489
  Input facets: 974
  Input segments: 1461
  Input holes: 0
  Input regions: 7

  Mesh points: 673
  Mesh tetrahedra: 2510
  Mesh faces: 5507
  Mesh faces on exterior boundary: 974
  Mesh faces on input facets: 974
  Mesh edges on input segments: 1461
  Steiner points inside domain: 184

Done meshing using TetGen!

Writing AFLR3 file ....
Finished writing AFLR3 file

ok
test_journal (test_tetgen.TestTETGEN.test_journal) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

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

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!

Writing TECPLOT file: test.dat ....
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

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 - 7137, elements - 14266
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!

Writing TECPLOT file: test.dat ....
Finished writing TECPLOT file

ok
test_reenter (test_tetgen.TestTETGEN.test_reenter) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 9583
Number of elements = 19158
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 19158
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9583
Total number of elements = 19158

Writing TECPLOT file: test.dat ....
Finished writing TECPLOT file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!

Writing TECPLOT file: test.dat ....
Finished writing TECPLOT file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!

Writing TECPLOT file: test.dat ....
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

----------------------------------------------------------------------
Ran 137 tests in 331.788s

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

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


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


Running AVL!


Value of Cltot = 0.619913

StripForces

Wing = {"Xle":[1.565221892029e+00,1.512117367810e+00,1.409527304938e+00,1.264443046659e+00,1.086751845411e+00,8.885630629098e-01,6.833829371601e-01,4.851941546545e-01,3.075029533974e-01,1.624186951053e-01,5.982863221714e-02,6.724107980270e-03,6.724107971058e-03,5.982863219013e-02,1.624186950623e-01,3.075029533414e-01,4.851941545893e-01,6.833829370902e-01,8.885630628399e-01,1.086751845346e+00,1.264443046603e+00,1.409527304895e+00,1.512117367783e+00,1.565221892020e+00],"Yle":[-3.856416046770e+00,-3.725576361740e+00,-3.472813499993e+00,-3.115352832843e+00,-2.677554714026e+00,-2.189254361841e+00,-1.683728638332e+00,-1.195428286135e+00,-7.576301672945e-01,-4.001695001132e-01,-1.474066383261e-01,-1.656695325269e-02,1.656695322999e-02,1.474066382596e-01,4.001695000074e-01,7.576301671565e-01,1.195428285974e+00,1.683728638159e+00,2.189254361668e+00,2.677554713865e+00,3.115352832706e+00,3.472813499887e+00,3.725576361674e+00,3.856416046747e+00],"Zle":[2.486597711706e-01,2.402232939480e-01,2.239252714835e-01,2.008763870743e-01,1.726473841027e-01,1.411620224705e-01,1.085659775407e-01,7.708061590764e-02,4.885161293456e-02,2.580272852328e-02,9.504706056265e-03,1.068228830823e-03,1.068228829360e-03,9.504706051974e-03,2.580272851645e-02,4.885161292566e-02,7.708061589728e-02,1.085659775295e-01,1.411620224593e-01,1.726473840924e-01,2.008763870654e-01,2.239252714767e-01,2.402232939437e-01,2.486597711692e-01],"Chord":[9.710071581587e-01,9.928137666999e-01,1.034940899447e+00,1.094517661923e+00,1.167483996219e+00,1.248867367237e+00,1.333121632734e+00,1.414505003754e+00,1.487471338054e+00,1.547048100535e+00,1.589175233289e+00,1.610981841837e+00,1.610981841841e+00,1.589175233300e+00,1.547048100553e+00,1.487471338077e+00,1.414505003781e+00,1.333121632763e+00,1.248867367266e+00,1.167483996246e+00,1.094517661946e+00,1.034940899465e+00,9.928137667110e-01,9.710071581625e-01],"Area":[6.420432739224e-02,1.924649501823e-01,3.191588402418e-01,4.398794051499e-01,5.463997379092e-01,6.272332670617e-01,6.695492724342e-01,6.620092145623e-01,5.978048871833e-01,4.770843222898e-01,3.080744268775e-01,1.065203328294e-01,1.065203327570e-01,3.080744268129e-01,4.770843222394e-01,5.978048871514e-01,6.620092145502e-01,6.695492724407e-01,6.272332670835e-01,5.463997379421e-01,4.398794051895e-01,3.191588402846e-01,1.924649502262e-01,6.420432743628e-02],"c_cl":[1.751976980130e-01,4.816388142977e-01,7.134545983421e-01,8.955798774849e-01,1.045275116632e+00,1.165642609065e+00,1.251488483105e+00,1.294909342036e+00,1.290147495293e+00,1.237589733954e+00,1.147354354589e+00,1.069716379937e+00,1.027204841579e+00,9.123069911134e-01,8.271224835183e-01,7.465072383823e-01,6.622506856520e-01,5.718077594714e-01,4.773770050899e-01,3.839108464450e-01,2.965810831876e-01,2.166269422077e-01,1.372747954615e-01,4.847522879848e-02],"ai":[2.423376448059e-01,1.891573605669e-01,1.387726073609e-01,1.136377561110e-01,1.056109957987e-01,1.077519869781e-01,1.163918473303e-01,1.297918603655e-01,1.465983278745e-01,1.624995174599e-01,1.707158095744e-01,1.656351191924e-01,-7.833998870070e-02,-4.190817556553e-02,-1.699095118257e-02,-7.589503463777e-04,7.958849673277e-03,1.019416065188e-02,8.688915578617e-03,6.053380335312e-03,5.120395026966e-03,9.296755297777e-03,2.004804046056e-02,3.330492577563e-02],"cl_norm":[2.044051829731e-01,5.494672225940e-01,7.808579037666e-01,9.268407130704e-01,1.014078158135e+00,1.057019341175e+00,1.062951411331e+00,1.036333388587e+00,9.816462634652e-01,9.051794884118e-01,8.167547094730e-01,7.499676468296e-01,7.211772113978e-01,6.503467495436e-01,6.057660560785e-01,5.686988847404e-01,5.305932247981e-01,4.861412346267e-01,4.332732553833e-01,3.727603475166e-01,3.071901673655e-01,2.373206031154e-01,1.568074209165e-01,5.666485024183e-02],"cl":[1.803741931755e-01,4.848688546456e-01,6.890559834541e-01,8.178762563193e-01,8.948575908400e-01,9.327503738518e-01,9.379850374383e-01,9.144963748396e-01,8.662385668547e-01,7.987616435479e-01,7.207325646086e-01,6.617973538491e-01,6.363916792637e-01,5.738884333901e-01,5.345488897542e-01,5.018395375442e-01,4.682137871228e-01,4.289878157184e-01,3.823352848865e-01,3.289366049978e-01,2.710752133780e-01,2.094198967377e-01,1.383722840114e-01,5.000302093674e-02],"cd":[4.708816796009e-03,1.893013552459e-02,2.388458719214e-02,2.809788812558e-02,3.450496926229e-02,4.310977683932e-02,5.296690620746e-02,6.273588035903e-02,7.092746653689e-02,7.623132904844e-02,7.793919402367e-02,1.330641046360e-01,7.642533954135e-02,1.575280561792e-02,1.020926164298e-02,5.734996040024e-03,2.453990236867e-03,7.034156943368e-05,-1.681061755703e-03,-2.904871637690e-03,-3.696799546923e-03,-4.291551637880e-03,-4.755989795801e-03,-4.178738547362e-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":[-6.175122770628e-02,-1.541367450247e-01,-1.990020049076e-01,-2.179523703797e-01,-2.259241555999e-01,-2.291785023831e-01,-2.301045091167e-01,-2.293937884748e-01,-2.266765134793e-01,-2.205756980543e-01,-2.089282623641e-01,-1.947906406100e-01,-1.847119741766e-01,-1.559354818193e-01,-1.355315131375e-01,-1.232795365876e-01,-1.170486694970e-01,-1.141869860843e-01,-1.128288355903e-01,-1.117855412668e-01,-1.094863434131e-01,-1.016126232938e-01,-7.889656776594e-02,-3.215621313953e-02],"cm_LE":[-9.907391078322e-02,-2.553625521059e-01,-3.443180862959e-01,-3.917771248733e-01,-4.170475207534e-01,-4.288879437377e-01,-4.309998082913e-01,-4.249313258857e-01,-4.112512348867e-01,-3.899661415021e-01,-3.610798550198e-01,-3.345295675167e-01,-3.190696575593e-01,-2.776668920569e-01,-2.496150543392e-01,-2.306580335185e-01,-2.170714278266e-01,-2.053105443163e-01,-1.932221818516e-01,-1.798625218872e-01,-1.643057066256e-01,-1.427050164897e-01,-1.051753523062e-01,-4.137433282272e-02],"C.P.x/c":[5.923506801009e-01,5.678936810396e-01,5.388038268096e-01,5.164857534324e-01,5.024693961503e-01,4.957018606561e-01,4.953178888068e-01,5.008416597224e-01,5.116790825908e-01,5.261470832206e-01,5.398832002652e-01,5.443357803973e-01,5.402488831883e-01,5.217174153488e-01,5.035437183301e-01,4.956552889214e-01,4.999897967898e-01,5.161776906019e-01,5.451044281037e-01,5.898391652627e-01,6.538965497759e-01,7.352099770688e-01,8.201760893059e-01,8.930854083839e-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":[4.143502484419e-02,1.146121890397e-01,1.669674480705e-01,2.000258625576e-01,2.165069436650e-01,2.173612378317e-01,2.020982864242e-01,1.687203348327e-01,1.143884794131e-01,4.073751989365e-02],"ai":[2.065296924523e-01,1.849180223915e-01,1.591285664757e-01,1.456224964408e-01,1.435231644007e-01,1.506386553621e-01,1.666466052407e-01,1.914179167695e-01,2.193221173430e-01,2.365321328633e-01],"cl_norm":[6.579957348177e-02,1.763463053601e-01,2.425545992662e-01,2.698370559986e-01,2.694590983040e-01,2.501591871290e-01,2.170544160382e-01,1.714623014106e-01,1.118766125250e-01,3.907064104111e-02],"cl":[5.682537081790e-02,1.522949719002e-01,2.094733190134e-01,2.330348048803e-01,2.327083956801e-01,2.160407403863e-01,1.874510278163e-01,1.480770823179e-01,9.661810337338e-02,3.374191575678e-02],"cd":[4.670566079260e-03,1.374698956983e-02,1.845844898552e-02,2.032218684725e-02,2.072187092673e-02,2.023884851599e-02,1.896705322934e-02,1.657142171121e-02,1.222733795468e-02,5.106244760924e-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":[-3.303465544544e-02,-8.761746958838e-02,-1.194746602282e-01,-1.341488123563e-01,-1.380350789963e-01,-1.339349413680e-01,-1.218867053325e-01,-1.002593790936e-01,-6.716156843032e-02,-2.373448304337e-02],"cm_LE":[-4.232877133357e-02,-1.126299441676e-01,-1.539951982649e-01,-1.724118490116e-01,-1.757829360724e-01,-1.683239687784e-01,-1.510824211718e-01,-1.228726806389e-01,-8.171902803731e-02,-2.878672165377e-02],"C.P.x/c":[8.313363814431e-01,8.253142634661e-01,8.203574125378e-01,8.256599853193e-01,8.431675932569e-01,8.699522420101e-01,9.002322593392e-01,9.270755982234e-01,9.451240614895e-01,9.534124326091e-01]}


real	0m0.396s
user	0m0.251s
sys	0m0.069s
+ status=0
+ set +x

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


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


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

Value of CL = 0.276892 

real	0m1.191s
user	0m1.084s
sys	0m0.037s
+ status=0
+ set +x

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


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


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

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


Running FRICTION!


Value of CDfric = 0.009900

Value of CDfric = 0.009190

real	0m0.334s
user	0m0.152s
sys	0m0.024s
+ status=0
+ set +x

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

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

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


Attention: fun3dAFLR2Test is hard coded to look for ../csmData/cfd2D.csm
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mquad                       = 1         
UG PARAM : mpp                         = 3         
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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          =     0.002   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          =     0.036   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      2159
AFLR2 QI : Nodes, Faces      =     18604     17104
AFLR2 QI : Nodes, Faces      =     18604     36367
AFLR2 QI : Nodes, Faces      =     18604      2159
AFLR2 QI : Nodes, Faces      =     18604     17104
AFLR2 QI : Nodes, Faces      =     18604      2159
AFLR2 QI : Nodes, Faces      =     18604     17104
 
AFLR2    : CPU Time          =     0.014   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 18604
Number of elements = 20104
Number of tris = 2159
Number of quad = 17104

Writing TECPLOT file: AFLR2_Test.dat ....
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 =  2159
	Number of Hexahedral =  17104

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	0m0.753s
user	0m0.589s
sys	0m0.320s
+ status=0
+ set +x

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


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


Attention: fun3dTetgenTest is hard coded to look for ../csmData/cfdMultiBody.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 9573
Number of elements = 19142
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 19142
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 6160
Number of elements = 12316
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 12316
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 258
Number of elements = 512
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 512
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 15991
Total number of elements = 31970
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 - 15991, elements - 31970
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.096128
Creating surface mesh ...
Surface mesh seconds:  0.013146
Recovering boundaries...
Boundary recovery seconds:  0.058623
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.018924
Recovering Delaunayness...
Delaunay recovery seconds:  0.036938
Refining mesh...
  21316 insertions, added 16866 points, 786217 tetrahedra in queue.
  7098 insertions, added 2814 points, 333350 tetrahedra in queue.
Refinement seconds:  0.719166
Smoothing vertices...
Mesh smoothing seconds:  0.929456
Improving mesh...
Mesh improvement seconds:  0.02568

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

Output seconds:  0.004437
Total running seconds:  1.90268

Statistics:

  Input points: 15991
  Input facets: 31970
  Input segments: 47955
  Input holes: 2
  Input regions: 0

  Mesh points: 36858
  Mesh tetrahedra: 177623
  Mesh faces: 371231
  Mesh faces on exterior boundary: 31970
  Mesh faces on input facets: 31970
  Mesh edges on input segments: 47955
  Steiner points inside domain: 20867

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	0m3.520s
user	0m3.956s
sys	0m0.111s
+ status=0
+ set +x

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

Running.... STRUCTURE c-Tests

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


Note: interferenceTest uses ../csmData/interference.csm
 classifyClouds: EG_generalBoolean = -7!
 classifyClouds: EG_generalBoolean = -7!
 classifyClouds: EG_generalBoolean = -7!
 classifyClouds: EG_generalBoolean = -7!
  1:  1.000000e+00  Box
  2:  5.850521e-01  Sphere
  3:  7.191810e-01  Cylinder
  4:  4.000000e+01  OuterBox

  0.000000e+00  -2.715465e-02   0.000000e+00   0.000000e+00 
 -2.715465e-02   0.000000e+00   0.000000e+00  -2.543571e-02 
  0.000000e+00   0.000000e+00   0.000000e+00   0.000000e+00 
  0.000000e+00  -2.543571e-02   0.000000e+00   1.000000e+00 

 classifyClouds: EG_generalBoolean = -7!
 classifyClouds: EG_generalBoolean = -7!
  1:  1.000000e+00  Box
  2:  5.886885e-01  Sphere
  3:  7.235323e-01  Cylinder

  0.000000e+00  -2.059198e-02   0.000000e+00 
 -2.059198e-02   0.000000e+00   0.000000e+00 
  0.000000e+00   0.000000e+00   0.000000e+00 


real	0m2.142s
user	0m3.839s
sys	0m0.038s
+ status=0
+ set +x

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


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


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

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

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

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

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

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

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

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

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.314E+01  0.628E+01  0.000E+00    0.080  ddx @ (   1.00   0.00   0.00)
   1*   0.341E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   1*   0.326E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.07   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   0.10   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   0.07   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   0.03   0.00)
   3*   0.163E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.03   0.00)
   3*   0.167E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   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   0.07   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   0.00   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   0.00   0.00)
   7*   0.297E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   7*   0.435E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   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   0.00   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   0.10   0.00)
   9*   0.167E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   9*   0.264E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   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   0.00   0.00)
  10*   0.239E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  10*   0.393E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  iter     dr         dd         dp         rlx   max
  11    0.257E+00  0.120E+01  0.614E-08    0.417  ddz @ (   1.00   0.00   0.00)
  11*   0.206E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   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    0.253E-15  0.930E-15  0.713E-15    1.000  ddx @ (   0.56   0.10   0.00)

 Converging n vectors ...
 it =  1    dn =  0.193E+01   rlx = 1.000  (   9 )
 it =  2    dn =  0.583E-15   rlx = 1.000  (  31 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.285E+01   rlx = 0.351  (  24 )
 it =  2    de =  0.269E+01   rlx = 0.372  (  14 )
 it =  3    de =  0.202E+01   rlx = 0.494  (  14 )
 it =  4    de =  0.122E+01   rlx = 0.820  (  14 )
 it =  5    de =  0.378E+00   rlx = 1.000  (  14 )
 it =  6    de =  0.127E-01   rlx = 1.000  (  40 )
 it =  7    de =  0.524E-06   rlx = 1.000  (  40 )
 it =  8    de =  0.128E-15   rlx = 1.000  (  22 )

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

real	0m0.325s
user	0m0.223s
sys	0m0.025s
+ status=0
+ set +x

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


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


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

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

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

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

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

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

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

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

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.609E+00  0.519E+01  0.240E+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*   0.837E-04  0.000E+00  0.000E+00    1.000  drz @ (   0.06   0.14   0.00)
   2    0.769E-02  0.753E+00  0.105E+01    0.478  dps @ (   0.00   0.00   0.00)
   2*   0.329E-03  0.000E+00  0.000E+00    1.000  drx @ (   0.06   0.06   0.00)
   2*   0.641E-06  0.000E+00  0.000E+00    1.000  drz @ (   0.06   0.08   0.00)
   3    0.264E-02  0.213E+00  0.280E+00    1.000  dps @ (   0.50   0.00   0.00)
   3*   0.194E-03  0.000E+00  0.000E+00    1.000  drz @ (   0.39   0.11   0.00)
   3*   0.741E-06  0.000E+00  0.000E+00    1.000  drx @ (   0.44   0.03   0.00)
   4    0.119E-03  0.159E-01  0.631E-01    1.000  dps @ (   0.39   0.14   0.00)
   4*   0.306E-05  0.000E+00  0.000E+00    1.000  drx @ (   0.44   0.22   0.00)
   5    0.133E-05  0.441E-03  0.208E-02    1.000  dps @ (   0.06   0.06   0.00)
   6    0.233E-08  0.153E-06  0.694E-06    1.000  dps @ (   0.50   0.00   0.00)
   7    0.378E-15  0.119E-12  0.317E-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 =  0.236E-15   rlx = 1.000  (  81 )

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

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

real	0m0.497s
user	0m0.403s
sys	0m0.023s
+ status=0
+ set +x

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


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


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

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

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

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

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

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

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

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

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

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

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

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

real	0m0.299s
user	0m0.204s
sys	0m0.025s
+ status=0
+ set +x

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

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

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

All tests pass!


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

=================================================
Using python : /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/python
=================================================

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

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

=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
CXtot   0.0006119078685800691
CYtot   -6.294248256212792e-15
CZtot   -0.3012861394881716
Cltot   -4.783257394769952e-14
Cmtot   -0.1945055953448142
Cntot   -2.33897052252666e-15
Cl'tot  -4.786610947920897e-14
Cn'tot  -1.50382076451035e-15
CLtot   0.3012509314146399
CDtot   0.00464635348821982
CDvis   0.0
CLff    0.3009503023516155
CYff    -7.721166100146254e-15
CDind   0.00464635348821982
CDff    0.00496896950089486
e       0.9669902146156001
StripForces 
Wing  cl =  [0.02994790451338, 0.08555545178909, 0.1329003532584, 0.1733025192691, 0.2100182422829, 0.2453427152542, 0.279274699636, 0.3101221284185, 0.3355632628219, 0.3531618776071, 0.3603457261529, 0.3542128805661, 0.3542128805657, 0.3603457261529, 0.3531618776083, 0.3355632628247, 0.3101221284231, 0.2792746996423, 0.2453427152618, 0.2100182422917, 0.1733025192796, 0.132900353272, 0.08555545180763, 0.0299479045407]
Wing  cd =  [-0.004234137763147, -0.004494543653181, -0.003752887372721, -0.002739626801633, -0.001762021024329, -0.0007386538946455, 0.0005114598078319, 0.00211914728609, 0.00414518990896, 0.006609094404164, 0.009540018987574, 0.01315518814705, 0.01315518814715, 0.00954001898777, 0.006609094404422, 0.004145189909247, 0.002119147286374, 0.0005114598080921, -0.0007386538944123, -0.001762021024098, -0.002739626801367, -0.003752887372441, -0.004494543653151, -0.00423413776453]

real	0m0.455s
user	0m0.584s
sys	0m0.176s
+ status=0
+ set +x

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


=================================================
+ echo 'avl_AutoSpan_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_AutoSpan_PyTest.py test;
+ python -u avl_AutoSpan_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wing3, index = 3
Getting vortex lattice surface data
	VLM surface name - Wing1
	VLM surface name - Wing2
	VLM surface name - Wing3
	Done getting vortex lattice surface data
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Writing surface - Wing1 (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - Wing2 (ID = 1)
	Section 1 of 7 (ID = 0)
	Section 2 of 7 (ID = 1)
	Section 3 of 7 (ID = 2)
	Section 4 of 7 (ID = 3)
	Section 5 of 7 (ID = 4)
	Section 6 of 7 (ID = 5)
	Section 7 of 7 (ID = 6)
Writing surface - Wing3 (ID = 2)
	Section 1 of 7 (ID = 0)
	Section 2 of 7 (ID = 3)
	  Control surface 1 of 1 
	Section 3 of 7 (ID = 4)
	  Control surface 1 of 1 
	Section 4 of 7 (ID = 1)
	Section 5 of 7 (ID = 5)
	  Control surface 1 of 1 
	Section 6 of 7 (ID = 6)
	  Control surface 1 of 1 
	Section 7 of 7 (ID = 2)
CXtot   -0.0412001563846227
CYtot   2.978622347381309e-11
CZtot   -1.125018848419552
Cltot   6.433305666344365e-11
Cmtot   -1.954741259599045
Cntot   -8.596041715790853e-12
Cl'tot  6.417323681353383e-11
Cn'tot  -9.717499149244883e-12
CLtot   1.124128460725282
CDtot   0.06082816759347054
CDvis   0.0
CLff    1.12310548217915
CYff    1.557646063320801e-11
CDind   0.06082816759347054
CDff    -0.2032105909613897
e       -0.3293014157959109

real	0m5.436s
user	0m5.645s
sys	0m5.096s
+ status=0
+ set +x

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


=================================================
+ echo 'avl_DesignSweep_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_DesignSweep_PyTest.py test;
+ python -u avl_DesignSweep_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Cd = 0.002572533601550746
Cl = 0.2009337808873514
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 = 0.002586364230241773
Cl = 0.2015191856814839
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 = 0.002609799718816135
Cl = 0.202507529643331
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 = 0.002643444008424596
Cl = 0.2039185811658758
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 = 0.002688200920998178
Cl = 0.2057816377790573
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 = 0.002745342060015916
Cl = 0.2081373840559939
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 = 0.002816610334298742
Cl = 0.2110406736705551
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 = 0.002904376657734686
Cl = 0.2145646488015986
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 = 0.003011879793042714
Cl = 0.2188068842334934
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 = 0.003143602034586197
Cl = 0.2238987294815716
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 = 0.003305877285452323
Cl = 0.2300199286487145
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 = 0.003507917885472498
Cl = 0.2374223860296622
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 = 0.003763643677259927
Cl = 0.2464707142744897
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 = 0.004095167898227168
Cl = 0.2577158067747692
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 = 0.004540047408135285
Cl = 0.2720394012163574
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 = 0.005168237926851837
Cl = 0.2909701507463247
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 = 0.006128930715329106
Cl = 0.3174875485935573
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 = 0.007818359051271607
Cl = 0.3586078919918749
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 = 0.01186220444373959
Cl = 0.438263863524391
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 = 0.002572533601550746
Cl = 0.2009337808873514
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 = 0.002586364230241773
Cl = 0.2015191856814839
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 = 0.002609799718816135
Cl = 0.202507529643331
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 = 0.002643444008424596
Cl = 0.2039185811658758
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 = 0.002688200920998178
Cl = 0.2057816377790573
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 = 0.002745342060015916
Cl = 0.2081373840559939
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 = 0.002816610334298742
Cl = 0.2110406736705551
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 = 0.002904376657734686
Cl = 0.2145646488015986
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 = 0.003011879793042714
Cl = 0.2188068842334934
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 = 0.003143602034586197
Cl = 0.2238987294815716
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 = 0.003305877285452323
Cl = 0.2300199286487145
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 = 0.003507917885472498
Cl = 0.2374223860296622
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 = 0.003763643677259927
Cl = 0.2464707142744897
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 = 0.004095167898227168
Cl = 0.2577158067747692
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 = 0.004540047408135285
Cl = 0.2720394012163574
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 = 0.005168237926851837
Cl = 0.2909701507463247
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 = 0.006128930715329106
Cl = 0.3174875485935573
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 = 0.007818359051271607
Cl = 0.3586078919918749
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 = 0.01186220444373959
Cl = 0.438263863524391
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 = 0.002572533601550746
Cl = 0.2009337808873514
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 = 0.002586364230241773
Cl = 0.2015191856814839
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 = 0.002609799718816135
Cl = 0.202507529643331
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 = 0.002643444008424596
Cl = 0.2039185811658758
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 = 0.002688200920998178
Cl = 0.2057816377790573
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 = 0.002745342060015916
Cl = 0.2081373840559939
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 = 0.002816610334298742
Cl = 0.2110406736705551
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 = 0.002904376657734686
Cl = 0.2145646488015986
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 = 0.003011879793042714
Cl = 0.2188068842334934
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 = 0.003143602034586197
Cl = 0.2238987294815716
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 = 0.003305877285452323
Cl = 0.2300199286487145
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 = 0.003507917885472498
Cl = 0.2374223860296622
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 = 0.003763643677259927
Cl = 0.2464707142744897
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 = 0.004095167898227168
Cl = 0.2577158067747692
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 = 0.004540047408135285
Cl = 0.2720394012163574
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 = 0.005168237926851837
Cl = 0.2909701507463247
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 = 0.006128930715329106
Cl = 0.3174875485935573
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 = 0.007818359051271607
Cl = 0.3586078919918749
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 = 0.01186220444373959
Cl = 0.438263863524391
Cl[0] =  0.2009337808873514
Cd[0] =  0.002572533601550746

real	0m16.225s
user	0m8.276s
sys	0m7.887s
+ status=0
+ set +x

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


=================================================
+ echo 'avl_ControlSurf_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_ControlSurf_PyTest.py test;
+ python -u avl_ControlSurf_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting design parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice control surface data
	VLM control surface name - Tail
	VLM control surface name - WingRightLE
	VLM control surface name - WingRightTE
	Done getting vortex lattice control surface data
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Alpha  1.0
Beta   0.0
Mach   0.5
pb/2V  -0.0
qc/2V  0.0
rb/2V  -0.0
p'b/2V -0.0
r'b/2V -0.0
CXtot  -0.01911479917641004
CYtot  0.03828770401115552
CZtot  -0.6203123021537943
Cltot  0.05803020542928476
Cmtot  -0.3649415791575075
Cntot  -0.02051317548232544
Cl'tot 0.05766336287208541
Cn'tot -0.02152281795713262
CLtot  0.6198842263414324
CDtot  0.02993783031514589
CDvis  0.0
CLff   0.6192452092592857
CYff   0.03287079625844262
CDind  0.02993783031514589
CDff   0.02861019822657772
e      0.7130586920543268

real	0m0.559s
user	0m0.653s
sys	0m0.189s
+ status=0
+ set +x

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


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

real	0m0.444s
user	0m0.582s
sys	0m0.168s
+ status=0
+ set +x

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


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

           * * *

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

At X0         0 variables are exactly at the bounds

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

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

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

At iterate    3    f=  2.43104D-05    |proj g|=  1.42017D-02
Alpha [-5.49659696] Beta [2.89526135] Cmtot2 [3.72334444e-08]
Cmtot2_Alpha [[0.00055304]]
Cmtot2_Beta [[8.73257587e-06]]

At iterate    4    f=  3.72334D-08    |proj g|=  5.53036D-04
Alpha [-5.50424967] Beta [2.89504288] Cmtot2 [2.19764419e-12]
Cmtot2_Alpha [[4.24792989e-06]]
Cmtot2_Beta [[6.7141843e-08]]

At iterate    5    f=  2.19764D-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 =   2.1976441939068914E-012

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

real	0m12.816s
user	0m4.150s
sys	0m0.807s
+ status=0
+ set +x

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

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

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

real	0m0.290s
user	0m0.374s
sys	0m0.068s
+ status=0
+ set +x

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

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

=================================================
+ echo 'tsfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting results
PAUSE Press the ENTER key to exit
To resume execution, type go.  Other input will terminate the job.
Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG
Cl =  0.933407
Cd =  0.000284
Cd Wave =  0.0
Cm =  -0.203436
Cp _Critcal =  -1.303869

real	0m0.315s
user	0m0.412s
sys	0m0.053s
+ status=0
+ set +x

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

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

=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  0.3783791085548177
Cd =  0.007775858417209677
Cm =  0.005262636995835036

real	0m1.844s
user	0m2.064s
sys	0m0.084s
+ status=0
+ set +x

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


=================================================
+ echo 'mses_OpenMDAO_3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_OpenMDAO_3_PyTest.py test;
+ python -u mses_OpenMDAO_3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - camber
	Done getting CFD design variables
camber [0.1] CD [0.01326534]
camber [0.1] CD [0.01326534]
CD_camber [[0.1764758]]
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 [-0.0764758] CD [0.01022332]
CD_camber [[-0.08759853]]

At iterate    1    f=  1.02233D-02    |proj g|=  8.75985D-02
camber [-0.01793539] CD [0.00770373]
CD_camber [[-0.01328932]]

At iterate    2    f=  7.70373D-03    |proj g|=  1.32893D-02
camber [-0.00746613] CD [0.00760241]
CD_camber [[-0.00542337]]

At iterate    3    f=  7.60241D-03    |proj g|=  5.42337D-03
camber [-0.00024784] CD [0.00758207]
CD_camber [[-0.00011854]]

At iterate    4    f=  7.58207D-03    |proj g|=  1.18538D-04
camber [-8.65457493e-05] CD [0.00758207]
CD_camber [[-3.94469721e-06]]
camber [-0.00019629] CD [0.00758207]
CD_camber [[-8.4257979e-05]]

At iterate    5    f=  7.58207D-03    |proj g|=  8.42580D-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   8.426D-05   7.582D-03
  F =   7.5820667358140921E-003

CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-0.00019629]

real	0m13.705s
user	0m13.740s
sys	0m0.317s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case mses_OpenMDAO_3_PyTest.py passed (as expected)
=================================================

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

=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  [1.05475230551148, 1.36488869373725, 1.56607214272246, 2.03059709357768, 1.9727108312095, 1.87307153172323, 1.76050475760053]
Cd =  [0.0131991208831308, 0.0166540240605859, 0.0200551482562657, 0.0458671341873005, 0.0754256009397268, 0.0994469174479059, 0.127479430989221]
Alpha =  [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location =  [0.49604411072842, 0.461377732041756, 0.442376568202227, 0.361251636144409, 0.276104140854608, 0.214381239321802, 0.132988264746433]

real	0m1.939s
user	0m2.175s
sys	0m0.070s
+ status=0
+ set +x

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

Running.... MESH PyTests


=================================================
+ echo 'egadsTess_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
	Name = Wing, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2

Getting mesh sizing parameters
	Mesh sizing name - LeadingEdge
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes    = 3793
Number of elements = 4001
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 4001
Body 2 (of 4)
Number of nodes    = 1
Number of elements = 1
Number of node elements          = 1
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 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
Body 3 (of 4)
Number of nodes    = 76
Number of elements = 55
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 55
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to 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 4 (of 4)
Number of nodes    = 100
Number of elements = 73
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 73
----------------------------
Total number of nodes    = 3970
Total number of elements = 4130

Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_2.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_3.dat ....
Finished writing TECPLOT file


real	0m3.210s
user	0m8.929s
sys	0m4.939s
+ status=0
+ set +x

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


=================================================
+ echo 'egadsTess_Box_Quad_Pytest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_Box_Quad_Pytest.py test;
+ python -u egadsTess_Box_Quad_Pytest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = box1, index = 1
	Name = box2, index = 2
	Name = box3, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 3 TFI quading disabled with attribute .qParams
	Face 4 TFI quading disabled with attribute .qParams
	TFI quading on all faces disabled with .qParams attribute on the body
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 602
Number of elements = 600
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 600
	capsIgnore attribute found for face - 6!!
Body 2 (of 3)
Number of nodes    = 537
Number of elements = 535
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 535
Body 3 (of 3)
Number of nodes    = 1356
Number of elements = 1354
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 1354
----------------------------
Total number of nodes    = 2495
Total number of elements = 2489

Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_2.dat ....
Finished writing TECPLOT file


real	0m2.080s
user	0m2.617s
sys	0m0.047s
+ status=0
+ set +x

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


=================================================
+ echo 'egadsTess_Spheres_Quad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_Spheres_Quad_PyTest.py test;
+ python -u egadsTess_Spheres_Quad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Spheres, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 4 has a degenerate edge - no TFI quading
	Face 5 has a degenerate edge - no TFI quading
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 6316
Number of elements = 6314
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 6314
----------------------------
Total number of nodes    = 6316
Total number of elements = 6314

Writing TECPLOT file: egadsTessMesh.dat ....
Finished writing TECPLOT file


real	0m5.457s
user	0m8.465s
sys	0m0.113s
+ status=0
+ set +x

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


=================================================
+ echo 'egadsTess_Nose_Quad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_Nose_Quad_PyTest.py test;
+ python -u egadsTess_Nose_Quad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = nose, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 2 has a degenerate edge - no TFI quading
Getting surface mesh for body 1 (of 1)
 EG_getSidepoint: LineSearch Failed (0.000000 0.973785)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.013232 0.966690)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.046939 0.962477)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.035340 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 node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 1496
----------------------------
Total number of nodes    = 1498
Total number of elements = 1496

Writing TECPLOT file: egadsTessMesh.dat ....
Finished writing TECPLOT file


real	0m1.805s
user	0m2.187s
sys	0m0.073s
+ status=0
+ set +x

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


=================================================
+ echo 'aflr2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       316       634
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       681      1018
AFLR2 GGp: Nodes, Faces      =      1013      1682
AFLR2 GGp: Nodes, Faces      =      1339      2334
AFLR2 GGp: Nodes, Faces      =      1652      2960
AFLR2 GGp: Nodes, Faces      =      1957      3570
AFLR2 GGp: Nodes, Faces      =      2252      4160
AFLR2 GGp: Nodes, Faces      =      2526      4708
AFLR2 GGp: Nodes, Faces      =      2809      5274
AFLR2 GGp: Nodes, Faces      =      3083      5822
AFLR2 GGp: Nodes, Faces      =      3327      6310
AFLR2 GGp: Nodes, Faces      =      3564      6784
AFLR2 GGp: Nodes, Faces      =      3788      7232
AFLR2 GGp: Nodes, Faces      =      3995      7646
AFLR2 GGp: Nodes, Faces      =      4194      8044
AFLR2 GGp: Nodes, Faces      =      4394      8444
AFLR2 GGp: Nodes, Faces      =      4585      8826
AFLR2 GGp: Nodes, Faces      =      4772      9200
AFLR2 GGp: Nodes, Faces      =      4943      9542
AFLR2 GGp: Nodes, Faces      =      5129      9914
AFLR2 GGp: Nodes, Faces      =      5293     10242
AFLR2 GGp: Nodes, Faces      =      5447     10550
AFLR2 GGp: Nodes, Faces      =      5594     10844
AFLR2 GGp: Nodes, Faces      =      5716     11088
AFLR2 GGp: Nodes, Faces      =      5830     11316
AFLR2 GGp: Nodes, Faces      =      5909     11474
AFLR2 GGp: Nodes, Faces      =      5964     11584
AFLR2 GGp: Nodes, Faces      =      6006     11668
AFLR2 GGp: Nodes, Faces      =      6025     11706
AFLR2 GGp: Nodes, Faces      =      6034     11724
 
AFLR2    : CPU Time          =     0.010   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      6034     11724
AFLR2 QI : Nodes, Faces      =      6033       454
AFLR2 QI : Nodes, Faces      =      6033      5634
AFLR2 QI : Nodes, Faces      =      6033     11722
AFLR2 QI : Nodes, Faces      =      6032       462
AFLR2 QI : Nodes, Faces      =      6032      5629
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       456
AFLR2 QI : Nodes, Faces      =      6032      5632
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       474
AFLR2 QI : Nodes, Faces      =      6032      5623
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6031       486
AFLR2 QI : Nodes, Faces      =      6031      5616
AFLR2 QI : Nodes, Faces      =      6031       488
AFLR2 QI : Nodes, Faces      =      6031      5616
 
AFLR2    : CPU Time          =     0.004   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

Writing TECPLOT file: pyCAPS_AFLR2_Test.dat ....
Finished writing TECPLOT file

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)!

real	0m0.435s
user	0m0.683s
sys	0m0.357s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_PyTest.py test;
+ python -u aflr4_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value

Writing TECPLOT file: pyCAPS_AFLR4_Test.dat ....
Finished writing TECPLOT file


real	0m1.005s
user	0m1.221s
sys	0m0.090s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_Symmetry_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_Symmetry_PyTest.py test;
+ python -u aflr4_Symmetry_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Farfield, index = 1
	Name = Symmetry, index = 2
	Name = Wing1, index = 3
	Name = Wing2, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = Symmetry, index = 2
	Name = Wing1, index = 3
	Name = Wing2, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - Symmetry
	Done getting mesh sizing parameters
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing TECPLOT file: pyCAPS_AFLR4_Test.dat ....
Finished writing TECPLOT file


real	0m1.174s
user	0m1.381s
sys	0m0.250s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_Symmetry_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_Generic_Missile.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_Generic_Missile.py test;
+ python -u aflr4_Generic_Missile.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = MissileOML, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing TECPLOT file: pyCAPS_AFLR4_Missile_Test.dat ....
Finished writing TECPLOT file


real	0m3.205s
user	0m5.985s
sys	0m0.300s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_Generic_Missile.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_TipTreat_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_TipTreat_PyTest.py test;
+ python -u aflr4_TipTreat_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing TECPLOT file: pyCAPS_AFLR4_1B2_Test.dat ....
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: pyCAPS_AFLR4_1B0_Test.dat ....
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: pyCAPS_AFLR4_1S2_Test.dat ....
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: pyCAPS_AFLR4_1S0_Test.dat ....
Finished writing TECPLOT file


real	0m4.386s
user	0m4.529s
sys	0m0.152s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_TipTreat_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_and_aflr3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value

Writing TECPLOT file: pyCAPS_AFLR4_AFLR3.dat ....
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 - 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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 150594
	Number of elements       = 452252
	Number of triangles      = 14380
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 216820
	Number of pyramids       = 424
	Number of prisms         = 220628
	Number of hexahedrals    = 0

Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_VolMesh.dat ....
Finished writing TECPLOT file


real	0m6.365s
user	0m6.477s
sys	0m0.180s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_and_aflr3_Symmetry_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_Symmetry_PyTest.py test;
+ python -u aflr4_and_aflr3_Symmetry_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Farfield, index = 1
	Name = Symmetry, index = 2
	Name = Wing1, index = 3
	Name = Wing2, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Farfield, index = 1
	Name = Symmetry, index = 2
	Name = Wing1, index = 3
	Name = Wing2, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - Symmetry
	Done getting mesh sizing parameters
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing TECPLOT file: pyCAPS_AFLR4_Test.dat ....
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 332429
	Number of elements       = 1065072
	Number of triangles      = 44190
	Number of quadrilatarals = 1613
	Number of tetrahedrals   = 569874
	Number of pyramids       = 327
	Number of prisms         = 449068
	Number of hexahedrals    = 0

Writing TECPLOT file: pyCAPS_AFLR3_VolMesh.dat ....
Finished writing TECPLOT file


real	0m13.677s
user	0m13.691s
sys	0m0.411s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_Symmetry_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_QuadMesh_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_QuadMesh_PyTest.py test;
+ python -u aflr4_QuadMesh_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2

Writing TECPLOT file: pyCAPS_AFLR4_QuadMesh_Test.dat ....
Finished writing TECPLOT file


real	0m3.607s
user	0m9.197s
sys	0m5.158s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_QuadMesh_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_and_Tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_Tetgen_PyTest.py test;
+ python -u aflr4_and_Tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing TECPLOT file: pyCAPS_AFLR4_Tetgen.dat ....
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 - 30088, elements - 60164
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!

Writing TECPLOT file: pyCAPS_AFLR4_Tetgen_VolMesh.dat ....
Finished writing TECPLOT file


real	0m5.386s
user	0m5.484s
sys	0m0.199s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_and_Tetgen_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_tetgen_Regions_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_tetgen_Regions_PyTest.py test;
+ python -u aflr4_tetgen_Regions_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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 Sense   Edges
EGADS    :      1     Yes     1   -1 2 3 -4
EGADS    :      2     Yes     1   -5 6 7 -2
EGADS    :      3     Yes     1   8 5 9 -10
EGADS    :      4     Yes     1   10 11 -12 -13
EGADS    :      5     Yes     1   14 15 -16 -11
EGADS    :      6     Yes     1   1 -17 -14 -9
EGADS    :      7     Yes     1   -18 12 -19 -7
EGADS    :      8     Yes     1   16 20 -3 19
EGADS    :      9     Yes     1   13 18 -6 -8
EGADS    :     10     Yes     1   -15 17 4 -20
EGADS    :     11     Yes     1   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=       135       228         0
AFLR4    : Nodes, Trias,Quads=       132       222         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       136       230         0
AFLR4    : Nodes, Trias,Quads=       132       222         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=      1232      2506       464

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      1232      2506

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       140       234         0
AFLR4    : Nodes, Trias,Quads=       133       220         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=       141       236         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=       206       360         0
AFLR4    : Nodes, Trias,Quads=       193       334         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       204       356         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=      1245      2532       464

OVERALL  : CPU Time          =     0.047   seconds
Body 1 (of 1)
Number of nodes    = 1245
Number of elements = 2532
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 2532
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1245
Total number of elements = 2532
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Number of surface: nodes - 1245, elements - 2532
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.018975
Creating surface mesh ...
Surface mesh seconds:  0.000701
Recovering boundaries...
Boundary recovery seconds:  0.003982
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000338
Recovering Delaunayness...
Delaunay recovery seconds:  0.000973
Refining mesh...
Refinement seconds:  0.016469
Smoothing vertices...
Mesh smoothing seconds:  0.019041
Improving mesh...
Mesh improvement seconds:  0.000755

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

Output seconds:  0.000137
Total running seconds:  0.061417

Statistics:

  Input points: 1245
  Input facets: 2532
  Input segments: 3774
  Input holes: 0
  Input regions: 2

  Mesh points: 1460
  Mesh tetrahedra: 5105
  Mesh faces: 11318
  Mesh faces on exterior boundary: 2216
  Mesh faces on input facets: 2532
  Mesh edges on input segments: 3774
  Steiner points inside domain: 215

Done meshing using TetGen!

Writing VTK file: volume.vtk....
Finished writing VTK file


real	0m0.398s
user	0m0.574s
sys	0m0.085s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_tetgen_Regions_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 2236
Number of elements = 4468
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 636
Number of elements = 1268
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 258
Number of elements = 512
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 512
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 3130
Total number of elements = 6248

Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_2.dat ....
Finished writing TECPLOT file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 3130, elements - 6248
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.013141
Creating surface mesh ...
Surface mesh seconds:  0.001703
Recovering boundaries...
Boundary recovery seconds:  0.038832
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.002291
Suppressing Steiner points ...
Steiner suppression seconds:  4e-06
Recovering Delaunayness...
Delaunay recovery seconds:  0.004763
Refining mesh...
  4177 insertions, added 2144 points, 130054 tetrahedra in queue.
  1390 insertions, added 431 points, 133424 tetrahedra in queue.
  1853 insertions, added 429 points, 130659 tetrahedra in queue.
  2470 insertions, added 556 points, 115243 tetrahedra in queue.
  3293 insertions, added 486 points, 72303 tetrahedra in queue.
  4389 insertions, added 459 points, 4095 tetrahedra in queue.
Refinement seconds:  0.335495
Smoothing vertices...
Mesh smoothing seconds:  0.176403
Improving mesh...
Mesh improvement seconds:  0.006147
Jettisoning redundant points.

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

Output seconds:  0.000543
Total running seconds:  0.579469

Statistics:

  Input points: 3130
  Input facets: 6248
  Input segments: 9372
  Input holes: 2
  Input regions: 0

  Mesh points: 8153
  Mesh tetrahedra: 40225
  Mesh faces: 83575
  Mesh faces on exterior boundary: 6250
  Mesh faces on input facets: 6250
  Mesh edges on input segments: 9373
  Steiner points on input segments:  1
  Steiner points inside domain: 5022

Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.

Writing TECPLOT file: pyCAPS_Tetgen_Test.dat ....
	Binary output is not currently supported for Tecplot output
	..... switching to ASCII!
Finished writing TECPLOT file


real	0m1.272s
user	0m1.559s
sys	0m0.121s
+ status=0
+ set +x

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


=================================================
+ echo 'tetgen_Holes_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_Holes_PyTest.py test;
+ python -u tetgen_Holes_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 8995
Number of elements = 18112
Number of node elements          = 0
Number of line elements          = 0
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:  0.155235
Creating surface mesh ...
Surface mesh seconds:  0.004502
Recovering boundaries...
Boundary recovery seconds:  0.056573
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.004669
Recovering Delaunayness...
Delaunay recovery seconds:  0.036814
Refining mesh...
Refinement seconds:  0.133777
Smoothing vertices...
Mesh smoothing seconds:  0.146547
Improving mesh...
Mesh improvement seconds:  0.004748
Jettisoning redundant points.

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

Output seconds:  0.000963
Total running seconds:  0.543999

Statistics:

  Input points: 8995
  Input facets: 18112
  Input segments: 27104
  Input holes: 1
  Input regions: 0

  Mesh points: 7132
  Mesh tetrahedra: 27859
  Mesh faces: 60758
  Mesh faces on exterior boundary: 10080
  Mesh faces on input facets: 10080
  Mesh edges on input segments: 15120
  Steiner points inside domain: 2090

Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.

Writing TECPLOT file: volume.dat ....
Finished writing TECPLOT file


real	0m1.196s
user	0m1.428s
sys	0m0.083s
+ status=0
+ set +x

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


=================================================
+ echo 'tetgen_Regions_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_Regions_PyTest.py test;
+ python -u tetgen_Regions_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 8995
Number of elements = 18112
Number of node elements          = 0
Number of line elements          = 0
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:  0.157027
Creating surface mesh ...
Surface mesh seconds:  0.004593
Recovering boundaries...
Boundary recovery seconds:  0.056551
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.002518
Recovering Delaunayness...
Delaunay recovery seconds:  0.069114
Refining mesh...
Refinement seconds:  0.263262
Smoothing vertices...
Mesh smoothing seconds:  0.302179
Improving mesh...
Mesh improvement seconds:  0.008878

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

Output seconds:  0.001292
Total running seconds:  0.865583

Statistics:

  Input points: 8995
  Input facets: 18112
  Input segments: 27104
  Input holes: 0
  Input regions: 2

  Mesh points: 13158
  Mesh tetrahedra: 55587
  Mesh faces: 119206
  Mesh faces on exterior boundary: 16064
  Mesh faces on input facets: 18112
  Mesh edges on input segments: 27104
  Steiner points inside domain: 4163

Done meshing using TetGen!

Writing TECPLOT file: volume.dat ....
Finished writing TECPLOT file


real	0m1.531s
user	0m1.763s
sys	0m0.084s
+ status=0
+ set +x

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

delaundo: /Users/jenkins/util/delaundo/delaundo/src/delaundo

=================================================
+ echo 'delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6

Getting mesh sizing parameters
	Mesh sizing name - Airfoil
	Mesh sizing name - AirfoilTE
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting edge discretization for body 1
	Delaundo expects 2D meshes be 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 - delaundoMesh.mesh
	Swapping y and z coordinates!

Writing TECPLOT file: delaundoMesh.dat ....
Finished writing TECPLOT file


real	0m0.424s
user	0m0.607s
sys	0m0.254s
+ status=0
+ set +x

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

Running.... CFD PyTests


=================================================
+ echo 'su2_and_AFLR2_NodeDist_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_NodeDist_PyTest.py test;
+ python -u su2_and_AFLR2_NodeDist_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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          =     0.004   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      3715      7206
 
AFLR2    : CPU Time          =     0.000   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 be 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 (8.0.0) "


Running SU2......

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

Parsing config file for zone 0

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

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

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

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

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

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_SU2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_SU2_aflr2.
Volume file name: flow_pyCAPS_SU2_aflr2.
Restart file name: restart_flow_pyCAPS_SU2_aflr2.dat.

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

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

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

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
3715 grid points.
7206 volume elements.
4 surface markers.
98 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_4).
78 boundary elements in index 3 (Marker = BC_5).
7206 triangles.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 7206 TRIANGLE volume elements.
There has been a re-orientation of 73 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.917.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 177.06. Mean K: 1.97231. Standard deviation K: 13.0434.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        63.4343|             90|
|     CV Face Area Aspect Ratio|              1|        5.23543|
|           CV Sub-Volume Ratio|              1|        3.11804|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      3715|    1/1.00|        10|
|         1|      1048|    1/3.54|   7.96696|
|         2|       298|    1/3.52|   6.37252|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06136 m.
Area projection in the x-plane = 0.178383 m, y-plane = 0.994925 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.138389 m.
Min. coordinate in the x-direction = -0.000250564 m, y-direction = -0.0151999 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is NOT a single straight.
Computing wall distances.

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

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

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.9991e-02|   -0.385358|    2.453598|    1.625650|    5.369499|    0.360138|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.9708e-02|   -0.512634|    2.087781|    1.374671|    4.973554|    1.183036|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.9424e-02|   -0.792582|    1.733529|    1.142729|    4.657622|    3.896320|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.9280e-02|   -0.880738|    1.486539|    1.023158|    4.334759|   14.592265|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.9189e-02|   -0.987528|    1.351478|    0.932491|    4.191092|  111.166022|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.9127e-02|   -1.104038|    1.188715|    0.874764|    3.951825| -483.924340|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.9083e-02|   -1.178622|    1.124587|    0.844310|    3.820426|  127.331200|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.9050e-02|   -1.243517|    1.097463|    0.824869|    3.768858|   40.162273|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.9025e-02|   -1.287932|    1.075843|    0.810639|    3.733440|   25.154653|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.9005e-02|   -1.300689|    1.046363|    0.775886|    3.684245|   21.097801|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.30069|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_SU2_aflr2.dat  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat).
|CSV file                           |surface_flow_pyCAPS_SU2_aflr2.csv  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat).
|Tecplot binary                     |flow_pyCAPS_SU2_aflr2.szplt        |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat).
|Tecplot binary surface             |surface_flow_pyCAPS_SU2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 352 more values.0: Error finishing Tecplot file output.

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.dat).
+-----------------------------------------------------------------------+

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

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

Total Force - Pressure + Viscous
Cl =  0.650457 Cd =  0.030831
Cmz =  0.373226
Cx =  0.030831 Cy =  0.650457
Pressure Contribution
Cl_p =  0.650457 Cd_p =  0.030831
Cmz_p =  0.373226
Cx_p =  0.030831 Cy_p =  0.650457
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0

real	0m1.083s
user	0m0.977s
sys	0m0.466s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_NodeDist_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Saving geometry
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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          =     0.021   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     11156     21767
AFLR2 QI : Nodes, Faces      =     11155       819
AFLR2 QI : Nodes, Faces      =     11155     10473
AFLR2 QI : Nodes, Faces      =     11155     21765
AFLR2 QI : Nodes, Faces      =     11154       811
AFLR2 QI : Nodes, Faces      =     11154     10476
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11154       805
AFLR2 QI : Nodes, Faces      =     11154     10479
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11154       911
AFLR2 QI : Nodes, Faces      =     11154     10426
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11153       915
AFLR2 QI : Nodes, Faces      =     11153     10423
AFLR2 QI : Nodes, Faces      =     11153       917
AFLR2 QI : Nodes, Faces      =     11153     10423
 
AFLR2    : CPU Time          =     0.008   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 11153
Number of elements = 11885
Number of tris = 917
Number of quad = 10423

Writing TECPLOT file: pyCAPS_su2_aflr2.dat ....
Finished writing TECPLOT file

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 SU2 file ....
SU2 expects 2D meshes be 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 (8.0.0) "


Running SU2......

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

Parsing config file for zone 0

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  4.8466e-02|    0.071067|    2.739763|    1.616077|    5.599701|    0.055267|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  4.7346e-02|   -0.447576|    2.193837|    1.571349|    5.070382|    0.046028|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  4.6793e-02|   -0.561159|    2.074597|    1.490746|    4.953698|    0.033910|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  4.6532e-02|   -0.723326|    1.921155|    1.390756|    4.790278|    0.049695|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  4.6359e-02|   -0.876572|    1.825653|    1.275093|    4.637161|    0.133976|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  4.6239e-02|   -1.029177|    1.759196|    1.156078|    4.482282|    0.368542|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  4.6164e-02|   -1.215334|    1.704909|    1.114966|    4.286060|    0.974759|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  4.6091e-02|   -1.329970|    1.644937|    1.145030|    4.116982|    2.716332|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  4.6044e-02|   -1.270672|    1.570739|    1.155400|    4.139480|   16.569216|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  4.6009e-02|   -1.221243|    1.499646|    1.130319|    4.189559|   -6.277653|

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

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

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

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

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

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

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

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

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

real	0m1.356s
user	0m1.460s
sys	0m0.664s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_AFLR4_AFLR3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR4_AFLR3_PyTest.py test;
+ python -u su2_and_AFLR4_AFLR3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value

Writing TECPLOT file: AFLR4_Mesh.dat ....
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 38502
	Number of elements       = 221920
	Number of triangles      = 12446
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 209474
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: AFLR3_Mesh.dat ....
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 (8.0.0) "


Running SU2......

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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 50 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 15.8114 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_1 (0, 0, 0).
   - BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Input mesh file name: ../aflr3/aflr3_0.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.
38502 grid points.
209474 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).
209474 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: 61.8683. 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.)|        25.7373|        86.6783|
|     CV Face Area Aspect Ratio|        1.09466|        7304.38|
|           CV Sub-Volume Ratio|        1.04044|        69268.7|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     38502|    1/1.00|        10|
|         1|      6385|    1/6.03|   8.24107|
|         2|      1003|    1/6.37|   6.66994|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 118.038 m^2.
Area projection in the x-plane = 11.1422 m^2, y-plane = 4.96709 m^2, z-plane = 55.4183 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.582636 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  6.0343e-01|   -0.060087|    2.302216|    2.037805|    5.430808|    1.979346|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  5.9174e-01|   -0.010036|    2.482646|    2.186974|    5.492648|    2.690164|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  5.8735e-01|    0.015122|    2.560028|    2.424390|    5.513110|    4.144990|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  5.8463e-01|   -0.037042|    2.579202|    2.559777|    5.446956|    6.076344|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  5.8209e-01|   -0.081173|    2.578114|    2.616175|    5.391591|    7.699778|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  5.7999e-01|   -0.085972|    2.582416|    2.631873|    5.398797|    8.892926|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  5.7895e-01|   -0.096180|    2.574091|    2.638010|    5.401796|    9.787209|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  5.7824e-01|   -0.128924|    2.539338|    2.641609|    5.371412|   10.317352|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  5.7770e-01|   -0.184841|    2.469269|    2.632268|    5.306572|   10.430833|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  5.7771e-01|   -0.254301|    2.406660|    2.598073|    5.225779|   10.218562|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|     -0.254301|          < -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 =  0.799154 Cd =  0.078206
Cmx =  0.000491 Cmy =  -0.204969 Cmz =  0.000591
Cx =  0.064247 Cy =  0.000689 Cz =  0.800398
Pressure Contribution
Cl_p =  0.799154 Cd_p =  0.078206
Cmx_p =  0.000491 Cmy_p =  -0.204969 Cmz_p =  0.000591
Cx_p =  0.064247 Cy_p =  0.000689 Cz_p =  0.800398
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	0m15.918s
user	0m15.793s
sys	0m0.409s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR4_AFLR3_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_Morph_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_Morph_PyTest.py test;
+ python -u su2_Morph_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value

Writing TECPLOT file: pyCAPS_AFLR4_AFLR3.dat ....
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 55692
	Number of elements       = 322597
	Number of triangles      = 15872
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 306725
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_VolMesh.dat ....
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 (8.0.0) "


Running SU2......

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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 40 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 14.1421 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_1 (0, 0, 0).
   - BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Surface(s) affected by the design variables: BC_1, BC_2.
Input mesh file name: ../volumeMesh/aflr3_0.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.
55692 grid points.
306725 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).
306725 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: 58.8178. 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.)|        17.6334|        85.6893|
|     CV Face Area Aspect Ratio|        1.03551|        10026.2|
|           CV Sub-Volume Ratio|        1.03837|        55476.6|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     55692|    1/1.00|        10|
|         1|      9209|    1/6.05|   8.23312|
|         2|      1415|    1/6.51|    6.6146|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.07107 m.
Wetted area = 96.2324 m^2.
Area projection in the x-plane = 7.65774 m^2, y-plane = 4.21853 m^2, z-plane = 45.5887 m^2.
Max. coordinate in the x-direction = 12.3872 m, y-direction = 7.07107 m, z-direction = 0.521791 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.0650201 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  9.1763e-01|   -0.456432|    1.874717|    1.658147|    5.034463|    0.751359|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.0711e-01|   -0.486415|    2.011739|    1.708650|    5.010503|    1.410135|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  8.9890e-01|   -0.426910|    2.085510|    1.930071|    5.059947|    3.183469|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  8.8589e-01|   -0.413221|    2.123390|    2.080595|    5.061524|    6.846574|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  8.8600e-01|   -0.415069|    2.144313|    2.168724|    5.045574|   12.481741|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  8.7966e-01|   -0.408728|    2.161839|    2.210835|    5.050178|   19.569122|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  8.7490e-01|   -0.400272|    2.162405|    2.231094|    5.064509|   27.279075|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  8.7135e-01|   -0.415420|    2.140420|    2.247896|    5.053374|   31.968213|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  8.6864e-01|   -0.459344|    2.092599|    2.258672|    5.008518|   30.523517|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  8.6648e-01|   -0.475584|    2.031862|    2.254220|    4.985969|   25.858195|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|     -0.475584|          < -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 =  0.52098 Cd =  0.020148
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 (8.0.0) "


Mesh Morphing......

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

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: aflr3_0.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: aflr3_0.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.
55692 grid points.
306725 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).
306725 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 4.286509 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |aflr3_0.su2                        |
|CSV file                           |surface_deformed.csv               |
|Paraview                           |volume_deformed.vtu                |
|Paraview surface                   |surface_deformed.vtu               |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------



Running SU2......

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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 40 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 14.1421 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_1 (0, 0, 0).
   - BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Surface(s) affected by the design variables: BC_1, BC_2.
Input mesh file name: aflr3_0.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.
55692 grid points.
306725 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).
306725 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.)|        17.5434|        84.9572|
|     CV Face Area Aspect Ratio|        1.03956|        11174.7|
|           CV Sub-Volume Ratio|        1.03737|        76809.1|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     55692|    1/1.00|        10|
|         1|      9209|    1/6.05|   8.23312|
|         2|      1415|    1/6.51|    6.6146|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.07107 m.
Wetted area = 95.6308 m^2.
Area projection in the x-plane = 9.17945 m^2, y-plane = 4.04295 m^2, z-plane = 44.962 m^2.
Max. coordinate in the x-direction = 12.3585 m, y-direction = 7.07107 m, z-direction = 0.521791 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.400127 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  9.0574e-01|   -0.395911|    1.980314|    1.646923|    5.094985|    1.913176|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  8.7872e-01|   -0.263244|    2.226198|    1.949589|    5.238568|    2.547049|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  8.6943e-01|   -0.208348|    2.309357|    2.198185|    5.285085|    3.914397|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  8.6676e-01|   -0.234717|    2.345148|    2.348550|    5.245683|    5.879161|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  8.7009e-01|   -0.273135|    2.359089|    2.421633|    5.194487|    7.767865|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  8.6613e-01|   -0.284384|    2.368405|    2.446997|    5.189344|    9.270982|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  8.6330e-01|   -0.294753|    2.363090|    2.455733|    5.191507|   10.462882|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  8.6119e-01|   -0.319538|    2.340251|    2.466131|    5.173062|   11.320106|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  8.5958e-01|   -0.349768|    2.292885|    2.471955|    5.137977|   11.778124|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  8.5835e-01|   -0.372277|    2.234008|    2.463003|    5.106430|   11.856729|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|     -0.372277|          < -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 =  0.074504

real	0m38.197s
user	0m36.747s
sys	0m1.417s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_Morph_PyTest.py passed (as expected)
=================================================

delaundo: /Users/jenkins/util/delaundo/delaundo/src/delaundo

=================================================
+ echo 'su2_and_Delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_Delaundo_PyTest.py test;
+ python -u su2_and_Delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting edge discretization for body 1
	Delaundo expects 2D meshes be 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 - delaundoMesh.mesh
	Swapping y and z coordinates!

Writing TECPLOT file: delaundoMesh.dat ....
Finished writing TECPLOT file


Writing SU2 file ....
SU2 expects 2D meshes be 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 (8.0.0) "


Running SU2......

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

Parsing config file for zone 0

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

Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../delaundo/delaundoMesh.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_delaundoMesh.dat.
Surface file name: surface_flow_delaundoMesh.
Volume file name: flow_delaundoMesh.
Restart file name: restart_flow_delaundoMesh.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.
6317 grid points.
12340 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).
12340 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|        89.2595|
|     CV Face Area Aspect Ratio|        1.03245|        15.7138|
|           CV Sub-Volume Ratio|              1|        7.93643|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      6317|    1/1.00|        10|
|         1|      1792|    1/3.53|   7.98923|
|         2|       509|    1/3.52|   6.38684|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.07206 m.
Area projection in the x-plane = 0.179342 m, y-plane = 1.00053 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.138492 m.
Min. coordinate in the x-direction = -0.00104578 m, y-direction = -0.0151891 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is a single straight.
Computing wall distances.

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

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

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  3.4739e-02|   -1.163068|    1.073873|    1.341547|    4.312268|    0.062082|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  3.4350e-02|   -1.558471|    0.813117|    0.969484|    3.926501|    0.143132|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  3.4045e-02|   -1.599269|    0.950037|    1.012154|    3.879885|    0.386300|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  3.3708e-02|   -1.661284|    1.005970|    1.023067|    3.797319|    0.981260|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  3.3583e-02|   -1.658421|    1.009907|    0.965279|    3.792658|    2.399755|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  3.3437e-02|   -1.630602|    0.996801|    0.859556|    3.833204|    6.390579|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  3.3334e-02|   -1.628009|    1.002770|    0.822847|    3.846297|   27.872536|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  3.3263e-02|   -1.646113|    1.024424|    0.882502|    3.830202|  -48.293527|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  3.3197e-02|   -1.672152|    1.033657|    0.939200|    3.797228|  -22.113788|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  3.3145e-02|   -1.695131|    1.018255|    0.944150|    3.765919|  -19.281368|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.69513|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_delaundoMesh.dat      |

Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|CSV file                           |surface_flow_delaundoMesh.csv      |

Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|Tecplot binary                     |flow_delaundoMesh.szplt            |

Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|Tecplot binary surface             |surface_flow_delaundoMesh.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_delaundoMesh.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 =  0.805707 Cd =  -0.041787
Cmz =  0.408515
Cx =  -0.041787 Cy =  0.805707
Pressure Contribution
Cl_p =  0.805707 Cd_p =  -0.041787
Cmz_p =  0.408515
Cx_p =  -0.041787 Cy_p =  0.805707
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0

real	0m1.064s
user	0m1.166s
sys	0m0.468s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_Delaundo_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_Tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_Tetgen_PyTest.py test;
+ python -u su2_and_Tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 2236
Number of elements = 4468
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 636
Number of elements = 1268
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 258
Number of elements = 512
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 512
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 3130
Total number of elements = 6248

Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_2.dat ....
Finished writing TECPLOT file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 3130, elements - 6248
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.013066
Creating surface mesh ...
Surface mesh seconds:  0.001847
Recovering boundaries...
Boundary recovery seconds:  0.034094
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.002338
Suppressing Steiner points ...
Steiner suppression seconds:  6e-06
Recovering Delaunayness...
Delaunay recovery seconds:  0.004642
Refining mesh...
  4180 insertions, added 2061 points, 130359 tetrahedra in queue.
  1391 insertions, added 425 points, 134059 tetrahedra in queue.
  1855 insertions, added 465 points, 131734 tetrahedra in queue.
  2472 insertions, added 531 points, 115562 tetrahedra in queue.
  3296 insertions, added 526 points, 67935 tetrahedra in queue.
  4393 insertions, added 433 points, 372 tetrahedra in queue.
  5856 insertions, added 571 points, 794 tetrahedra in queue.
Refinement seconds:  0.316925
Smoothing vertices...
Mesh smoothing seconds:  0.17725
Improving mesh...
Mesh improvement seconds:  0.005959
Jettisoning redundant points.

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

Output seconds:  0.000615
Total running seconds:  0.556874

Statistics:

  Input points: 3130
  Input facets: 6248
  Input segments: 9372
  Input holes: 2
  Input regions: 0

  Mesh points: 8154
  Mesh tetrahedra: 40351
  Mesh faces: 83827
  Mesh faces on exterior boundary: 6250
  Mesh faces on input facets: 6250
  Mesh edges on input segments: 9373
  Steiner points on input segments:  1
  Steiner points inside domain: 5023

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 (8.0.0) "


Running SU2......

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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 50 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 15.8114 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_1 (0, 0, 0).
   - BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Input mesh file name: ../myMesh/tetgen_0.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.
8154 grid points.
40351 volume elements.
3 surface markers.
4468 boundary elements in index 0 (Marker = BC_1).
1270 boundary elements in index 1 (Marker = BC_2).
512 boundary elements in index 2 (Marker = BC_3).
40351 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: 2.08741e+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: 30.6158. Standard deviation K: 37.5195.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        1.93303|        83.8522|
|     CV Face Area Aspect Ratio|        1.66492|        8220.52|
|           CV Sub-Volume Ratio|         1.0945|         249103|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      8154|    1/1.00|        10|
|         1|      1365|    1/5.97|   8.26695|
|         2|       222|    1/6.15|   6.76877|
+-------------------------------------------+
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 = 4.5843 m^2, z-plane = 57.287 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.557773 m.
Min. coordinate in the x-direction = -0.00409054 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.0667e-01|    0.616284|    3.048260|    2.091357|    6.107180|    1.815389|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.0573e-01|    0.741001|    3.258088|    2.952168|    6.243294|    2.156707|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.0512e-01|    0.650783|    3.322878|    3.201040|    6.147243|    3.157692|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.0478e-01|    0.569960|    3.293032|    3.250810|    6.036360|    4.529265|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.0456e-01|    0.533226|    3.191940|    3.195181|    5.994483|    5.686317|

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

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      0.533226|         < -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 =  0.757437 Cd =  0.133203
Cmx =  -0.003663 Cmy =  -0.214942 Cmz =  0.000732
Cx =  0.119964 Cy =  0.000385 Cz =  0.759646

real	0m2.532s
user	0m2.681s
sys	0m0.245s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_Tetgen_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_X43a_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_X43a_PyTest.py test;
+ python -u su2_X43a_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = x43A, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 3801
Number of elements = 7602
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 7602
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 5678
Number of elements = 11352
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 11352
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9479
Total number of elements = 18954

Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
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 - 9479, elements - 18954
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.030835
Creating surface mesh ...
Surface mesh seconds:  0.006251
Recovering boundaries...
Boundary recovery seconds:  0.076281
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.005186
Recovering Delaunayness...
Delaunay recovery seconds:  0.013295
Refining mesh...
  12636 insertions, added 5223 points, 13721 tetrahedra in queue.
Refinement seconds:  0.302265
Smoothing vertices...
Mesh smoothing seconds:  0.222505
Improving mesh...
Mesh improvement seconds:  0.009628
Jettisoning redundant points.

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

Output seconds:  0.001602
Total running seconds:  0.66806

Statistics:

  Input points: 9479
  Input facets: 18954
  Input segments: 28431
  Input holes: 1
  Input regions: 0

  Mesh points: 14887
  Mesh tetrahedra: 61377
  Mesh faces: 132231
  Mesh faces on exterior boundary: 18954
  Mesh faces on input facets: 18954
  Mesh edges on input segments: 28431
  Steiner points inside domain: 5408

Done meshing using TetGen!

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 (8.0.0) "


Running SU2......

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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 3.5.
Angle of attack (AoA): 3 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_1.

Surface(s) plotted in the output file: BC_1.
Input mesh file name: ../myMesh/tetgen_0.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.
14887 grid points.
61377 volume elements.
2 surface markers.
7602 boundary elements in index 0 (Marker = BC_1).
11352 boundary elements in index 1 (Marker = BC_2).
61377 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: 2.67745e+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: 0.525135. Standard deviation K: 2.58749.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        5.16386|        84.6502|
|     CV Face Area Aspect Ratio|        1.64402|        2742.24|
|           CV Sub-Volume Ratio|              1|    1.84831e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     14887|    1/1.00|        10|
|         1|      2696|    1/5.52|    8.4865|
|         2|       504|    1/5.35|   7.27875|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30 m.
Wetted area = 13592.9 m^2.
Area projection in the x-plane = 761.52 m^2, y-plane = 2060.65 m^2, z-plane = 5463.74 m^2.
Max. coordinate in the x-direction = 150 m, y-direction = 30 m, z-direction = 19 m.
Min. coordinate in the x-direction = 0 m, y-direction = -30 m, z-direction = -10.3 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        916077|             1|   m^2/s^2|        916077|
|            Velocity-X|       1189.41|             1|       m/s|       1189.41|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       62.3342|             1|       m/s|       62.3342|
|    Velocity Magnitude|       1191.04|             1|       m/s|       1191.04|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           3.5|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.0177e-01|    2.730964|    5.665275|    4.731423|    8.730439|   -0.395648|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.9484e-01|    3.174156|    6.235391|    5.715889|    9.174756|   -0.117154|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.9141e-01|    3.277847|    6.355257|    5.895285|    9.253987|   -0.024962|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.9018e-01|    3.266256|    6.318770|    5.740790|    9.221197|   -0.009379|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.8946e-01|    3.237301|    6.293206|    5.572048|    9.228342|   -0.028277|

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

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|        3.2373|         < -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 122 non-physical points in the solution.
Warning: 66 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 =  -3.304274 Cd =  116.853222
Cmx =  1.489219 Cmy =  8823.598105 Cmz =  124.696329
Cx =  116.866011 Cy =  1.290643 Cz =  2.815879

real	0m4.938s
user	0m6.605s
sys	0m0.868s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_X43a_PyTest.py passed (as expected)
=================================================

./execute_PyTestRegression.sh: line 413: ulimit: stack size: cannot modify limit: Operation not permitted
flowCart: /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC//flowCart

=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ python -u cart3d_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.796888
 Tessellating body 1 with  MaxEdge = 0.094922  Sag = 0.003797  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 6 -maxR 9  > autoInputs.out
 Executing: ./aero.csh > aero.out
C_A  0.023693377
C_Y  -0.0012129282
C_N  0.065395002
C_D  0.025961197
C_S  -0.0012129282
C_L  0.064528278
C_l  0.0510971
C_m  0.000248187
C_n  -0.017525
C_M_x  0.0504544
C_M_y  0.000248187
C_M_z  -0.0192976

real	0m8.475s
user	0m14.972s
sys	0m0.331s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'cart3d_OpenMDAO_3_alpha_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_alpha_PyTest.py test;
+ python -u cart3d_OpenMDAO_3_alpha_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
----------------------------------------
>>> alpha [2.]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - alpha
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 1
	Objective name - CL2
	Done getting CFD functional
 Body size = 3.625615
 Tessellating body 1 with  MaxEdge = 0.090640  Sag = 0.003626  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 7  -mesh2d > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:41:00) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (20:41:02) aero.csh done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.01631562]  CL 0.12773309
----------------------------------------
----------------------------------------
>>> alpha [2.]
>>> CL2 [0.01631562]  CL 0.12773309
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:41:03) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (20:41:04) 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
   (20:41:05) Linearizing cut-cells
   (20:41:05) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:41:05) Computing gradients
   (20:41:09) ... done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[0.01572627]]
========================================
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            1     M =           10

At X0         0 variables are exactly at the bounds

At iterate    0    f=  1.63156D-02    |proj g|=  1.57263D-02
----------------------------------------
>>> alpha [1.98427373]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:41:09) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1
   (20:41:11) aero.csh done
 o case M0.5901A1.98427B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.01606724]  CL 0.12675617
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:41:11) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1
   (20:41:13) 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
   (20:41:13) Linearizing cut-cells
   (20:41:13) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:41:13) Computing gradients
   (20:41:17) ... done
 o case M0.5901A1.98427B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[0.01560329]]
========================================

At iterate    1    f=  1.60672D-02    |proj g|=  1.56033D-02
----------------------------------------
>>> alpha [-0.01099175]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:41:18) Running aero.csh on 2 core(s) in M0.5901A-0.0109917B0_DP1
   (20:41:19) aero.csh done
 o case M0.5901A-0.0109917B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [6.05653711e-06]  CL 0.00246101
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:41:20) Running aero.csh on 2 core(s) in M0.5901A-0.0109917B0_DP1
   (20:41:22) 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
   (20:41:22) Linearizing cut-cells
   (20:41:22) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:41:22) Computing gradients
   (20:41:26) ... done
 o case M0.5901A-0.0109917B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[0.00031042]]
========================================

At iterate    2    f=  6.05654D-06    |proj g|=  3.10424D-04
----------------------------------------
>>> alpha [-0.05149286]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:41:26) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1
   (20:41:28) aero.csh done
 o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [2.59817062e-10]  CL 1.612e-05
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:41:29) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1
   (20:41:30) 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
   (20:41:31) Linearizing cut-cells
   (20:41:31) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:41:31) Computing gradients
   (20:41:35) ... done
 o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[2.03612433e-06]]
========================================

At iterate    3    f=  2.59817D-10    |proj g|=  2.03612D-06
----------------------------------------
>>> alpha [-0.05176027]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:41:35) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1
   (20:41:37) aero.csh done
 o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [9.25766089e-15]  CL 1e-07
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:41:37) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1
   (20:41:39) 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
   (20:41:39) Linearizing cut-cells
   (20:41:39) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:41:39) Computing gradients
   (20:41:43) ... done
 o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[1.21372408e-08]]
========================================

At iterate    4    f=  9.25766D-15    |proj g|=  1.21372D-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   9.258D-15
  F =   9.2576608860000000E-015

CONVERGENCE: NORM_OF_PROJECTED_GRADIENT_<=_PGTOL            
Optimization Complete
-----------------------------------
Optimized value: [-0.05176027]

real	0m44.750s
user	0m30.226s
sys	0m4.693s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_alpha_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'cart3d_OpenMDAO_3_twist_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_twist_PyTest.py test;
+ python -u cart3d_OpenMDAO_3_twist_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
----------------------------------------
>>> twist [4.]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - twist
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 1
	Objective name - CL2
	Done getting CFD functional
 Body size = 3.630958
 Tessellating body 1 with  MaxEdge = 0.018155  Sag = 0.000908  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:41:45) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:41:53) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.00411365]  CL 0.0641354
----------------------------------------
----------------------------------------
>>> twist [4.]
>>> CL2 [0.00411365]  CL 0.0641354
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:41:54) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:42:04) 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
   (20:42:04) Linearizing cut-cells
   (20:42:06) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:42:06) Computing gradients
   (20:42:10) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[0.00210056]]
========================================
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            1     M =           10

At X0         0 variables are exactly at the bounds

At iterate    0    f=  4.11365D-03    |proj g|=  2.10056D-03
----------------------------------------
>>> twist [3.99789944]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.630955
 Tessellating body 1 with  MaxEdge = 0.018155  Sag = 0.000908  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:42:12) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:42:19) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.0041123]  CL 0.0641197
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:42:20) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:42:30) 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
   (20:42:30) Linearizing cut-cells
   (20:42:32) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:42:32) Computing gradients
   (20:42:36) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[0.00210014]]
========================================

At iterate    1    f=  4.11230D-03    |proj g|=  2.10014D-03
----------------------------------------
>>> twist [-6.51746917]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.635732
 Tessellating body 1 with  MaxEdge = 0.018179  Sag = 0.000909  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:42:38) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:42:45) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.00998116]  CL -0.099904
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:42:46) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:42:56) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               37089
              Estimated cutter memory:  0.003709 GB / DV
              Estimated xsensit memory: 0.070469 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (20:42:56) Linearizing cut-cells
   (20:42:58) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:42:58) Computing gradients
   (20:43:02) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[-0.003197]]
========================================
----------------------------------------
>>> twist [-0.14353734]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.625762
 Tessellating body 1 with  MaxEdge = 0.018129  Sag = 0.000906  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:43:04) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:43:11) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [6.66921728e-08]  CL -0.00023482
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:43:12) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:43:22) 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
   (20:43:22) Linearizing cut-cells
   (20:43:24) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:43:24) Computing gradients
   (20:43:28) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[-8.5476956e-06]]
========================================

At iterate    2    f=  6.66922D-08    |proj g|=  8.54770D-06
----------------------------------------
>>> twist [-0.12674978]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.625744
 Tessellating body 1 with  MaxEdge = 0.018129  Sag = 0.000906  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:43:30) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:43:37) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [5.57224144e-09]  CL 0.00010424
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:43:38) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:43:48) 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
   (20:43:48) Linearizing cut-cells
   (20:43:50) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:43:50) Computing gradients
   (20:43:54) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[2.4723127e-06]]
========================================

At iterate    3    f=  5.57224D-09    |proj g|=  2.47231D-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   2.472D-06   5.572D-09
  F =   5.5722414353000007E-009

CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-0.12674978]

real	2m10.788s
user	2m56.388s
sys	0m5.267s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_twist_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'fun3d_Morph_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
fun3d_Morph_PyTest.py test;
+ python -u fun3d_Morph_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing TECPLOT file: pyCAPS_AFLR4_AFLR3.dat ....
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 81189
	Number of elements       = 474220
	Number of triangles      = 15680
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 458540
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_VolMesh.dat ....
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	0m5.169s
user	0m5.152s
sys	0m0.312s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case fun3d_Morph_PyTest.py passed (as expected)
=================================================

Running.... STRUCTURE PyTests


=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results mass properties.....

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 1159
Number of elements = 798
Number of node elements          = 0
Number of line elements          = 0
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      3.428666259746
Mass      5383.006027801
Centroid  [1.222256036872, 0.1634981473779, -4.406149178354e-11]
CG        [1.222256036872, 0.1634981473779, -4.406161310553e-11]
Ixx       22133.97306028
Iyy       23448.30046701
Izz       1389.213122561
Ixy       164.2055275652
Ixz       -7.483326592478e-06
Iyz       1.710428542532e-06
I         [22133.97306028, 23448.30046701, 1389.213122561, 164.2055275652, -7.483326592478e-06, 1.710428542532e-06]
II        [[22133.97306028, -164.2055275652, 7.483326592478e-06], [-164.2055275652, 23448.30046701, -1.710428542532e-06], [7.483326592478e-06, -1.710428542532e-06, 1389.213122561]]

real	0m3.244s
user	0m4.530s
sys	0m7.789s
+ status=0
+ set +x

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


=================================================
+ echo 'masstran_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_AGARD445_PyTest.py test;
+ python -u masstran_AGARD445_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results mass properties.....

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

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = constEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 36
	Number of elements = 25
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 25

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

Getting FEA properties.......
	Number of properties - 1
	Property name - yatesPlate
	Done getting FEA properties
Updating mesh element types based on properties input
Area      547.7004
Mass      0.01605224431138
Centroid  [20.03586282449, 14.01686746988, 0.0]
CG        [20.03586282449, 14.01686746988, 0.0]
Ixx       1.140246300554
Iyy       0.919317482675
Izz       2.059563783229
Ixy       0.7352134614013
Ixz       0.0
Iyz       0.0
I         [1.140246300554, 0.919317482675, 2.059563783229, 0.7352134614013, 0.0, 0.0]
II        [[1.140246300554, -0.7352134614013, -0.0], [-0.7352134614013, 0.919317482675, -0.0], [-0.0, -0.0, 2.059563783229]]

real	0m0.264s
user	0m0.320s
sys	0m0.068s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case masstran_AGARD445_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

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

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

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

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

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

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

real	0m0.405s
user	0m0.624s
sys	0m0.048s
+ status=0
+ set +x

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


=================================================
+ echo 'hsm_CantileverPlate_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_CantileverPlate_PyTest.py test;
+ python -u hsm_CantileverPlate_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = plate, index = 1

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

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

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

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

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

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

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

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.314E+01  0.628E+01  0.000E+00    0.080  ddx @ (   1.00   0.00   0.00)
   1*   0.341E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   1*   0.326E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   1*   0.438E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   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   0.00   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   0.03   0.00)
   3*   0.623E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.03   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   0.03   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   0.07   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*   0.193E-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   0.07   0.00)
   7*   0.259E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   7*   0.297E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   7*   0.435E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   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   0.00   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   0.00   0.00)
   9*   0.330E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   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   0.00   0.00)
  10*   0.239E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  10*   0.393E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  iter     dr         dd         dp         rlx   max
  11    0.257E+00  0.120E+01  0.614E-08    0.417  ddz @ (   1.00   0.00   0.00)
  11*   0.206E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   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   0.00   0.00)
  12*   0.238E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  12*   0.357E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  12*   0.849E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
  13    0.393E-01  0.238E+00  0.325E-07    1.000  ddx @ (   1.00   0.07   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   0.10   0.00)
  14    0.475E-03  0.514E-02  0.635E-07    1.000  ddx @ (   1.00   0.10   0.00)
  15    0.893E-06  0.651E-06  0.135E-08    1.000  drx @ (   1.00   0.00   0.00)
  16    0.574E-10  0.216E-09  0.140E-11    1.000  ddx @ (   0.44   0.00   0.00)
  17    0.148E-15  0.575E-15  0.104E-14    1.000  dps @ (   1.00   0.10   0.00)

 Converging n vectors ...
 it =  1    dn =  0.193E+01   rlx = 1.000  (   9 )
 it =  2    dn =  0.423E-15   rlx = 1.000  (  31 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.285E+01   rlx = 0.351  (  24 )
 it =  2    de =  0.269E+01   rlx = 0.372  (  14 )
 it =  3    de =  0.202E+01   rlx = 0.494  (  40 )
 it =  4    de =  0.122E+01   rlx = 0.820  (  40 )
 it =  5    de =  0.378E+00   rlx = 1.000  (  40 )
 it =  6    de =  0.127E-01   rlx = 1.000  (  14 )
 it =  7    de =  0.524E-06   rlx = 1.000  (  40 )
 it =  8    de =  0.938E-16   rlx = 1.000  (  22 )

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

real	0m0.338s
user	0m0.493s
sys	0m0.046s
+ status=0
+ set +x

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

ASTROS_ROOT: /Users/jenkins/util/astros/Astros/Darwin-64bit

=================================================
+ echo 'astros_Aeroelastic_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Aeroelastic_PyTest.py test;
+ python -u astros_Aeroelastic_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
	Name = Wing, index = 7
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 368
	Number of elements = 527
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 194
	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 = 369
	Combined Number of elements = 528
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 194
	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
	43 automatic connections were made for capsConnect Rib_Root (node id 369)
	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

real	0m6.265s
user	0m11.626s
sys	0m5.797s
+ status=0
+ set +x

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


=================================================
+ echo 'astros_AGARD445_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_AGARD445_PyTest.py test;
+ python -u astros_AGARD445_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results natural frequencies.....
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = constEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = yatesPlate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 36
	Number of elements = 25
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 25
Aero_Reference value is NULL - No aero reference parameters set

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 2
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
Natural freq (Mode 1) = 5.78 (Hz)
Natural freq (Mode 2) = 30.66 (Hz)

real	0m0.375s
user	0m0.513s
sys	0m0.098s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_AGARD445_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'astros_Composite_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Composite_PyTest.py test;
+ python -u astros_Composite_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = plate, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - plate
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plateTip, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 15
	Number of elements = 8
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 8
Aero_Reference value is NULL - No aero reference parameters set

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - cantilever
	No "constraintType" specified for Constraint tuple cantilever, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
	Writing coordinate system cards

real	0m0.473s
user	0m0.677s
sys	0m0.100s
+ status=0
+ set +x

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


=================================================
+ echo 'astros_CompositeWingFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_CompositeWingFreq_PyTest.py test;
+ python -u astros_CompositeWingFreq_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results for natural frequencies.....
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = wing, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - wing
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = wing, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = wing, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 402
	Number of elements = 763
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 763
	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) = 5.92088 (Hz)
Natural freq (Mode 2) = 29.77630 (Hz)
Natural freq (Mode 3) = 39.17100 (Hz)
Natural freq (Mode 4) = 77.68370 (Hz)
Natural freq (Mode 5) = 99.80360 (Hz)
Natural freq (Mode 6) = 145.83600 (Hz)
Natural freq (Mode 7) = 177.88500 (Hz)
Natural freq (Mode 8) = 237.90000 (Hz)
Natural freq (Mode 9) = 280.01500 (Hz)
Natural freq (Mode 10) = 305.57400 (Hz)
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 402 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 = 402 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 = 402 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 = 402 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 = 402 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	0m16.236s
user	0m16.143s
sys	0m0.364s
+ status=0
+ set +x

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


=================================================
+ echo 'astros_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ python -u astros_Flutter_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

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

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

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

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

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

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

real	0m0.691s
user	0m0.810s
sys	0m0.182s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected)
=================================================


=================================================
+ echo 'astros_MultipleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_MultipleLoadCase_PyTest.py test;
+ python -u astros_MultipleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 16
	Number of elements = 9
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 9
Aero_Reference value is NULL - No aero reference parameters set

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

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

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

Getting FEA loads.......
	Number of loads - 5
	Load name - load_0
	Load name - load_1
	Load name - load_2
	Load name - load_3
	Load name - load_4
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 5
	Analysis name - load_0
	Analysis name - load_1
	Analysis name - load_2
	Analysis name - load_3
	Analysis name - load_4
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_2, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_3, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_4, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

real	0m0.561s
user	0m0.758s
sys	0m0.106s
+ status=0
+ set +x

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


=================================================
+ echo 'astros_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_PyTest.py test;
+ python -u astros_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results for natural frequencies.....
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 293
Number of elements = 217
Number of node elements          = 0
Number of line elements          = 0
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	0m8.235s
user	0m9.332s
sys	0m7.967s
+ status=0
+ set +x

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


=================================================
+ echo 'astros_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_SingleLoadCase_PyTest.py test;
+ python -u astros_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 6
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 6
Aero_Reference value is NULL - No aero reference parameters set

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

real	0m0.466s
user	0m0.672s
sys	0m0.098s
+ status=0
+ set +x

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


=================================================
+ echo 'astros_ThreeBarFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBarFreq_PyTest.py test;
+ python -u astros_ThreeBarFreq_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results for natural frequencies.....
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

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

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - BoundaryCondition
	No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 2
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
Natural freq (Mode 1) = 86.13400 (Hz)
Natural freq (Mode 2) = 168.53300 (Hz)

real	0m0.468s
user	0m0.671s
sys	0m0.100s
+ status=0
+ set +x

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


=================================================
+ echo 'astros_ThreeBarLinkDesign_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBarLinkDesign_PyTest.py test;
+ python -u astros_ThreeBarLinkDesign_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

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

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

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

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

Getting FEA optimization control.......
Done getting FEA Optimization Control

Getting FEA design variables.......
	Number of design variables          - 3
	Design_Variable name - Bar1A
	Design_Variable name - Bar2A
	Design_Variable name - Bar3A
	Design_Variable_Relation name - Bar1A
	Design_Variable_Relation name - Bar2A
	Design_Variable_Relation name - Bar3A
	Number of design variable relations - 3
	Done getting FEA design variables

Getting FEA design constraints.......
	Number of design constraints - 3
	Design_Constraint name - stress1
	Design_Constraint name - stress2
	Design_Constraint name - stress3
Done getting FEA design constraints

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

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing design constraint cards
	Writing load cards
	Writing material cards
	Writing property cards
	Writing design variable cards


Running Astros......
Done running Astros!

real	0m0.552s
user	0m0.753s
sys	0m0.103s
+ status=0
+ set +x

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


=================================================
+ echo 'astros_ThreeBarMultiLoad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBarMultiLoad_PyTest.py test;
+ python -u astros_ThreeBarMultiLoad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

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

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 2
	Constraint name - conOne
	No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement"
	Constraint name - conTwo
	No "constraintType" specified for Constraint tuple conTwo, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 2
	Load name - loadOne
	Load name - loadTwo
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 2
	Analysis name - analysisOne
	Analysis name - analysisTwo
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards

real	0m0.479s
user	0m0.681s
sys	0m0.101s
+ status=0
+ set +x

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


=================================================
+ echo 'astros_ThreeBar_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_ThreeBar_PyTest.py test;
+ python -u astros_ThreeBar_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
WARNING:: WireBody is non-manifold
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = boundary, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = force, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = bar1, index = 1
	Name = bar2, index = 2
	Name = bar3, index = 3
	capsIgnore attribute found for edge - 3!!
capsIgnore attribute found. Removing unneeded nodes and elements from mesh!
Removing unused nodes...
	Removed 0 (out of 4) unused nodes!
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 4
	Number of elements = 3
	Elemental Nodes = 0
	Elemental Rods  = 3
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

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

Getting FEA properties.......
	Number of properties - 3
	Property name - bar1
	Property name - bar2
	Property name - bar3
	Done getting FEA properties
Updating mesh element types based on properties input

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards

real	0m0.461s
user	0m0.664s
sys	0m0.100s
+ status=0
+ set +x

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


=================================================
+ echo 'astros_Trim_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Trim_15degree.py test;
+ python -u astros_Trim_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

Getting FEA properties.......
	Number of properties - 3
	Property name - Body
	Property name - Edge
	Property name - Root
	Done getting FEA properties
Updating mesh element types based on properties input

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

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

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Root
	No "groupName" specified for Connection tuple Root!
	Looking for automatic connections from the use of capsConnectLink for Root
	8 automatic connections were made for capsConnect Root (node id 97)
	Done getting FEA connections

Getting FEA loads.......
	Number of loads - 2
	Load name - GravityLoad
	No "groupName" specified for Load tuple GravityLoad, going to use load name
	Load name - PointLoad
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

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

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

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

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

Writing Astros instruction file....
	Writing aeros card
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing support cards
	Writing material cards
	Writing property cards
	Writing aeroelastic cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

real	0m0.667s
user	0m0.812s
sys	0m0.159s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Trim_15degree.py passed (as expected)
=================================================

Running.... AEROELASTIC PyTests


=================================================
+ echo 'aeroelasticSimple_Pressure_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Pressure_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Pressure_SU2_and_Astros.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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 Sense   Edges
EGADS    :      1     Yes     1   1 2 -3 -4
EGADS    :      2     Yes     1   5 6 -7 -1
EGADS    :      3     Yes     1   -2 7 9 -8
EGADS    :      4     Yes     1   -10 -11
EGADS    :      5     Yes     1   -12 3 8 -13
EGADS    :      6     Yes     1   4 12 -14 -5
EGADS    :      7     Yes     1   -6 14 13 -9
EGADS    :      8     Yes     1   15 10 -17 -16
EGADS    :      9     Yes     1   17 11 -15 -18
EGADS    :     10     Yes     1   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    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      9344     18684

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1336      2538         0
AFLR4    : Nodes, Trias,Quads=      1321      2508         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1340      2546         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3812      7470         0
AFLR4    : Nodes, Trias,Quads=      2928      5702         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1337      2540         0
AFLR4    : Nodes, Trias,Quads=      1320      2506         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1338      2542         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1340      2546         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       233       404         0
AFLR4    : Nodes, Trias,Quads=       210       358         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       224       386         0
AFLR4    : Nodes, Trias,Quads=       196       330         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      9465     18926       946

OVERALL  : CPU Time          =     0.137   seconds
Body 1 (of 1)
Number of nodes    = 9465
Number of elements = 18926
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 18926
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9465
Total number of elements = 18926
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 58649
	Number of elements       = 337486
	Number of triangles      = 18926
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 318560
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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 (8.0.0) "


Running SU2......

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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_0.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.
58649 grid points.
318560 volume elements.
3 surface markers.
12526 boundary elements in index 0 (Marker = BC_1).
5702 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
318560 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: 83.4538. Mean K: 0.864574. Standard deviation K: 5.00994.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        54.7348|        86.5097|
|     CV Face Area Aspect Ratio|        1.06172|        21.5651|
|           CV Sub-Volume Ratio|              1|        8.56379|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     58649|    1/1.00|        10|
|         1|      9982|    1/5.88|   8.31273|
|         2|      1772|    1/5.63|   7.00783|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 9.2451 m^2.
Area projection in the x-plane = 0.651846 m^2, y-plane = 0.30478 m^2, z-plane = 4.4157 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.38 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.86329e-18 m, z-direction = -0.0467611 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  9.6714e-01|   -1.350049|    0.930283|    0.592066|    4.119057|   -0.975174|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.5469e-01|   -1.745176|    0.769686|    0.421814|    3.710349|   -0.522367|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.4922e-01|   -1.753732|    0.584287|    0.243601|    3.703267|    1.886644|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.75373|         < -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 = 361
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 3.101438e+09, tgt = 3.101438e+09, diff = 1.877431e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
	Number of variables = 16
	Number of data points = 361
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 3.018930e+09, tgt = 3.018930e+09, diff = 1.945207e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Pressure_SA.csv
	Number of variables = 16
	Number of data points = 361
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 4.374734e+07, tgt = 4.374734e+07, diff = 6.132574e-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

real	0m10.064s
user	0m10.324s
sys	0m0.901s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Pressure_SU2_and_Astros.py passed (as expected)
=================================================


=================================================
+ echo 'aeroelasticSimple_Displacement_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Displacement_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Displacement_SU2_and_Astros.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Running PreAnalysis ...... astros
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 180
	Number of elements = 194
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 32
	Elemental Quad4 = 162
Aero_Reference value is NULL - No aero reference parameters set

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards


Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG

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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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 Sense   Edges
EGADS    :      1     Yes     1   1 2 -3 -4
EGADS    :      2     Yes     1   5 6 -7 -1
EGADS    :      3     Yes     1   -2 7 9 -8
EGADS    :      4     Yes     1   -10 -11
EGADS    :      5     Yes     1   -12 3 8 -13
EGADS    :      6     Yes     1   4 12 -14 -5
EGADS    :      7     Yes     1   -6 14 13 -9
EGADS    :      8     Yes     1   15 10 -17 -16
EGADS    :      9     Yes     1   17 11 -15 -18
EGADS    :     10     Yes     1   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    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      9344     18684

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1336      2538         0
AFLR4    : Nodes, Trias,Quads=      1321      2508         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1340      2546         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3812      7470         0
AFLR4    : Nodes, Trias,Quads=      2928      5702         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1337      2540         0
AFLR4    : Nodes, Trias,Quads=      1320      2506         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1338      2542         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1340      2546         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       233       404         0
AFLR4    : Nodes, Trias,Quads=       210       358         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       224       386         0
AFLR4    : Nodes, Trias,Quads=       196       330         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      9465     18926       946

OVERALL  : CPU Time          =     0.137   seconds
Body 1 (of 1)
Number of nodes    = 9465
Number of elements = 18926
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 18926
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9465
Total number of elements = 18926
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 58649
	Number of elements       = 337486
	Number of triangles      = 18926
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 318560
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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 (8.0.0) "


Running SU2......

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

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_0.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_0.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.
58649 grid points.
318560 volume elements.
3 surface markers.
12526 boundary elements in index 0 (Marker = BC_1).
5702 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
318560 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 9.557862 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_0.su2               |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_0.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.
58649 grid points.
318560 volume elements.
3 surface markers.
12526 boundary elements in index 0 (Marker = BC_1).
5702 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
318560 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 2 TETRAHEDRON volume elements.
There has been a re-orientation of 1 TRIANGLE surface elements.
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: 83.9101. Mean K: 0.904589. Standard deviation K: 4.47748.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        37.6974|        86.4905|
|     CV Face Area Aspect Ratio|          1.068|        23.4392|
|           CV Sub-Volume Ratio|              1|        94.1303|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     58649|    1/1.00|        10|
|         1|      9982|    1/5.88|   8.31273|
|         2|      1772|    1/5.63|   7.00783|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.89892 m.
Wetted area = 11.6364 m^2.
Area projection in the x-plane = 2.8893 m^2, y-plane = 1.28921 m^2, z-plane = 4.27235 m^2.
Max. coordinate in the x-direction = 2.53729 m, y-direction = 3.89892 m, z-direction = 0.526515 m.
Min. coordinate in the x-direction = 0.000170858 m, y-direction = -2.86329e-18 m, z-direction = -0.706552 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  9.6112e-01|   -0.678896|    1.760803|    1.264301|    4.790210|    0.038456|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.5697e-01|   -1.122450|    1.498914|    1.120504|    4.348779|    0.006780|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.5360e-01|   -1.132662|    1.314462|    0.931988|    4.331991|    0.031135|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.13266|         < -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	0m23.991s
user	0m23.285s
sys	0m1.795s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Displacement_SU2_and_Astros.py passed (as expected)
=================================================


=================================================
+ echo 'aeroelasticSimple_Iterative_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Iterative_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Iterative_SU2_and_Astros.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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 Sense   Edges
EGADS    :      1     Yes     1   1 2 -3 -4
EGADS    :      2     Yes     1   5 6 -7 -1
EGADS    :      3     Yes     1   -2 7 9 -8
EGADS    :      4     Yes     1   -10 -11
EGADS    :      5     Yes     1   -12 3 8 -13
EGADS    :      6     Yes     1   4 12 -14 -5
EGADS    :      7     Yes     1   -6 14 13 -9
EGADS    :      8     Yes     1   15 10 -17 -16
EGADS    :      9     Yes     1   17 11 -15 -18
EGADS    :     10     Yes     1   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            = 3.22749
AFLR4    : BL Thickness                = 0
AFLR4    : Abs Min Surf Spacing        = 0.00806872
AFLR4    : Min Surf Spacing            = 0.322749
AFLR4    : Max Surf Spacing            = 2.42061
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=       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=       984      1890         0
AFLR4    : Nodes, Trias,Quads=       852      1626         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=        91       147         0
AFLR4    : Nodes, Trias,Quads=        72       109         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        89       142         0
AFLR4    : Nodes, Trias,Quads=        70       104         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=      2648      5292       492

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      2648      5292

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       385       700         0
AFLR4    : Nodes, Trias,Quads=       379       688         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       382       694         0
AFLR4    : Nodes, Trias,Quads=       381       692         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      1084      2088         0
AFLR4    : Nodes, Trias,Quads=      1012      1944         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       381       692         0
AFLR4    : Nodes, Trias,Quads=       378       686         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       383       696         0
AFLR4    : Nodes, Trias,Quads=       381       692         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       383       696         0
AFLR4    : Nodes, Trias,Quads=       379       688         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=        99       160         0
AFLR4    : Nodes, Trias,Quads=        81       124         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        96       154         0
AFLR4    : Nodes, Trias,Quads=        77       116         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        11        12         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      2820      5636       500

OVERALL  : CPU Time          =     0.061   seconds
Body 1 (of 1)
Number of nodes    = 2820
Number of elements = 5636
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 5636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2820
Total number of elements = 5636
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 11908
	Number of elements       = 67561
	Number of triangles      = 5636
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 61925
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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 (8.0.0) "


Running SU2......

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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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: 50.9602. Mean K: 0.841392. Standard deviation K: 3.91829.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        54.7347|        85.0322|
|     CV Face Area Aspect Ratio|        1.16344|        19.2647|
|           CV Sub-Volume Ratio|              1|        11.2523|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11908|    1/1.00|        10|
|         1|      2108|    1/5.65|   8.42239|
|         2|       441|    1/4.78|   7.49979|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 8.34825 m^2.
Area projection in the x-plane = 0.587638 m^2, y-plane = 0.276904 m^2, z-plane = 3.94911 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380417 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.85958e-18 m, z-direction = -0.0467006 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.7744e-01|   -0.835779|    1.475337|    1.164402|    4.633327|   -1.069323|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.7510e-01|   -1.169523|    1.337951|    0.991972|    4.282357|   -0.707163|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.7631e-01|   -1.219552|    1.197742|    0.832257|    4.232440|    0.340563|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.21955|         < -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 = 130
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 3.094239e+09, tgt = 3.094239e+09, diff = 1.697796e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 3.011585e+09, tgt = 3.011585e+09, diff = 1.847555e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 4.097986e+07, tgt = 4.097986e+07, diff = 3.341614e-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
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 (8.0.0) "


Running SU2......

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

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_0.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 0.670391 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_0.su2               |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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 1103 TETRAHEDRON volume elements.
There has been a re-orientation of 64 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 64440.8.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 25.9358. Mean K: 0.573224. Standard deviation K: 1.86381.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.568085|        85.2217|
|     CV Face Area Aspect Ratio|        1.23147|        204.176|
|           CV Sub-Volume Ratio|              1|         197161|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11908|    1/1.00|        10|
|         1|      2088|     1/5.7|   8.39567|
|         2|       424|    1/4.92|   7.40216|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 5.04689 m.
Wetted area = 174.995 m^2.
Area projection in the x-plane = 66.7106 m^2, y-plane = 38.0858 m^2, z-plane = 6.30894 m^2.
Max. coordinate in the x-direction = 2.8362 m, y-direction = 5.04689 m, z-direction = 7.00377 m.
Min. coordinate in the x-direction = -0.81093 m, y-direction = -0.0123551 m, z-direction = -19.8631 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.8663e-01|    1.720014|    4.670347|    4.852889|    7.189119|    0.036087|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.8970e-01|    2.050374|    4.610643|    4.787622|    7.486479|   -0.011983|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.9072e-01|    2.230285|    4.776975|    4.799901|    7.661578|   -0.064284|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       2.23028|         < -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 28 non-physical points in the solution.
Warning: 9 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 = 130
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.528910e+09, tgt = 1.528911e+09, diff = 3.948348e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 1.417409e+09, tgt = 1.417409e+09, diff = 1.691035e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 2.450056e+07, tgt = 2.450056e+07, diff = 2.537084e-01
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 16 (total = 178)

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
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 (8.0.0) "


Running SU2......

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

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_0.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 1103 TETRAHEDRON volume elements.
There has been a re-orientation of 64 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 64440.8.
  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 1.617004 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_0.su2               |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


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

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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 32493 TETRAHEDRON volume elements.
There has been a re-orientation of 1656 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 768397.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 68.4801. Mean K: 1.48855. Standard deviation K: 5.3251.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.789304|        81.2248|
|     CV Face Area Aspect Ratio|        1.70696|        1443.72|
|           CV Sub-Volume Ratio|              1|        68046.3|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11908|    1/1.00|        10|
|         1|      2098|    1/5.68|   8.40905|
|         2|       430|    1/4.88|   7.43691|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 22.756 m.
Wetted area = 1816.34 m^2.
Area projection in the x-plane = 945.548 m^2, y-plane = 256.811 m^2, z-plane = 29.1949 m^2.
Max. coordinate in the x-direction = 2.09844 m, y-direction = 22.756 m, z-direction = 0.155398 m.
Min. coordinate in the x-direction = -3.70658 m, y-direction = -2.85958e-18 m, z-direction = -238.685 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.8278e-01|    3.643452|    6.607905|    6.649404|    9.112558|   -0.075438|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.8899e-01|    3.973473|    6.567229|    6.628976|    9.388960|   -0.091461|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.9048e-01|    4.045356|    6.641283|    6.646420|    9.458361|   -0.084590|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       4.04536|         < -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 303 non-physical points in the solution.
Warning: 6 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 = 130
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 2.115109e+09, tgt = 2.115108e+09, diff = 6.871555e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 2.093310e+09, tgt = 2.093310e+09, diff = 2.820739e+01
Reading SU2 AeroLoad File - surface_flow_aeroelasticSimple_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 1.865993e+07, tgt = 1.865993e+07, diff = 1.753187e-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
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 (8.0.0) "


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Mesh Deformation Code)                     |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_0.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 32493 TETRAHEDRON volume elements.
There has been a re-orientation of 1656 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 768397.
  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 24.951728 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_0.su2               |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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 19828 TETRAHEDRON volume elements.
There has been a re-orientation of 2837 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 7.14074e+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: 72.7515. Mean K: 0.679573. Standard deviation K: 2.34024.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.909038|        82.6277|
|     CV Face Area Aspect Ratio|         1.1202|         6742.5|
|           CV Sub-Volume Ratio|              1|    8.12104e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11908|    1/1.00|        10|
|         1|      2108|    1/5.65|   8.42239|
|         2|       421|    1/5.01|   7.38466|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 32.1598 m.
Wetted area = 5665.54 m^2.
Area projection in the x-plane = 3299.69 m^2, y-plane = 704.462 m^2, z-plane = 28.5975 m^2.
Max. coordinate in the x-direction = 9.70414 m, y-direction = 32.1598 m, z-direction = 1.54253 m.
Min. coordinate in the x-direction = -0.0131842 m, y-direction = -0.141473 m, z-direction = -418.415 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.8151e-01|    5.498950|    8.465771|    8.452556|   10.968056|   -0.037521|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.8794e-01|    6.017813|    8.605945|    8.542315|   11.446029|   -0.078958|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.8978e-01|    6.205320|    8.836920|    8.594849|   11.634731|   -0.063121|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       6.20532|         < -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 521 non-physical points in the solution.
Warning: 59 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 =  309.986638
Cd =  -4910.998774

real	0m38.740s
user	0m37.907s
sys	0m1.773s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Iterative_SU2_and_Astros.py passed (as expected)
=================================================


=================================================
+ echo 'aeroelastic_Iterative_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelastic_Iterative_SU2_and_Astros.py test;
+ python -u aeroelastic_Iterative_SU2_and_Astros.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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 Sense   Edges
EGADS    :      1     Yes     1   1 2 -3 -4
EGADS    :      2     Yes     1   5 6 -7 -1
EGADS    :      3     Yes     1   -2 7 9 -8
EGADS    :      4     Yes     1   -10 -11
EGADS    :      5     Yes     1   -12 3 8 -13
EGADS    :      6     Yes     1   4 12 -14 -5
EGADS    :      7     Yes     1   -6 14 13 -9
EGADS    :      8     Yes     1   15 10 -17 -16
EGADS    :      9     Yes     1   17 11 -15 -18
EGADS    :     10     Yes     1   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            = 3.22749
AFLR4    : BL Thickness                = 0
AFLR4    : Abs Min Surf Spacing        = 0.00806872
AFLR4    : Min Surf Spacing            = 0.322749
AFLR4    : Max Surf Spacing            = 2.42061
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=       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=       984      1890         0
AFLR4    : Nodes, Trias,Quads=       852      1626         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=        91       147         0
AFLR4    : Nodes, Trias,Quads=        72       109         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        89       142         0
AFLR4    : Nodes, Trias,Quads=        70       104         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=      2648      5292       492

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      2648      5292

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       385       700         0
AFLR4    : Nodes, Trias,Quads=       379       688         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       382       694         0
AFLR4    : Nodes, Trias,Quads=       381       692         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      1084      2088         0
AFLR4    : Nodes, Trias,Quads=      1012      1944         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       381       692         0
AFLR4    : Nodes, Trias,Quads=       378       686         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       383       696         0
AFLR4    : Nodes, Trias,Quads=       381       692         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       383       696         0
AFLR4    : Nodes, Trias,Quads=       379       688         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=        99       160         0
AFLR4    : Nodes, Trias,Quads=        81       124         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        96       154         0
AFLR4    : Nodes, Trias,Quads=        77       116         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        11        12         0
AFLR4    : Nodes, Trias,Quads=         8         6         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      2820      5636       500

OVERALL  : CPU Time          =     0.062   seconds
Body 1 (of 1)
Number of nodes    = 2820
Number of elements = 5636
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 5636
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2820
Total number of elements = 5636
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 11908
	Number of elements       = 67561
	Number of triangles      = 5636
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 61925
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

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 (8.0.0) "


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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: 50.9602. Mean K: 0.841392. Standard deviation K: 3.91829.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        54.7347|        85.0322|
|     CV Face Area Aspect Ratio|        1.16344|        19.2647|
|           CV Sub-Volume Ratio|              1|        11.2523|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11908|    1/1.00|        10|
|         1|      2108|    1/5.65|   8.42239|
|         2|       441|    1/4.78|   7.49979|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 8.34825 m^2.
Area projection in the x-plane = 0.587638 m^2, y-plane = 0.276904 m^2, z-plane = 3.94911 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.380417 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.85958e-18 m, z-direction = -0.0467006 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.7714e-01|   -0.835779|    1.475337|    1.164402|    4.633327|   -1.069323|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.7482e-01|   -1.169523|    1.337951|    0.991972|    4.282357|   -0.707163|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.7617e-01|   -1.219552|    1.197742|    0.832257|    4.232440|    0.340563|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.21955|         < -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 = 130
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 3.094239e+09, tgt = 3.094240e+09, diff = 9.801585e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 3.011585e+09, tgt = 3.011585e+09, diff = 6.390332e+01
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 4.097986e+07, tgt = 4.097985e+07, diff = 3.286700e+00
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
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 (8.0.0) "


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Mesh Deformation Code)                     |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_0.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 0.682053 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_0.su2               |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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 25539 TETRAHEDRON volume elements.
There has been a re-orientation of 1443 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 433151.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 174.848. Mean K: 1.81464. Standard deviation K: 9.67786.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        1.02474|        82.8568|
|     CV Face Area Aspect Ratio|        1.27915|        746.178|
|           CV Sub-Volume Ratio|              1|        27636.8|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11908|    1/1.00|        10|
|         1|      2100|    1/5.67|   8.41172|
|         2|       419|    1/5.01|   7.37294|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 24.2419 m.
Wetted area = 3029.92 m^2.
Area projection in the x-plane = 535.45 m^2, y-plane = 986.125 m^2, z-plane = 108.557 m^2.
Max. coordinate in the x-direction = 4.83758 m, y-direction = 24.2419 m, z-direction = 26.8693 m.
Min. coordinate in the x-direction = -13.0716 m, y-direction = -0.915654 m, z-direction = -247.285 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.8046e-01|    3.556322|    6.521883|    6.735668|    9.025428|   -0.363276|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.8744e-01|    3.775224|    6.384952|    6.551528|    9.224250|   -0.392841|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.8948e-01|    4.025558|    6.414910|    6.646520|    9.411271|   -0.249156|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       4.02556|         < -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 186 non-physical points in the solution.
Warning: 6 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 = 130
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.410187e+09, tgt = 1.410186e+09, diff = 3.602318e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 8.591697e+08, tgt = 8.591703e+08, diff = 5.944963e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 8.125293e+06, tgt = 8.125314e+06, diff = 2.059804e+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
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 (8.0.0) "


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Mesh Deformation Code)                     |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_0.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 25539 TETRAHEDRON volume elements.
There has been a re-orientation of 1443 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 433151.
  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 24.909629 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_0.su2               |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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 38328 TETRAHEDRON volume elements.
There has been a re-orientation of 1598 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 7.42434e+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: 12.2371. Mean K: 0.221668. Standard deviation K: 0.773141.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.285943|        81.3626|
|     CV Face Area Aspect Ratio|        1.45886|         417020|
|           CV Sub-Volume Ratio|              1|    3.17763e+07|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11908|    1/1.00|        10|
|         1|      2110|    1/5.64|   8.42505|
|         2|       433|    1/4.87|   7.45416|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 19.7694 m.
Wetted area = 1.74808e+06 m^2.
Area projection in the x-plane = 338696 m^2, y-plane = 594656 m^2, z-plane = 40453.6 m^2.
Max. coordinate in the x-direction = 62.4212 m, y-direction = 19.7694 m, z-direction = 8016.54 m.
Min. coordinate in the x-direction = -42.5817 m, y-direction = -590.328 m, z-direction = -0.229846 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.8784e-01|    7.454779|   10.421451|   10.456663|   12.923885|   -0.033773|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.9146e-01|    8.012761|   10.668752|   10.464329|   13.576159|   -0.033620|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.9243e-01|    8.111493|   10.617099|   10.585648|   13.504448|   -0.033451|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       8.11149|         < -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 502 non-physical points in the solution.
Warning: 50 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 = 130
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.517138e+09, tgt = 1.517138e+09, diff = 4.692427e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Pressure'
            Rank 0: src = 1.539054e+09, tgt = 1.539053e+09, diff = 2.540065e+02
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Pressure'
            Rank 0: src = 2.579027e+07, tgt = 2.579021e+07, diff = 5.582233e+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
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 (8.0.0) "


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Mesh Deformation Code)                     |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_0.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 38328 TETRAHEDRON volume elements.
There has been a re-orientation of 1598 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 7.42434e+11.
  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 24.905462 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_0.su2               |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_0.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.
11908 grid points.
61925 volume elements.
3 surface markers.
3446 boundary elements in index 0 (Marker = BC_1).
1944 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
61925 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 33081 TETRAHEDRON volume elements.
There has been a re-orientation of 2988 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 5.8158e+15.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 11.3037. Mean K: 0.182876. Standard deviation K: 0.782659.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.766697|         82.092|
|     CV Face Area Aspect Ratio|        1.79727|     8.3847e+08|
|           CV Sub-Volume Ratio|              1|    3.69912e+09|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11908|    1/1.00|        10|
|         1|      2100|    1/5.67|   8.41172|
|         2|       424|    1/4.95|   7.40216|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 404.148 m.
Wetted area = 1.0396e+06 m^2.
Area projection in the x-plane = 153335 m^2, y-plane = 367670 m^2, z-plane = 16927.4 m^2.
Max. coordinate in the x-direction = 70.0988 m, y-direction = 404.148 m, z-direction = 4.72929 m.
Min. coordinate in the x-direction = -16.5462 m, y-direction = -10.1271 m, z-direction = -5698.95 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.8060e-01|   10.044140|   13.010996|   13.056978|   15.513246|   -0.018041|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.8753e-01|   10.667977|   13.092077|   13.232395|   16.099153|   -0.020224|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.8944e-01|   10.680255|   13.183304|   13.214584|   16.066809|   -0.020200|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       10.6803|         < -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 491 non-physical points in the solution.
Warning: 36 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	1m22.754s
user	1m26.696s
sys	0m8.176s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aeroelastic_Iterative_SU2_and_Astros.py passed (as expected)
=================================================


=================================================
+ echo 'aeroelasticSimple_Temperature_SU2_and_TACS.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Temperature_SU2_and_TACS.py test;
+ python -u aeroelasticSimple_Temperature_SU2_and_TACS.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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 Sense   Edges
EGADS    :      1     Yes     1   1 2 -3 -4
EGADS    :      2     Yes     1   5 6 -7 -1
EGADS    :      3     Yes     1   -2 7 9 -8
EGADS    :      4     Yes     1   -10 -11
EGADS    :      5     Yes     1   -12 3 8 -13
EGADS    :      6     Yes     1   4 12 -14 -5
EGADS    :      7     Yes     1   -6 14 13 -9
EGADS    :      8     Yes     1   15 10 -17 -16
EGADS    :      9     Yes     1   17 11 -15 -18
EGADS    :     10     Yes     1   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    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      9344     18684

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1336      2538         0
AFLR4    : Nodes, Trias,Quads=      1321      2508         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1340      2546         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3812      7470         0
AFLR4    : Nodes, Trias,Quads=      2928      5702         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1337      2540         0
AFLR4    : Nodes, Trias,Quads=      1320      2506         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1338      2542         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1340      2546         0
AFLR4    : Nodes, Trias,Quads=      1319      2504         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       233       404         0
AFLR4    : Nodes, Trias,Quads=       210       358         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=       224       386         0
AFLR4    : Nodes, Trias,Quads=       196       330         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=        18        22         0
AFLR4    : Nodes, Trias,Quads=        12        10         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      9465     18926       946

OVERALL  : CPU Time          =     0.137   seconds
Body 1 (of 1)
Number of nodes    = 9465
Number of elements = 18926
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 18926
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9465
Total number of elements = 18926
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 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.6.0 arm64
AFLR2    : Compile Date   08/01/23 @ 11:39PM
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 11.5.9
AFLR4    : Version Date   08/14/23 @ 12:27AM
AFLR4    : Compile OS     Darwin 22.6.0 arm64
AFLR4    : Compile Date   08/14/23 @ 12:31AM
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          = 58649
	Number of elements       = 337486
	Number of triangles      = 18926
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 318560
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Skin
	Boundary condition name - SymmPlane
	Done getting CFD boundary conditions
Info: No recognized data transfer names found.
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_3.

Surface(s) plotted in the output file: BC_3.
Surface(s) affected by the design variables: BC_3.
Input mesh file name: ../aflr3/aflr3_0.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.
58649 grid points.
318560 volume elements.
3 surface markers.
12526 boundary elements in index 0 (Marker = BC_1).
5702 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
318560 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: 83.4538. Mean K: 0.864574. Standard deviation K: 5.00994.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        54.7348|        86.5097|
|     CV Face Area Aspect Ratio|        1.06172|        21.5651|
|           CV Sub-Volume Ratio|              1|        8.56379|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     58649|    1/1.00|        10|
|         1|      9982|    1/5.88|   8.31273|
|         2|      1772|    1/5.63|   7.00783|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 9.2451 m^2.
Area projection in the x-plane = 0.651846 m^2, y-plane = 0.30478 m^2, z-plane = 4.4157 m^2.
Max. coordinate in the x-direction = 2.53651 m, y-direction = 3.87298 m, z-direction = 0.38 m.
Min. coordinate in the x-direction = 0 m, y-direction = -2.86329e-18 m, z-direction = -0.0467611 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  9.6054e-01|   -1.350049|    0.930283|    0.592066|    4.119057|   -0.975174|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  9.5430e-01|   -1.745176|    0.769686|    0.421814|    3.710349|   -0.522367|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  9.4923e-01|   -1.753732|    0.584287|    0.243601|    3.703267|    1.886644|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.75373|         < -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 node elements          = 0
Number of line elements          = 0
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 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 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 = 361
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Temperature'
            Rank 0: src = 1.497300e+03, tgt = 1.497300e+03, diff = 1.045589e-05
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA 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 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 = 361
 CAPS Info: Bound 'Skin_Bottom' Normalized Integrated 'Temperature'
            Rank 0: src = 1.453584e+03, tgt = 1.453584e+03, diff = 9.270707e-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 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 = 361
 CAPS Info: Bound 'Skin_Tip' Normalized Integrated 'Temperature'
            Rank 0: src = 2.098482e+01, tgt = 2.098482e+01, diff = 5.684342e-14
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	0m10.663s
user	0m10.905s
sys	0m0.861s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Temperature_SU2_and_TACS.py passed (as expected)
=================================================

Running.... CORSAIRLITE PyTests


=================================================
+ echo 'gp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
gp.py test;
+ python -u gp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   0.00713 dimensionless

Variables
---------
   x  :   3.00000   [-]   The X variable
   y  :  81.00008   [-]   The Y variable
   z  :   0.19245   [-]   The Z variable

Sensitivities
-------------
   No Constants in the Formulation

Solve Report
------------
   Solve Method           :  Geometric Program 
   Classification         :  Convex 
   Solver                 :  cvxopt 


real	0m1.858s
user	0m1.122s
sys	0m0.108s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case gp.py passed (as expected)
=================================================


=================================================
+ echo 'qp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
qp.py test;
+ python -u qp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   -21.56250 dimensionless

Variables
---------
   x  :  1.62500   [-]   The X variable
   y  :  1.37500   [-]   The Y variable

Constants
---------
   c   :  3         [-]   A constant
   c2  :  2         [-]   A constant

Sensitivities
-------------
   c   :  + 0.46957   A constant
   c2  :  - 0.22338   A constant

Solve Report
------------
   Solve Method           :  Quadratic Program 
   Classification         :  Convex 
   Solver                 :  cvxopt 


real	0m0.697s
user	0m0.978s
sys	0m0.051s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case qp.py passed (as expected)
=================================================


=================================================
+ echo 'sp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
sp.py test;
+ python -u sp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   0.45721 dimensionless

Variables
---------
   x  :  2.56155   [-]   The X variable
   y  :  6.56155   [-]   The Y variable
   z  :  1.17116   [-]   The Z variable

Constants
---------
   c  :  2         [-]   A constant

Sensitivities
-------------
   Sensitivities not computed

Solve Report
------------
   Solve Method           :  Signomial Program--Standard 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  3 
   Termination Status     :  Converged, relative error (3.15e-04) is less than specified tolerance (1.00e-03) 


real	0m0.684s
user	0m0.964s
sys	0m0.052s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case sp.py passed (as expected)
=================================================


=================================================
+ echo 'boydBox.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
boydBox.py test;
+ python -u boydBox.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   0.00520 1 / meter ** 3

Variables
---------
   d  :  11.26658   meter   The Z variable
   h  :   2.92246   meter   The Y variable
   w  :   5.84486   meter   The X variable

Constants
---------
   Aflr   :  1000         meter ** 2   Area of floor          
   Awall  :   100         meter ** 2   Area of wall           
   alpha  :     0.50000      [-]       Aspect Ratio Constraint
   beta   :     2            [-]       Aspect Ratio Constraint
   delta  :     2            [-]       Aspect Ratio Constraint
   gamma  :     0.50000      [-]       Aspect Ratio Constraint

Sensitivities
-------------
   Sensitivities not computed

Solve Report
------------
   Solve Method           :  Geometric Program 
   Classification         :  Convex 
   Solver                 :  cvxopt 


real	0m0.594s
user	0m0.877s
sys	0m0.050s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case boydBox.py passed (as expected)
=================================================


=================================================
+ echo 'hoburg_gp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hoburg_gp.py test;
+ python -u hoburg_gp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   5905.58568 newton

Variables
---------
   AR          :       20.36983        [-]         aspect ratio                                                            
   C_D_0       :        0.01271        [-]         Drag Coefficient, segment 0                                             
   C_D_1       :        0.01273        [-]         Drag Coefficient, segment 1                                             
   C_D_2       :        0.00778        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0   :        0.00180        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1   :        0.00180        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2   :        0.00180        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0      :        0.00542        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1      :        0.00542        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2      :        0.00023        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0      :        0.00549        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1      :        0.00551        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2      :        0.00575        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0       :        0.57420        [-]         Lift Coefficient, segment 0                                             
   C_L_1       :        0.57421        [-]         Lift Coefficient, segment 1                                             
   C_L_2       :        0.11881        [-]         Lift Coefficient, segment 2                                             
   I_cap_bar   :        0.00002        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar     :    36139.20785       newton       Root Bending unit per unit chord                                        
   P_max       :  1185884.98442        watt        Maximum Engine Power                                                    
   R           :     4999.98983     kilometer      Single Segment range                                                    
   Re_0        :  4232645.50367        [-]         Reynolds Number, segment 0                                              
   Re_1        :  4051247.93913        [-]         Reynolds Number, segment 1                                              
   Re_2        :  9305153.26607        [-]         Reynolds Number, segment 2                                              
   S           :       27.73109     meter ** 2     total wing area                                                         
   T_0         :      746.21338       newton       Thrust, segment 0                                                       
   T_1         :      684.51827       newton       Thrust, segment 1                                                       
   T_2         :     2208.51611       newton       Thrust, segment 2                                                       
   V_0         :       68.23357   meter / second   Velocity, segment 0                                                     
   V_1         :       65.30930   meter / second   Velocity, segment 1                                                     
   V_2         :      150.00638   meter / second   Velocity, segment 2                                                     
   V_stall     :       37.99896   meter / second   stall speed                                                             
   W_0         :    33698.97702       newton       Weight, segment 0                                                       
   W_1         :    30873.13301       newton       Weight, segment 1                                                       
   W_2         :    33698.96566       newton       Weight, segment 2                                                       
   W_MTO       :    36788.13387       newton       Maximum Takeoff Weight                                                  
   W_cap       :     4091.65066       newton       Weight of Wing Spar Cap                                                 
   W_eng       :     2806.10727       newton       Engine Weight                                                           
   W_fuel_out  :     3079.86524       newton       Weight of fuel, outbound                                                
   W_fuel_ret  :     2825.71897       newton       Weight of fuel, return                                                  
   W_pay       :     4905.15902       newton       Payload Weight                                                          
   W_tilde     :    22409.98513       newton       Dry Weight, no wing                                                     
   W_web       :      139.91823       newton       Weight of Wing Spar Shear Web                                           
   W_wing      :     8462.91404       newton       wing weight                                                             
   W_zfw       :    30872.92436       newton       Zero Fuel Weight                                                        
   eta_0_0     :        0.26999        [-]         Overall Efficiency, segment 0                                           
   eta_0_1     :        0.26996        [-]         Overall Efficiency, segment 1                                           
   eta_0_2     :        0.27945        [-]         Overall Efficiency, segment 2                                           
   eta_i_0     :        0.90752        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1     :        0.90742        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2     :        0.93932        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0  :        0.77139        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1  :        0.77131        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2  :        0.79842        [-]         Propeller Efficiency, segment 2                                         
   nu          :        0.78603        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p           :        1.90003        [-]         Dummy Variable (1+2*lam_w)                                              
   q           :        1.45002        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar   :        0.00456        [-]         Spar cap thickness per unit chord                                       
   t_web_bar   :        0.00069        [-]         Spar web thickness per unit chord                                       
   tau         :        0.15000        [-]         airfoil thickness to chord ratio                                        
   z_bre_0     :        0.08745        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1     :        0.08758        [-]         Breguet Range Factor, segment 1                                         

Constants
---------
   A_prop           :         0.78500           meter ** 2          Disk area of propeller                             
   CDA0             :         0.05000           meter ** 2          fuselage drag area                                 
   C_Lmax           :         1.50000              [-]              max CL with flaps down                             
   N_lift           :         6                    [-]              Ultimate Load Factor                               
   W_fixed          :     14700                   newton            fixed weight                                       
   e                :         0.95000              [-]              Oswald efficiency factor                           
   eta_eng          :         0.35000              [-]              Engine Efficiency                                  
   eta_v            :         0.85000              [-]              Propeller Viscous Efficiency                       
   f_wadd           :         2                    [-]              Added Weight Fraction                              
   g                :         9.81000      meter / second ** 2      Gravitational constant                             
   h_fuel           :  46000000              joule / kilogram       Fuel Specific energy density                       
   k_ew             :         0.03720     newton / watt ** 0.803    Constant for engine weight                         
   mu               :         0.00002   kilogram / meter / second   viscosity of air                                   
   r_h              :         0.75000              [-]              Ratio of height at rear spar to maximum wing height
   rho              :         0.90912     kilogram / meter ** 3     density of air                                     
   rho_SL           :         1.22500     kilogram / meter ** 3     density of air, sea level                          
   rho_cap          :      2700           kilogram / meter ** 3     Density of wing cap material (aluminum)            
   rho_web          :      2700           kilogram / meter ** 3     Density of wing web material (aluminum)            
   sigma_max        :       310                 megapascal          Allowable tensile stress of aluminum               
   sigma_max_shear  :       167                 megapascal          Allowable shear stress of aluminum                 
   w_bar            :         0.50000              [-]              Ratio of spar box width to chord length            

Sensitivities
-------------
   Sensitivities not computed

Solve Report
------------
   Solve Method           :  Geometric Program 
   Classification         :  Convex 
   Solver                 :  cvxopt 


real	0m4.684s
user	0m4.949s
sys	0m0.053s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case hoburg_gp.py passed (as expected)
=================================================


=================================================
+ echo 'hoburg_blackbox.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hoburg_blackbox.py test;
+ python -u hoburg_blackbox.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   5905.2294 newton

Variables
---------
   AR          :       20.3737        [-]         aspect ratio                                                            
   C_D_0       :        0.0127        [-]         Drag Coefficient, segment 0                                             
   C_D_1       :        0.0127        [-]         Drag Coefficient, segment 1                                             
   C_D_2       :        0.0078        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0   :        0.0018        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1   :        0.0018        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2   :        0.0018        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0      :        0.0054        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1      :        0.0054        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2      :        0.0002        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0      :        0.0055        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1      :        0.0055        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2      :        0.0057        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0       :        0.5743        [-]         Lift Coefficient, segment 0                                             
   C_L_1       :        0.5743        [-]         Lift Coefficient, segment 1                                             
   C_L_2       :        0.1189        [-]         Lift Coefficient, segment 2                                             
   I_cap_bar   :        0.0000        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar     :    36141.5015       newton       Root Bending unit per unit chord                                        
   P_max       :  1184357.7686        watt        Maximum Engine Power                                                    
   R           :     5000.0000     kilometer      Single Segment range                                                    
   Re_0        :  4231748.4657        [-]         Reynolds Number, segment 0                                              
   Re_1        :  4050340.4368        [-]         Reynolds Number, segment 1                                              
   Re_2        :  9301869.2068        [-]         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 (9.636631e-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	0m18.819s
user	0m19.041s
sys	0m0.083s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case hoburg_blackbox.py passed (as expected)
=================================================


=================================================
+ echo 'pyCAPS/sizeWing.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/sizeWing.py test;
+ python -u pyCAPS/sizeWing.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nrock 2

Objective
---------
   0.075 dimensionless

Variables
---------
   AR     :  10.000        [-]         Wing aspect ratio
   CD     :   0.075        [-]         Drag Coefficient 
   CL     :   0.999        [-]         Lift Coefficient 
   S      :   2.642     meter ** 2     Wing area        
   V      :   2.722   meter / second   Airspeed         
   W      :  11.979       newton       Aircraft weight  
   Wwing  :   1.598       newton       Wing weight      

Constants
---------
   ARmax     :  10                [-]            Max AR                                         
   CD0       :   0.040            [-]            Profile drag                                   
   CLmax     :   1                [-]            Max CL                                         
   E0        :  10               joule           Maximum elastic potential energy in rubber band
   Wfixed    :   0.100           newton          Weight of fixed components                     
   Wrock     :   2               newton          Weight of each rock                            
   e         :   0.900            [-]            Oswawld efficiency factor                      
   g         :   9.810    meter / second ** 2    Gravitational constant                         
   nrock     :   2                [-]            Number of rocks to carry                       
   rho       :   1.225   kilogram / meter ** 3   Density of air                                 
   rho_wing  :   1       kilogram / meter ** 3   Weight density of wing                         
   tau       :   0.120            [-]            Airfoil thickness as t/c                       

Sensitivities
-------------
   Sensitivities not computed

Solve Report
------------
   Solve Method           :  Geometric Program 
   Classification         :  Convex 
   Solver                 :  cvxopt 

Optimized L/D: 13.267784561972137
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!

real	0m0.851s
user	0m1.111s
sys	0m0.077s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/sizeWing.py passed (as expected)
=================================================

avl: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/avl

=================================================
+ echo 'pyCAPS/optTaperAvl.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/optTaperAvl.py test;
+ python -u pyCAPS/optTaperAvl.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)

Objective
---------
   1.00805 dimensionless

Variables
---------
   e    :  0.99202   [-]   Oswald efficiency factor
   lam  :  0.39881   [-]   Wing taper ratio        

Sensitivities
-------------
   Sensitivities not available for optimizations of type Sequential Log Convex Program 

Solve Report
------------
   Solve Method           :  Sequential Log Convex Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  6 
   Termination Status     :  Converged, gradient of Lagrangian (5.888774e-08) within tolerance (1.000000e-06)  

Messages
--------
   1. Wolfe Condition 1 failed at iteration 5 (Step 5).  Watchdog counter is 1


real	0m3.066s
user	0m2.303s
sys	0m1.040s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/optTaperAvl.py passed (as expected)
=================================================


=================================================
+ echo 'pyCAPS/optWingAvl.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/optWingAvl.py test;
+ python -u pyCAPS/optWingAvl.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nrock 2
Starting iteration 0 at 0.1678 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: 0.990550414371373 dimensionless
dydx: [<Quantity(0.060834734963571835, 'dimensionless')>, <Quantity(-0.0014769756679916535, 'dimensionless')>]
Calling cvxopt.solvers.cp at 0.7110 seconds
Got sol from cvxopt at 0.7199 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 8.743959706200045e-09
relative gap 7.1941976174589016e-09
primal objective -1.2154183372694929
dual objective -1.2154183416834794
primal slack 1.3843122277340912e-11
dual slack 8.310943825855639e-12
primal infeasibility 1.13903462789848e-09
dual infeasibility 2.3823418495103618e-11
AVL run case - lam, AR: 0.3017253411787602 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: 0.9892210301573232 dimensionless
dydx: [<Quantity(0.06359341837018917, 'dimensionless')>, <Quantity(-0.0014812479862164052, 'dimensionless')>]
logspace stuff at 1.2602 seconds
Starting iteration 1 at 1.2751 seconds
AR : 9.999999995701312 dimensionless
CD : 0.07217671497330859 dimensionless
CL : 0.9999999999851361 dimensionless
S : 0.6639217992634345 meter ** 2
V : 3.600068783658014 meter / second
W : 5.270412635736404 newton
Wwing : 0.20138431695627712 newton
e : 0.9892553874046033 dimensionless
lam : 0.3017253411787602 dimensionless
Calling cvxopt.solvers.cp at 1.2790 seconds
Got sol from cvxopt at 1.2857 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 2.1363031593454878e-08
relative gap 8.126967446080017e-09
primal objective -2.628659673511942
dual objective -2.628659684337833
primal slack 2.0577846480825846e-11
dual slack 2.53050406780468e-11
primal infeasibility 3.085803284597273e-09
dual infeasibility 3.13391320011975e-09
AVL run case - lam, AR: 0.30434464835769004 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: 0.9893844569300133 dimensionless
dydx: [<Quantity(0.061358790088644755, 'dimensionless')>, <Quantity(-0.001469791715157931, 'dimensionless')>]
logspace stuff at 1.8259 seconds
Starting iteration 2 at 1.8432 seconds
AR : 9.99999999959832 dimensionless
CD : 0.07217242517886707 dimensionless
CL : 0.9999998041107226 dimensionless
S : 0.6639218068635588 meter ** 2
V : 3.6000690493939635 meter / second
W : 5.270412441791246 newton
Wwing : 0.20138432037500312 newton
e : 0.9893868959019062 dimensionless
lam : 0.30434464835769004 dimensionless
Calling cvxopt.solvers.cp at 1.8469 seconds
Got sol from cvxopt at 1.8537 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 2.097954193386208e-08
relative gap 7.980432613224019e-09
primal objective -2.628872763000068
dual objective -2.628872773631917
primal slack 2.0226195523752228e-11
dual slack 2.4870270238975127e-11
primal infeasibility 3.030673275151341e-09
dual infeasibility 3.0769326689078285e-09
AVL run case - lam, AR: 0.3174093513141515 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: 0.9901147289476044 dimensionless
dydx: [<Quantity(0.05073085616785211, 'dimensionless')>, <Quantity(-0.001419190987608232, 'dimensionless')>]
logspace stuff at 2.3955 seconds
Starting iteration 3 at 2.4129 seconds
AR : 9.999999999606068 dimensionless
CD : 0.07214699157334123 dimensionless
CL : 0.9999998084033913 dimensionless
S : 0.6639218067235316 meter ** 2
V : 3.6000690442960233 meter / second
W : 5.270412448377285 newton
Wwing : 0.20138432031121437 newton
e : 0.9901696737885595 dimensionless
lam : 0.3174093513141515 dimensionless
Calling cvxopt.solvers.cp at 2.4168 seconds
Got sol from cvxopt at 2.4235 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 1.9913348949433526e-08
relative gap 7.57253767423933e-09
primal objective -2.629679746219796
dual objective -2.629679756312171
primal slack 1.9233234440857094e-11
dual slack 2.3654666051747643e-11
primal infeasibility 2.8765759057609882e-09
dual infeasibility 2.9202707353765115e-09
AVL run case - lam, AR: 0.38029905717662316 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: 0.9919295458295864 dimensionless
dydx: [<Quantity(0.009583432732646058, 'dimensionless')>, <Quantity(-0.0013533445524760435, 'dimensionless')>]
logspace stuff at 2.9628 seconds
Starting iteration 4 at 2.9804 seconds
AR : 9.999999999627487 dimensionless
CD : 0.0720544031114864 dimensionless
CL : 0.9999998201037487 dimensionless
S : 0.6639218063847038 meter ** 2
V : 3.600069031643119 meter / second
W : 5.270412470306208 newton
Wwing : 0.20138432015683602 newton
e : 0.993029781490428 dimensionless
lam : 0.38029905717662316 dimensionless
Calling cvxopt.solvers.cp at 2.9843 seconds
Got sol from cvxopt at 2.9910 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 2.0688403479344937e-08
relative gap 7.866667127626345e-09
primal objective -2.629881644119772
dual objective -2.629881654604473
primal slack 1.9944303018503003e-11
dual slack 2.4539201182220112e-11
primal infeasibility 2.9853825022328838e-09
dual infeasibility 3.036428971722002e-09
AVL run case - lam, AR: 0.4005573159778744 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: 0.9920150584836487 dimensionless
dydx: [<Quantity(-0.0008541793310445911, 'dimensionless')>, <Quantity(-0.0013850816280491784, 'dimensionless')>]
logspace stuff at 3.5367 seconds
Starting iteration 5 at 3.5542 seconds
AR : 9.999999999611775 dimensionless
CD : 0.07208383829260301 dimensionless
CL : 0.9999998115160276 dimensionless
S : 0.6639218067517705 meter ** 2
V : 3.600069044356998 meter / second
W : 5.270412465184867 newton
Wwing : 0.20138432032400524 newton
e : 0.9921187131764504 dimensionless
lam : 0.4005573159778744 dimensionless
Calling cvxopt.solvers.cp at 3.5581 seconds
Got sol from cvxopt at 3.5648 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 2.031955843004712e-08
relative gap 7.726423169498243e-09
primal objective -2.6298790506664265
dual objective -2.629879060964246
primal slack 1.961702717405949e-11
dual slack 2.4096853737212874e-11
primal infeasibility 2.93236429442893e-09
dual infeasibility 2.967263152169171e-09
AVL run case - lam, AR: 0.39882645454912435 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: 0.9920158805953975 dimensionless
dydx: [<Quantity(-6.436454802472014e-06, 'dimensionless')>, <Quantity(-0.0013814190268079951, 'dimensionless')>]
logspace stuff at 4.1045 seconds
Starting iteration 6 at 4.1220 seconds
AR : 9.999999999619773 dimensionless
CD : 0.07208714305299402 dimensionless
CL : 0.9999998157581855 dimensionless
S : 0.6639218065905538 meter ** 2
V : 3.6000690386621352 meter / second
W : 5.270412469588729 newton
Wwing : 0.20138432025057307 newton
e : 0.9920165401543579 dimensionless
lam : 0.39882645454912435 dimensionless
Calling cvxopt.solvers.cp at 4.1257 seconds
Got sol from cvxopt at 4.1325 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 2.0211071384287106e-08
relative gap 7.685171306970461e-09
primal objective -2.6298790979396434
dual objective -2.629879108182298
primal slack 1.9527381359129242e-11
dual slack 2.395834706018389e-11
primal infeasibility 2.9156313147459703e-09
dual infeasibility 2.9337884446774703e-09
AVL run case - lam, AR: 0.39881343719465984 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: 0.9920158812322912 dimensionless
dydx: [<Quantity(-5.709581030188815e-07, 'dimensionless')>, <Quantity(-0.0013813957758107565, 'dimensionless')>]
logspace stuff at 4.6702 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 (1.043842e-07) within tolerance (1.000000e-06)  

Messages
--------
   1. Wolfe Condition 1 failed at iteration 3 (Step 3).  Watchdog counter is 1

13.872092548132818

real	0m5.505s
user	0m3.891s
sys	0m1.842s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/optWingAvl.py passed (as expected)
=================================================


=================================================
+ echo 'pyCAPS/GPSize.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/GPSize.py test;
+ python -u pyCAPS/GPSize.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   6339.9402476213 newton

Variables
---------
   AR          :       18.0583068591        [-]         aspect ratio                                                            
   C_D_0       :        0.0127966186        [-]         Drag Coefficient, segment 0                                             
   C_D_1       :        0.0128135534        [-]         Drag Coefficient, segment 1                                             
   C_D_2       :        0.0077622395        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0   :        0.0017626506        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1   :        0.0017626506        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2   :        0.0017626510        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0      :        0.0056016002        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1      :        0.0056028716        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2      :        0.0002594009        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0      :        0.0054327043        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1      :        0.0054483614        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2      :        0.0057382717        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0       :        0.5494535783        [-]         Lift Coefficient, segment 0                                             
   C_L_1       :        0.5495159270        [-]         Lift Coefficient, segment 1                                             
   C_L_2       :        0.1182390122        [-]         Lift Coefficient, segment 2                                             
   I_cap_bar   :        0.0000193397        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar     :    32106.9717613474       newton       Root Bending unit per unit chord                                        
   P_max       :  1211155.7559680410        watt        Maximum Engine Power                                                    
   R           :     4999.9816129528     kilometer      Single Segment range                                                    
   Re_0        :  4636790.3991634697        [-]         Reynolds Number, segment 0                                              
   Re_1        :  4427330.4209076529        [-]         Reynolds Number, segment 1                                              
   Re_2        :  9995446.9239517339        [-]         Reynolds Number, segment 2                                              
   S           :       28.3664420021     meter ** 2     total wing area                                                         
   T_0         :      799.0178645705       newton       Thrust, segment 0                                                       
   T_1         :      729.4239244544       newton       Thrust, segment 1                                                       
   T_2         :     2252.7493855701       newton       Thrust, segment 2                                                       
   V_0         :       69.5874592840   meter / second   Velocity, segment 0                                                     
   V_1         :       66.4439512429   meter / second   Velocity, segment 1                                                     
   V_2         :      150.0084591036   meter / second   Velocity, segment 2                                                     
   V_stall     :       37.9986643205   meter / second   stall speed                                                             
   W_0         :    34307.5807516552       newton       Weight, segment 0                                                       
   W_1         :    31281.5531631160       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	0m4.819s
user	0m5.034s
sys	0m0.119s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/GPSize.py passed (as expected)
=================================================

mses: /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/mses

=================================================
+ echo 'pyCAPS/MSES.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/MSES.py test;
+ python -u pyCAPS/MSES.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Objective
---------
   6436.9111747642 newton

Variables
---------
   AR                :        17.8847143703        [-]         aspect ratio                                                            
   Alpha_p20_MSES_0  :        22.6676624733       degree       Angle of Attack + 20deg from MSES, segment 0                            
   Alpha_p20_MSES_1  :        22.7725605594       degree       Angle of Attack + 20deg from MSES, segment 1                            
   Alpha_p20_MSES_2  :        18.8664426951       degree       Angle of Attack + 20deg from MSES, segment 2                            
   C_D_0             :         0.0127680026        [-]         Drag Coefficient, segment 0                                             
   C_D_1             :         0.0130143941        [-]         Drag Coefficient, segment 1                                             
   C_D_2             :         0.0074765087        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0         :         0.0017731859        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1         :         0.0017731859        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2         :         0.0017731859        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0            :         0.0053689965        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1            :         0.0055861389        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2            :         0.0002610120        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0            :         0.0056258204        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1            :         0.0056550700        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2            :         0.0054423095        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0             :         0.5353228067        [-]         Lift Coefficient, segment 0                                             
   C_L_1             :         0.5460488610        [-]         Lift Coefficient, segment 1                                             
   C_L_2             :         0.1180337615        [-]         Lift Coefficient, segment 2                                             
   C_L_MSES_0        :         0.5353228067        [-]         Lift Coefficient from MSES, segment 0                                   
   C_L_MSES_1        :         0.5460488610        [-]         Lift Coefficient from MSES, segment 1                                   
   C_L_MSES_2        :         0.1180337615        [-]         Lift Coefficient from MSES, segment 2                                   
   I_cap_bar         :         0.0000189923        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar           :     31649.2629256045       newton       Root Bending unit per unit chord                                        
   P_max             :   1155819.0983774771        watt        Maximum Engine Power                                                    
   R                 :      5000.0000010210     kilometer      Single Segment range                                                    
   Re_0              :   4702125.2746726070        [-]         Reynolds Number, segment 0                                              
   Re_1              :   4440814.5793337049        [-]         Reynolds Number, segment 1                                              
   Re_2              :  10013489.5565969180        [-]         Reynolds Number, segment 2                                              
   S                 :        28.1978812745     meter ** 2     total wing area                                                         
   T_0               :       811.9144361127       newton       Thrust, segment 0                                                       
   T_1               :       738.1899382843       newton       Thrust, segment 1                                                       
   T_2               :      2156.2042613309       newton       Thrust, segment 2                                                       
   V_0               :        70.4366540784   meter / second   Velocity, segment 0                                                     
   V_1               :        66.5224856090   meter / second   Velocity, segment 1                                                     
   V_2               :       150.0000049409   meter / second   Velocity, segment 2                                                     
   V_stall           :        37.9999998304   meter / second   stall speed                                                             
   W_0               :     34040.6240956632       newton       Weight, segment 0                                                       
   W_1               :     30972.5122439076       newton       Weight, segment 1                                                       
   W_2               :     34040.6240956631       newton       Weight, segment 2                                                       
   W_MTO             :     37409.4238057056       newton       Maximum Takeoff Weight                                                  
   W_cap             :      4178.0707911956       newton       Weight of Wing Spar Cap                                                 
   W_eng             :      2748.1693321190       newton       Engine Weight                                                           
   W_fuel_out        :      3368.7993606073       newton       Weight of fuel, outbound                                                
   W_fuel_ret        :      3068.1118141569       newton       Weight of fuel, return                                                  
   W_pay             :      4905.0000238714       newton       Payload Weight                                                          
   W_tilde           :     22353.1693245709       newton       Dry Weight, no wing                                                     
   W_web             :       131.6008887574       newton       Weight of Wing Spar Shear Web                                           
   W_wing            :      8619.3429955669       newton       wing weight                                                             
   W_zfw             :     30972.5122296163       newton       Zero Fuel Weight                                                        
   eta_0_0           :         0.2695063546        [-]         Overall Efficiency, segment 0                                           
   eta_0_1           :         0.2690604520        [-]         Overall Efficiency, segment 1                                           
   eta_0_2           :         0.2798281448        [-]         Overall Efficiency, segment 2                                           
   eta_i_0           :         0.9059037131        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1           :         0.9044048805        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2           :         0.9405988059        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0        :         0.7700181561        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1        :         0.7687441484        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2        :         0.7995089850        [-]         Propeller Efficiency, segment 2                                         
   nu                :         0.7859963973        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p                 :         1.9000000011        [-]         Dummy Variable (1+2*lam_w)                                              
   q                 :         1.4500000023        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar         :         0.0042510724        [-]         Spar cap thickness per unit chord                                       
   t_web_bar         :         0.0005949804        [-]         Spar web thickness per unit chord                                       
   tau               :         0.1499998017        [-]         airfoil thickness to chord ratio                                        
   z_bre_0           :         0.0943682262        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1           :         0.0944547882        [-]         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   :  31 
   Termination Status     :  Converged, relative change in the objective function (8.48e-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 8 (Step 8).  Watchdog counter is 2
    6. Wolfe Condition 1 failed at iteration 11 (Step 11).  Watchdog counter is 1
    7. Wolfe Condition 1 failed at iteration 12 (Step 12).  Watchdog counter is 2
    8. Wolfe Condition 1 failed at iteration 13 (Step 13).  Watchdog counter is 3
    9. 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.
   10. Wolfe Condition 1 failed at iteration 14 (Step 14).  Watchdog counter is 4
   11. Wolfe Condition 1 failed at iteration 16 (Step 16).  Watchdog counter is 1
   12. Wolfe Condition 1 failed at iteration 17 (Step 17).  Watchdog counter is 2


real	3m24.053s
user	3m20.253s
sys	0m3.659s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/MSES.py passed (as expected)
=================================================


=================================================
+ echo 'pyCAPS/Camber.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/Camber.py test;
+ python -u pyCAPS/Camber.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 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
---------
   5491.4359225133 newton

Variables
---------
   AR                :        16.4147174429        [-]         aspect ratio                                                            
   Alpha_p20_MSES_0  :        18.0126155823       degree       Angle of Attack + 20deg from MSES, segment 0                            
   Alpha_p20_MSES_1  :        18.1754881520       degree       Angle of Attack + 20deg from MSES, segment 1                            
   Alpha_p20_MSES_2  :        14.5292099988       degree       Angle of Attack + 20deg from MSES, segment 2                            
   C_D_0             :         0.0102948117        [-]         Drag Coefficient, segment 0                                             
   C_D_1             :         0.0107150833        [-]         Drag Coefficient, segment 1                                             
   C_D_2             :         0.0069659104        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0         :         0.0019058054        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1         :         0.0019058054        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2         :         0.0019058054        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0            :         0.0044487314        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1            :         0.0048480057        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2            :         0.0002903621        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0            :         0.0039402749        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1            :         0.0039612726        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2            :         0.0047697411        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0             :         0.4642555300        [-]         Lift Coefficient, segment 0                                             
   C_L_1             :         0.4845048407        [-]         Lift Coefficient, segment 1                                             
   C_L_2             :         0.1187898747        [-]         Lift Coefficient, segment 2                                             
   C_L_MSES_0        :         0.4642555300        [-]         Lift Coefficient from MSES, segment 0                                   
   C_L_MSES_1        :         0.4845048407        [-]         Lift Coefficient from MSES, segment 1                                   
   C_L_MSES_2        :         0.1187898747        [-]         Lift Coefficient from MSES, segment 2                                   
   I_cap_bar         :         0.0000169655        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar           :     28632.8148697486       newton       Root Bending unit per unit chord                                        
   P_max             :    995317.3030262130        watt        Maximum Engine Power                                                    
   R                 :      5000.0000150914     kilometer      Single Segment range                                                    
   Re_0              :   5146611.2342969924        [-]         Reynolds Number, segment 0                                              
   Re_1              :   4834919.6517840819        [-]         Reynolds Number, segment 1                                              
   Re_2              :  10114462.7451584097        [-]         Reynolds Number, segment 2                                              
   S                 :        26.2686333615     meter ** 2     total wing area                                                         
   T_0               :       708.1364694815       newton       Thrust, segment 0                                                       
   T_1               :       647.1687649939       newton       Thrust, segment 1                                                       
   T_2               :      1869.9310318896       newton       Thrust, segment 2                                                       
   V_0               :        76.2664901710   meter / second   Velocity, segment 0                                                     
   V_1               :        71.6311268476   meter / second   Velocity, segment 1                                                     
   V_2               :       150.0000569370   meter / second   Velocity, segment 2                                                     
   V_stall           :        37.9862969911   meter / second   stall speed                                                             
   W_0               :     31915.7596170390       newton       Weight, segment 0                                                       
   W_1               :     29289.9561426453       newton       Weight, segment 1                                                       
   W_2               :     31915.7596170390       newton       Weight, segment 2                                                       
   W_MTO             :     34825.3028076972       newton       Maximum Takeoff Weight                                                  
   W_cap             :      3504.9733685113       newton       Weight of Wing Spar Cap                                                 
   W_eng             :      2435.1503729458       newton       Engine Weight                                                           
   W_fuel_out        :      2865.6326794429       newton       Weight of fuel, outbound                                                
   W_fuel_ret        :      2625.8032430704       newton       Weight of fuel, return                                                  
   W_pay             :      4905.0001242919       newton       Payload Weight                                                          
   W_tilde           :     22040.1505203108       newton       Dry Weight, no wing                                                     
   W_web             :       119.9293311624       newton       Weight of Wing Spar Shear Web                                           
   W_wing            :      7249.8053469954       newton       wing weight                                                             
   W_zfw             :     29289.9559483835       newton       Zero Fuel Weight                                                        
   camberLocation    :         0.7087509688        [-]         location of maximum airfoil camber scaled by chord                      
   eta_0_0           :         0.2755554590        [-]         Overall Efficiency, segment 0                                           
   eta_0_1           :         0.2747888706        [-]         Overall Efficiency, segment 1                                           
   eta_0_2           :         0.2819554372        [-]         Overall Efficiency, segment 2                                           
   eta_i_0           :         0.9262368370        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1           :         0.9236600693        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2           :         0.9477493688        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0        :         0.7873013115        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1        :         0.7851110589        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2        :         0.8055869634        [-]         Propeller Efficiency, segment 2                                         
   maxCamber         :         0.0491463515        [-]         maximum airfoil camber scaled by chord                                  
   nu                :         0.7859964213        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p                 :         1.9000000162        [-]         Dummy Variable (1+2*lam_w)                                              
   q                 :         1.4500000250        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar         :         0.0037976551        [-]         Spar cap thickness per unit chord                                       
   t_web_bar         :         0.0005785209        [-]         Spar web thickness per unit chord                                       
   tau               :         0.1495748504        [-]         airfoil thickness to chord ratio                                        
   z_bre_0           :         0.0860294936        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1           :         0.0859477878        [-]         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   :  99 
   Termination Status     :  Converged, relative change in the objective function (7.65e-06) is witin specified tolerance (1.00e-05) 

Messages
--------
    1. Attempted step of size 1.00e+00 at iteration 1 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 1.00e+00 at iteration 7 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    4. Wolfe Condition 1 failed at iteration 8 (Step 8).  Watchdog counter is 1
    5. 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.
    6. Wolfe Condition 1 failed at iteration 11 (Step 11).  Watchdog counter is 1
    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 14 (Step 14).  Watchdog counter is 1
    9. 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.
   10. Wolfe Condition 1 failed at iteration 18 (Step 18).  Watchdog counter is 1
   11. Wolfe Condition 1 failed at iteration 21 (Step 21).  Watchdog counter is 1
   12. Attempted step of size 2.15e-01 at iteration 27 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   13. Attempted step of size 1.77e-01 at iteration 32 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   14. Attempted step of size 1.57e-01 at iteration 36 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 37 (Step 37).  Watchdog counter is 1
   16. Attempted step of size 1.42e-01 at iteration 40 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   17. Wolfe Condition 1 failed at iteration 43 (Step 43).  Watchdog counter is 1
   18. Attempted step of size 1.30e-01 at iteration 44 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   19. Wolfe Condition 1 failed at iteration 49 (Step 49).  Watchdog counter is 1
   20. Wolfe Condition 1 failed at iteration 50 (Step 50).  Watchdog counter is 2
   21. Attempted step of size 1.13e-01 at iteration 52 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   22. Attempted step of size 1.09e-01 at iteration 54 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   23. Attempted step of size 3.28e-02 at iteration 54 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   24. Wolfe Condition 1 failed at iteration 59 (Step 59).  Watchdog counter is 1
   25. Wolfe Condition 1 failed at iteration 60 (Step 60).  Watchdog counter is 2
   26. Wolfe Condition 1 failed at iteration 62 (Step 62).  Watchdog counter is 1
   27. Wolfe Condition 1 failed at iteration 67 (Step 67).  Watchdog counter is 1
   28. Wolfe Condition 1 failed at iteration 68 (Step 68).  Watchdog counter is 2
   29. Attempted step of size 8.84e-02 at iteration 71 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   30. Wolfe Condition 1 failed at iteration 72 (Step 72).  Watchdog counter is 1
   31. Wolfe Condition 1 failed at iteration 73 (Step 73).  Watchdog counter is 2
   32. Wolfe Condition 1 failed at iteration 74 (Step 74).  Watchdog counter is 3
   33. Wolfe Condition 1 failed at iteration 75 (Step 75).  Watchdog counter is 4
   34. Wolfe Condition 1 failed at iteration 95 (Step 95).  Watchdog counter is 1


real	10m54.967s
user	10m42.488s
sys	0m11.527s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/Camber.py passed (as expected)
=================================================


=================================================
+ echo 'pyCAPS/CMConstraint.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/CMConstraint.py test;
+ python -u pyCAPS/CMConstraint.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 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
---------
   6389.1599788872 newton

Variables
---------
   AR                :       18.1246600755        [-]         aspect ratio                                                            
   Alpha_p20_MSES_0  :       22.7354842586       degree       Angle of Attack + 20deg from MSES, segment 0                            
   Alpha_p20_MSES_1  :       22.7563511509       degree       Angle of Attack + 20deg from MSES, segment 1                            
   Alpha_p20_MSES_2  :       18.6841775414       degree       Angle of Attack + 20deg from MSES, segment 2                            
   C_D_0             :        0.0132149995        [-]         Drag Coefficient, segment 0                                             
   C_D_1             :        0.0132499519        [-]         Drag Coefficient, segment 1                                             
   C_D_2             :        0.0075834110        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0         :        0.0017623324        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1         :        0.0017623324        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2         :        0.0017623324        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0            :        0.0058797215        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1            :        0.0059269314        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2            :        0.0002582450        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0            :        0.0055729459        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1            :        0.0055606884        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2            :        0.0055628314        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0             :        0.5638905478        [-]         Lift Coefficient, segment 0                                             
   C_L_1             :        0.5661550132        [-]         Lift Coefficient, segment 1                                             
   C_L_2             :        0.1181879141        [-]         Lift Coefficient, segment 2                                             
   C_L_MSES_0        :        0.5638905478        [-]         Lift Coefficient from MSES, segment 0                                   
   C_L_MSES_1        :        0.5661550132        [-]         Lift Coefficient from MSES, segment 1                                   
   C_L_MSES_2        :        0.1181879141        [-]         Lift Coefficient from MSES, segment 2                                   
   I_cap_bar         :        0.0000194277        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar           :    32142.4766677387       newton       Root Bending unit per unit chord                                        
   P_max             :  1180922.1189759877        watt        Maximum Engine Power                                                    
   R                 :     5000.0000115189     kilometer      Single Segment range                                                    
   Re_0              :  4569113.0350051858        [-]         Reynolds Number, segment 0                                              
   Re_1              :  4352777.0943119153        [-]         Reynolds Number, segment 1                                              
   Re_2              :  9977785.5636399947        [-]         Reynolds Number, segment 2                                              
   S                 :       28.3718598326     meter ** 2     total wing area                                                         
   T_0               :      803.8161139074       newton       Thrust, segment 0                                                       
   T_1               :      731.4741552257       newton       Thrust, segment 1                                                       
   T_2               :     2200.5003332610       newton       Thrust, segment 2                                                       
   V_0               :       68.6872633568   meter / second   Velocity, segment 0                                                     
   V_1               :       65.4352286761   meter / second   Velocity, segment 1                                                     
   V_2               :      150.0000174706   meter / second   Velocity, segment 2                                                     
   V_stall           :       37.9999992819   meter / second   stall speed                                                             
   W_0               :    34295.4186254629       newton       Weight, segment 0                                                       
   W_1               :    31251.0744708949       newton       Weight, segment 1                                                       
   W_2               :    34295.4186254629       newton       Weight, segment 2                                                       
   W_MTO             :    37640.2357223150       newton       Maximum Takeoff Weight                                                  
   W_cap             :     4291.8687051105       newton       Weight of Wing Spar Cap                                                 
   W_eng             :     2795.9949775438       newton       Engine Weight                                                           
   W_fuel_out        :     3344.8158627813       newton       Weight of fuel, outbound                                                
   W_fuel_ret        :     3044.3441161059       newton       Weight of fuel, return                                                  
   W_pay             :     4905.0002866763       newton       Payload Weight                                                          
   W_tilde           :    22400.9952205062       newton       Dry Weight, no wing                                                     
   W_web             :      133.1707762079       newton       Weight of Wing Spar Shear Web                                           
   W_wing            :     8850.0789606646       newton       wing weight                                                             
   W_zfw             :    31251.0742320470       newton       Zero Fuel Weight                                                        
   camberLocation    :        0.3743117570        [-]         location of maximum airfoil camber scaled by chord                      
   eta_0_0           :        0.2685537422        [-]         Overall Efficiency, segment 0                                           
   eta_0_1           :        0.2684906678        [-]         Overall Efficiency, segment 1                                           
   eta_0_2           :        0.2795064938        [-]         Overall Efficiency, segment 2                                           
   eta_i_0           :        0.9027016546        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1           :        0.9024896397        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2           :        0.9395176263        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0        :        0.7672964064        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1        :        0.7671161938        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2        :        0.7985899824        [-]         Propeller Efficiency, segment 2                                         
   maxCamber         :        0.0222539259        [-]         maximum airfoil camber scaled by chord                                  
   negCMp1_0         :        1.0554550403        [-]         Negative CM about 0.25c + 1, segment 0                                  
   negCMp1_1         :        1.0551745498        [-]         Negative CM about 0.25c + 1, segment 1                                  
   negCMp1_2         :        1.0580510080        [-]         Negative CM about 0.25c + 1, segment 2                                  
   nu                :        0.7859964727        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p                 :        1.9000000085        [-]         Dummy Variable (1+2*lam_w)                                              
   q                 :        1.4500000156        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar         :        0.0043555913        [-]         Spar cap thickness per unit chord                                       
   t_web_bar         :        0.0006005377        [-]         Spar web thickness per unit chord                                       
   tau               :        0.1499999234        [-]         airfoil thickness to chord ratio                                        
   z_bre_0           :        0.0930629119        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1           :        0.0929596776        [-]         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   :  26 
   Termination Status     :  Converged, relative change in the objective function (3.87e-06) is witin specified tolerance (1.00e-05) 

Messages
--------
    1. Wolfe Condition 1 failed at iteration 3 (Step 3).  Watchdog counter is 1
    2. Attempted step of size 1.00e+00 at iteration 6 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 7 (Step 7).  Watchdog counter is 1
    4. Wolfe Condition 1 failed at iteration 9 (Step 9).  Watchdog counter is 1
    5. Wolfe Condition 1 failed at iteration 12 (Step 12).  Watchdog counter is 1
    6. Wolfe Condition 1 failed at iteration 13 (Step 13).  Watchdog counter is 2
    7. 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.
    8. 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.
    9. Wolfe Condition 1 failed at iteration 21 (Step 21).  Watchdog counter is 1
   10. Attempted step of size 2.87e-01 at iteration 22 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   11. Attempted step of size 2.37e-01 at iteration 25 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   12. Attempted step of size 7.12e-02 at iteration 25 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   13. Attempted step of size 2.14e-02 at iteration 25 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   14. Attempted step of size 6.41e-03 at iteration 25 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.


real	3m36.137s
user	3m32.597s
sys	0m3.480s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case pyCAPS/CMConstraint.py passed (as expected)
=================================================

Traceback (most recent call last):
  File "<string>", line 1, in <module>
ModuleNotFoundError: No module named 'torch'

*************************************************
*************************************************

=================================================
Did not run examples for:

awave
autoLink
Pointwise
Fun3D
abaqus
Nastran
Mystran
Plato
Mystran
=================================================

All tests pass!


=================================================
=================================================
+ cd /Users/jenkins/workspace/ESP_bPreBuilt
+ mkdir -p /Users/jenkins/workspace/ESP_bPreBuilt/test/plugs
+ cd /Users/jenkins/workspace/ESP_bPreBuilt/test/plugs
+ find /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs -name 'plugs0*.csm'
+ sort -f
+ awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/data/plugs/plugsFailure.txt
+ cp /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/data/plugs/plugsIgnore.txt .
+ set +x
Testing CSM files:
data/Plugs/plugs0a.csm
data/Plugs/plugs0b.csm
data/Plugs/plugs0c.csm
data/Plugs/plugs0d.csm
total 46488
-rw-r--r--  1 jenkins  staff   1.2M Dec 20 15:00 ASTRO.D01
-rw-r--r--  1 jenkins  staff   277K Dec 20 15:00 ASTRO.IDX
-rwxr-xr-x  1 jenkins  staff   130K Dec 20 15:01 ESPxddm
-rwxr-xr-x  1 jenkins  staff   212K Feb 28 10:02 Slugs
-rwxr-xr-x  1 jenkins  staff    86K Feb 28 10:02 TestFit
-rwxr-xr-x  1 jenkins  staff   1.6M Dec 20 15:00 avl
-rwxr-xr-x  1 jenkins  staff    51K Feb 28 10:02 cart3dTest
-rwxr-xr-x  1 jenkins  staff    51K Mar  6 20:09 egads2cart
-rwxr-xr-x  1 jenkins  staff   403K Dec 20 15:00 friction
-rwxr-xr-x  1 jenkins  staff    10M Dec 20 15:00 mastros.exe
-rwxr-xr-x  1 jenkins  staff   749K Dec 20 15:00 mses
-rwxr-xr-x  1 jenkins  staff   1.4M Dec 20 15:00 mset
-rwxr-xr-x  1 jenkins  staff    51K Feb 28 10:02 phaseUtil
-rw-r--r--  1 jenkins  staff   1.6K Mar  6 20:31 pod.egads
-rw-r--r--  1 jenkins  staff     0B Mar  6 20:31 port7681.jrnl
-rwxr-xr-x  1 jenkins  staff   1.2M Dec 20 15:00 pplot
-rwxr-xr-x  1 jenkins  staff   1.1M Dec 20 15:00 pxplot
-rwxr-xr-x  1 jenkins  staff    68K Feb 28 10:02 sensCSM
-rwxr-xr-x  1 jenkins  staff   192K Feb 28 10:02 serveCSM
-rwxr-xr-x  1 jenkins  staff   176K Feb 28 10:02 serveESP
-rwxr-xr-x  1 jenkins  staff    52K Feb 28 10:02 vCurvature
-rwxr-xr-x  1 jenkins  staff    51K Feb 28 10:02 vGeom
-rwxr-xr-x  1 jenkins  staff    53K Feb 28 10:02 vTess
-rwxr-xr-x  1 jenkins  staff   1.7M Mar  6 20:09 vTesstatic
-rw-r--r--  1 jenkins  staff   195K Mar  6 20:31 wingMultiModel.bdf
-rwxr-xr-x  1 jenkins  staff   1.7M Dec 20 15:00 xfoil
( 1 / 4 )
data/Plugs/plugs0a.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0a.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0a.vfy", so verification is being skipped

===================================
PLUGS with 4562 points in the cloud
===================================


PLUGS phase1: match bounding boxes


PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
    Pass  1 converged, dmax= 5.416e-07,     rmsbest= 6.132e-04, reclass= 4562, unclass=    0
Starting pass 2 (of 25) of phase2
    Pass  2 converged, dmax= 5.366e-07,     rmsbest= 7.097e-04, reclass=    2, unclass=    0
Starting pass 3 (of 25) of phase2

    Phase2 passes converged because points are classified same as previous pass


==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m4.321s
user	0m4.321s
sys	0m0.216s
++ set +x
data/Plugs/plugs0a                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 2 / 4 )
data/Plugs/plugs0b.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0b.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0b.vfy", so verification is being skipped

===================================
PLUGS with 4562 points in the cloud
===================================


PLUGS phase1: match bounding boxes


PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
    Pass  1 converged, dmax= 3.039e-07,     rmsbest= 4.036e-02, reclass= 4562, unclass=    0
Starting pass 2 (of 25) of phase2
    Pass  2 converged, dmax= 2.814e-07,     rmsbest= 1.924e-03, reclass= 1033, unclass=    0
Starting pass 3 (of 25) of phase2
    Pass  3 converged, dmax= 4.494e-07,     rmsbest= 5.920e-04, reclass=  473, unclass=    0
Starting pass 4 (of 25) of phase2
    Pass  4 converged, dmax= 5.366e-07,     rmsbest= 7.097e-04, reclass=   17, unclass=    0
Starting pass 5 (of 25) of phase2

    Phase2 passes converged because points are classified same as previous pass


==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m3.831s
user	0m4.800s
sys	0m0.019s
++ set +x
data/Plugs/plugs0b                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 3 / 4 )
data/Plugs/plugs0c.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0c.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0c.vfy", so verification is being skipped

===================================
PLUGS with 4562 points in the cloud
===================================


PLUGS phase1: match bounding boxes


PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
    Pass  1 ran out of iterations,          rmsbest= 1.677e-01, reclass= 4562, unclass=  554
Starting pass 2 (of 25) of phase2
    Pass  2 converged, dmax= 4.016e-07,     rmsbest= 6.330e-02, reclass= 1676, unclass=    0
Starting pass 3 (of 25) of phase2
    Pass  3 converged, dmax= 1.881e-07,     rmsbest= 8.736e-03, reclass=  791, unclass=    0
Starting pass 4 (of 25) of phase2
    Pass  4 converged, dmax= 3.081e-07,     rmsbest= 1.037e-03, reclass=  428, unclass=    0
Starting pass 5 (of 25) of phase2
    Pass  5 converged, dmax= 5.816e-07,     rmsbest= 7.097e-04, reclass=  109, unclass=    0
Starting pass 6 (of 25) of phase2

    Phase2 passes converged because points are classified same as previous pass


==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m12.055s
user	0m19.190s
sys	0m0.037s
++ set +x
data/Plugs/plugs0c                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 4 / 4 )
data/Plugs/plugs0d.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0d.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0d.vfy", so verification is being skipped

===================================
PLUGS with 4562 points in the cloud
===================================


PLUGS phase1: match bounding boxes


PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
    Pass  1 ran out of iterations,          rmsbest= 1.677e-01, reclass= 4562, unclass=  554
Starting pass 2 (of 25) of phase2
    Pass  2 converged, dmax= 4.016e-07,     rmsbest= 6.330e-02, reclass= 1676, unclass=    0
Starting pass 3 (of 25) of phase2
    Pass  3 converged, dmax= 1.881e-07,     rmsbest= 8.736e-03, reclass=  791, unclass=    0
Starting pass 4 (of 25) of phase2
    Pass  4 converged, dmax= 3.081e-07,     rmsbest= 1.037e-03, reclass=  428, unclass=    0
Starting pass 5 (of 25) of phase2
    Pass  5 converged, dmax= 5.816e-07,     rmsbest= 7.097e-04, reclass=  109, unclass=    0
Starting pass 6 (of 25) of phase2

    Phase2 passes converged because points are classified same as previous pass


==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m12.006s
user	0m19.100s
sys	0m0.032s
++ set +x
data/Plugs/plugs0d                  passed (as expected)
--------------------------------------------------------------------------------------------------
[Execution node] check if [viggen] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_bPreBuilt/ESPVersion=beta,buildnode=viggen #67'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS