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 macys 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 [macys] is in [[macys, macys_VM, master, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-rhel7, reynolds-ubuntu16, reynolds-ubuntu18, reynolds-ubuntu20]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[ESP_bPreBuilt] $ /bin/bash -xe /var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T/jenkins5257304172116761627.sh
+ bash -ex /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/ESP_PreBuilt.sh
+ source /Users/jenkins/workspace/ESP_bPreBuilt/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.6
++ OCCTREF=7.6
++ AFLR_VERSION=11.5.9
++ 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
++ [[ macys == \r\e\y\n\o\l\d\s ]]
++ [[ '' == *\.\i\f\o\r\t ]]
++ '[' -f /opt/intel/oneapi/setvars.sh ']'
++ source /opt/intel/oneapi/setvars.sh
++ '[' -f /Users/jenkins/.bashrc ']'
++ export CAPS_OUTLEVEL=0
++ CAPS_OUTLEVEL=0
++ [[ '' == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ ESP_BLOC=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ ESP_ROOT=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/
++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//julia
++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.6 != '' ]]
++ [[ '' != '' ]]
++ [[ macys == *\r\e\y\n\o\l\d\s* ]]
++ [[ macys == *\m\a\c\y\s* ]]
++ export EMPnumProc=2
++ EMPnumProc=2
++ export OMP_NUM_THREADS=2
++ OMP_NUM_THREADS=2
++ source /Users/jenkins/.bash_profile
+++ export PATH=/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ export PATH=/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ PATH=/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin
+++ export pwid_LICENSE=5053@acdl.mit.edu
+++ pwid_LICENSE=5053@acdl.mit.edu
++ [[ macys == *\m\a\c\y\s* ]]
++ export PATH=/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys == \m\a\c\y\s ]]
++ echo 'data/fighter4.csm;          ERROR:: build not completed because error -214 (did_not_create_body) was detected'
++ echo 'data/fighter4.csm;          ERROR:: build not completed because error -214 (did_not_create_body) was detected'
++ export CASARCH=.
++ CASARCH=.
++ '[' '!' -z '' ']'
+++ ls -d '/Users/jenkins/util/ESP/OpenCASCADE-.?'
ls: /Users/jenkins/util/ESP/OpenCASCADE-.?: No such file or directory
++ export CASROOT=
++ CASROOT=
++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP/udunits/udunits2.xml
++ export ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ export DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//lib:/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/ipp/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib
++ DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//lib:/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/ipp/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib
++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.9
++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.9
++ [[ macys == *\m\a\c\y\s* ]]
++ export AFLR_ARCH=MacOSX-x86-64
++ AFLR_ARCH=MacOSX-x86-64
++ export ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ export PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ export CART3D_ARCH=OSX64_ICC
++ CART3D_ARCH=OSX64_ICC
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.34.0-MacOS
++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.34.0-MacOS
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/
++ [[ macys == \m\a\c\y\s ]]
++ export SEACAS=/Users/jenkins/util/sandialabs/seacas
++ SEACAS=/Users/jenkins/util/sandialabs/seacas
++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']'
+++ perl -I/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 -Mlocal::lib=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
++ eval 'PATH="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin${PATH:+:${PATH}}"; export PATH;
PERL5LIB="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5${PERL5LIB:+:${PERL5LIB}}"; export PERL5LIB;
PERL_LOCAL_LIB_ROOT="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl${PERL_LOCAL_LIB_ROOT:+:${PERL_LOCAL_LIB_ROOT}}"; export PERL_LOCAL_LIB_ROOT;
PERL_MB_OPT="--install_base \"/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl\""; export PERL_MB_OPT;
PERL_MM_OPT="INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"; export PERL_MM_OPT;'
+++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
+++ export PATH
+++ PERL5LIB=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5
+++ export PERL5LIB
+++ PERL_LOCAL_LIB_ROOT=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
+++ export PERL_LOCAL_LIB_ROOT
+++ PERL_MB_OPT='--install_base "/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"'
+++ export PERL_MB_OPT
+++ PERL_MM_OPT=INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
+++ export PERL_MM_OPT
++ export PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_bPreBuilt/ESP//test:/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_bPreBuilt/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_bPreBuilt/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_bPreBuilt/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ [[ macys == \m\a\c\y\s* ]]
++ mkdir -p /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin
++ rm -f /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python
++ rm -f /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/python-config
++ rm -f /Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/virtualenv
++ rm -f '/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/analyze-*'
++ rm -f '/Users/jenkins/workspace/ESP_bPreBuilt/ESP//bin/intercept-*'
++ [[ macys == \m\a\c\y\s ]]
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/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'
++ [[ macys == \m\a\c\y\s ]]
++ 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=x86_64
+ wget --tries=3 https://acdl.mit.edu/ESP/archive/ESPbeta-macos-x86_64.tgz
--2024-03-06 20:30:42--  https://acdl.mit.edu/ESP/archive/ESPbeta-macos-x86_64.tgz
Resolving acdl.mit.edu (acdl.mit.edu)... 18.18.33.14
Connecting to acdl.mit.edu (acdl.mit.edu)|18.18.33.14|:443... connected.
HTTP request sent, awaiting response... 200 OK
Length: 550292565 (525M) [application/x-gzip]
Saving to: ‘ESPbeta-macos-x86_64.tgz’

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  6950K .......... .......... .......... .......... ..........  1% 13.6M 57s
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  7050K .......... .......... .......... .......... ..........  1% 33.4M 57s
  7100K .......... .......... .......... .......... ..........  1% 26.1M 56s
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  7200K .......... .......... .......... .......... ..........  1% 27.4M 56s
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  7650K .......... .......... .......... .......... ..........  1% 23.7M 54s
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  8000K .......... .......... .......... .......... ..........  1% 15.2M 53s
  8050K .......... .......... .......... .......... ..........  1% 15.5M 53s
  8100K .......... .......... .......... .......... ..........  1% 12.1M 53s
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  8200K .......... .......... .......... .......... ..........  1% 9.49M 53s
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  9100K .......... .......... .......... .......... ..........  1% 15.6M 54s
  9150K .......... .......... .......... .......... ..........  1% 39.1M 54s
  9200K .......... .......... .......... .......... ..........  1% 26.0M 54s
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  9900K .......... .......... .......... .......... ..........  1% 11.8M 52s
  9950K .......... .......... .......... .......... ..........  1% 8.99M 52s
 10000K .......... .......... .......... .......... ..........  1% 11.0M 52s
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 20400K .......... .......... .......... .......... ..........  3% 4.01M 51s
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 20650K .......... .......... .......... .......... ..........  3%  105M 51s
 20700K .......... .......... .......... .......... ..........  3% 26.0M 51s
 20750K .......... .......... .......... .......... ..........  3% 21.0M 51s
 20800K .......... .......... .......... .......... ..........  3% 30.6M 51s
 20850K .......... .......... .......... .......... ..........  3% 24.5M 51s
 20900K .......... .......... .......... .......... ..........  3% 30.9M 50s
 20950K .......... .......... .......... .......... ..........  3% 19.9M 50s
 21000K .......... .......... .......... .......... ..........  3% 25.4M 50s
 21050K .......... .......... .......... .......... ..........  3% 13.0M 50s
 21100K .......... .......... .......... .......... ..........  3% 16.9M 50s
 21150K .......... .......... .......... .......... ..........  3% 17.3M 50s
 21200K .......... .......... .......... .......... ..........  3% 13.5M 50s
 21250K .......... .......... .......... .......... ..........  3% 17.9M 50s
 21300K .......... .......... .......... .......... ..........  3% 18.0M 50s
 21350K .......... .......... .......... .......... ..........  3% 11.4M 50s
 21400K .......... .......... .......... .......... ..........  3% 14.0M 50s
 21450K .......... .......... .......... .......... ..........  4% 12.0M 50s
 21500K .......... .......... .......... .......... ..........  4% 11.1M 50s
 21550K .......... .......... .......... .......... ..........  4% 11.5M 50s
 21600K .......... .......... .......... .......... ..........  4% 24.9M 50s
 21650K .......... .......... .......... .......... ..........  4% 25.4M 50s
 21700K .......... .......... .......... .......... ..........  4% 14.1M 50s
 21750K .......... .......... .......... .......... ..........  4% 90.4M 50s
 21800K .......... .......... .......... .......... ..........  4% 14.5M 50s
 21850K .......... .......... .......... .......... ..........  4% 19.6M 50s
 21900K .......... .......... .......... .......... ..........  4% 16.6M 49s
 21950K .......... .......... .......... .......... ..........  4% 21.4M 49s
 22000K .......... .......... .......... .......... ..........  4% 15.4M 49s
 22050K .......... .......... .......... .......... ..........  4% 11.1M 49s
 22100K .......... .......... .......... .......... ..........  4% 9.71M 49s
 22150K .......... .......... .......... .......... ..........  4% 11.4M 49s
 22200K .......... .......... .......... .......... ..........  4% 9.50M 49s
 22250K .......... .......... .......... .......... ..........  4% 10.8M 49s
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 22350K .......... .......... .......... .......... ..........  4% 8.27M 49s
 22400K .......... .......... .......... .......... ..........  4% 13.0M 49s
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 22500K .......... .......... .......... .......... ..........  4% 12.2M 49s
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 22600K .......... .......... .......... .......... ..........  4% 15.3M 49s
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 22700K .......... .......... .......... .......... ..........  4% 20.1M 49s
 22750K .......... .......... .......... .......... ..........  4% 26.1M 49s
 22800K .......... .......... .......... .......... ..........  4% 65.5M 49s
 22850K .......... .......... .......... .......... ..........  4% 14.1M 49s
 22900K .......... .......... .......... .......... ..........  4% 22.1M 49s
 22950K .......... .......... .......... .......... ..........  4% 17.6M 49s
 23000K .......... .......... .......... .......... ..........  4% 19.1M 49s
 23050K .......... .......... .......... .......... ..........  4% 17.7M 49s
 23100K .......... .......... .......... .......... ..........  4% 18.5M 49s
 23150K .......... .......... .......... .......... ..........  4% 14.0M 49s
 23200K .......... .......... .......... .......... ..........  4% 12.2M 49s
 23250K .......... .......... .......... .......... ..........  4% 19.0M 49s
 23300K .......... .......... .......... .......... ..........  4% 17.4M 48s
 23350K .......... .......... .......... .......... ..........  4% 11.9M 48s
 23400K .......... .......... .......... .......... ..........  4% 17.1M 48s
 23450K .......... .......... .......... .......... ..........  4% 15.1M 48s
 23500K .......... .......... .......... .......... ..........  4% 21.1M 48s
 23550K .......... .......... .......... .......... ..........  4% 9.15M 48s
 23600K .......... .......... .......... .......... ..........  4% 7.20M 48s
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 23700K .......... .......... .......... .......... ..........  4% 5.66M 48s
 23750K .......... .......... .......... .......... ..........  4% 5.52M 49s
 23800K .......... .......... .......... .......... ..........  4% 6.68M 49s
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 24050K .......... .......... .......... .......... ..........  4% 7.81M 49s
 24100K .......... .......... .......... .......... ..........  4% 5.58M 49s
 24150K .......... .......... .......... .......... ..........  4% 6.80M 49s
 24200K .......... .......... .......... .......... ..........  4% 4.78M 49s
 24250K .......... .......... .......... .......... ..........  4% 10.4M 49s
 24300K .......... .......... .......... .......... ..........  4% 11.5M 49s
 24350K .......... .......... .......... .......... ..........  4% 9.52M 49s
 24400K .......... .......... .......... .......... ..........  4% 11.1M 49s
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 24650K .......... .......... .......... .......... ..........  4% 7.43M 49s
 24700K .......... .......... .......... .......... ..........  4% 7.66M 49s
 24750K .......... .......... .......... .......... ..........  4% 8.61M 49s
 24800K .......... .......... .......... .......... ..........  4% 8.10M 49s
 24850K .......... .......... .......... .......... ..........  4% 14.6M 49s
 24900K .......... .......... .......... .......... ..........  4% 18.2M 49s
 24950K .......... .......... .......... .......... ..........  4% 15.4M 49s
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 25050K .......... .......... .......... .......... ..........  4% 19.4M 49s
 25100K .......... .......... .......... .......... ..........  4% 16.1M 49s
 25150K .......... .......... .......... .......... ..........  4% 16.3M 49s
 25200K .......... .......... .......... .......... ..........  4% 16.1M 49s
 25250K .......... .......... .......... .......... ..........  4% 18.7M 49s
 25300K .......... .......... .......... .......... ..........  4% 11.7M 49s
 25350K .......... .......... .......... .......... ..........  4% 20.2M 49s
 25400K .......... .......... .......... .......... ..........  4% 15.0M 49s
 25450K .......... .......... .......... .......... ..........  4% 13.5M 49s
 25500K .......... .......... .......... .......... ..........  4% 14.6M 49s
 25550K .......... .......... .......... .......... ..........  4% 18.1M 49s
 25600K .......... .......... .......... .......... ..........  4% 9.77M 49s
 25650K .......... .......... .......... .......... ..........  4% 11.5M 49s
 25700K .......... .......... .......... .......... ..........  4% 8.54M 49s
 25750K .......... .......... .......... .......... ..........  4% 8.17M 49s
 25800K .......... .......... .......... .......... ..........  4% 7.49M 49s
 25850K .......... .......... .......... .......... ..........  4% 9.96M 49s
 25900K .......... .......... .......... .......... ..........  4% 12.2M 49s
 25950K .......... .......... .......... .......... ..........  4% 11.4M 49s
 26000K .......... .......... .......... .......... ..........  4% 11.8M 49s
 26050K .......... .......... .......... .......... ..........  4% 9.64M 49s
 26100K .......... .......... .......... .......... ..........  4% 9.37M 49s
 26150K .......... .......... .......... .......... ..........  4% 9.52M 49s
 26200K .......... .......... .......... .......... ..........  4% 7.01M 49s
 26250K .......... .......... .......... .......... ..........  4% 5.29M 49s
 26300K .......... .......... .......... .......... ..........  4% 13.8M 49s
 26350K .......... .......... .......... .......... ..........  4% 17.0M 49s
 26400K .......... .......... .......... .......... ..........  4% 24.6M 49s
 26450K .......... .......... .......... .......... ..........  4% 17.9M 49s
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 26550K .......... .......... .......... .......... ..........  4% 13.0M 49s
 26600K .......... .......... .......... .......... ..........  4% 8.09M 49s
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 26700K .......... .......... .......... .......... ..........  4% 6.79M 49s
 26750K .......... .......... .......... .......... ..........  4% 7.71M 49s
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 26850K .......... .......... .......... .......... ..........  5% 6.02M 49s
 26900K .......... .......... .......... .......... ..........  5% 9.86M 49s
 26950K .......... .......... .......... .......... ..........  5% 11.9M 49s
 27000K .......... .......... .......... .......... ..........  5% 10.3M 49s
 27050K .......... .......... .......... .......... ..........  5% 9.96M 49s
 27100K .......... .......... .......... .......... ..........  5% 7.90M 49s
 27150K .......... .......... .......... .......... ..........  5% 10.4M 49s
 27200K .......... .......... .......... .......... ..........  5% 8.48M 49s
 27250K .......... .......... .......... .......... ..........  5% 20.7M 49s
 27300K .......... .......... .......... .......... ..........  5% 21.0M 49s
 27350K .......... .......... .......... .......... ..........  5% 26.6M 49s
 27400K .......... .......... .......... .......... ..........  5% 20.8M 49s
 27450K .......... .......... .......... .......... ..........  5% 15.9M 49s
 27500K .......... .......... .......... .......... ..........  5% 14.5M 48s
 27550K .......... .......... .......... .......... ..........  5% 24.4M 48s
 27600K .......... .......... .......... .......... ..........  5% 8.55M 48s
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 27700K .......... .......... .......... .......... ..........  5% 9.27M 48s
 27750K .......... .......... .......... .......... ..........  5% 10.9M 48s
 27800K .......... .......... .......... .......... ..........  5% 12.5M 48s
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 27900K .......... .......... .......... .......... ..........  5% 15.6M 48s
 27950K .......... .......... .......... .......... ..........  5% 11.5M 48s
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 28100K .......... .......... .......... .......... ..........  5% 7.74M 48s
 28150K .......... .......... .......... .......... ..........  5% 10.2M 48s
 28200K .......... .......... .......... .......... ..........  5% 8.59M 48s
 28250K .......... .......... .......... .......... ..........  5% 9.79M 48s
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 28900K .......... .......... .......... .......... ..........  5% 39.7M 49s
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 29050K .......... .......... .......... .......... ..........  5% 37.0M 48s
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 29200K .......... .......... .......... .......... ..........  5% 25.3M 48s
 29250K .......... .......... .......... .......... ..........  5% 19.9M 48s
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 29350K .......... .......... .......... .......... ..........  5% 15.0M 48s
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 29600K .......... .......... .......... .......... ..........  5% 14.5M 48s
 29650K .......... .......... .......... .......... ..........  5% 15.4M 48s
 29700K .......... .......... .......... .......... ..........  5% 14.5M 48s
 29750K .......... .......... .......... .......... ..........  5% 15.8M 48s
 29800K .......... .......... .......... .......... ..........  5% 10.0M 48s
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 29900K .......... .......... .......... .......... ..........  5% 16.6M 48s
 29950K .......... .......... .......... .......... ..........  5% 31.5M 48s
 30000K .......... .......... .......... .......... ..........  5% 27.1M 48s
 30050K .......... .......... .......... .......... ..........  5% 38.0M 48s
 30100K .......... .......... .......... .......... ..........  5% 20.4M 47s
 30150K .......... .......... .......... .......... ..........  5% 25.4M 47s
 30200K .......... .......... .......... .......... ..........  5% 37.4M 47s
 30250K .......... .......... .......... .......... ..........  5% 31.9M 47s
 30300K .......... .......... .......... .......... ..........  5% 24.0M 47s
 30350K .......... .......... .......... .......... ..........  5% 23.7M 47s
 30400K .......... .......... .......... .......... ..........  5% 21.8M 47s
 30450K .......... .......... .......... .......... ..........  5% 15.6M 47s
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 30650K .......... .......... .......... .......... ..........  5% 17.8M 47s
 30700K .......... .......... .......... .......... ..........  5% 14.1M 47s
 30750K .......... .......... .......... .......... ..........  5% 20.0M 47s
 30800K .......... .......... .......... .......... ..........  5% 18.7M 47s
 30850K .......... .......... .......... .......... ..........  5% 14.2M 47s
 30900K .......... .......... .......... .......... ..........  5% 19.2M 47s
 30950K .......... .......... .......... .......... ..........  5% 13.6M 47s
 31000K .......... .......... .......... .......... ..........  5% 17.2M 47s
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 33800K .......... .......... .......... .......... ..........  6% 19.8M 46s
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 34150K .......... .......... .......... .......... ..........  6%  135M 46s
 34200K .......... .......... .......... .......... ..........  6% 27.1M 46s
 34250K .......... .......... .......... .......... ..........  6% 21.6M 46s
 34300K .......... .......... .......... .......... ..........  6% 17.0M 46s
 34350K .......... .......... .......... .......... ..........  6% 13.6M 46s
 34400K .......... .......... .......... .......... ..........  6% 11.6M 46s
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 34650K .......... .......... .......... .......... ..........  6% 16.6M 46s
 34700K .......... .......... .......... .......... ..........  6% 12.3M 45s
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 61800K .......... .......... .......... .......... .......... 11% 12.0M 46s
 61850K .......... .......... .......... .......... .......... 11% 8.61M 46s
 61900K .......... .......... .......... .......... .......... 11% 12.1M 46s
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 62100K .......... .......... .......... .......... .......... 11% 11.6M 46s
 62150K .......... .......... .......... .......... .......... 11% 12.1M 46s
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 62900K .......... .......... .......... .......... .......... 11% 7.60M 46s
 62950K .......... .......... .......... .......... .......... 11% 6.64M 46s
 63000K .......... .......... .......... .......... .......... 11% 6.70M 46s
 63050K .......... .......... .......... .......... .......... 11% 7.20M 46s
 63100K .......... .......... .......... .......... .......... 11% 6.79M 46s
 63150K .......... .......... .......... .......... .......... 11% 6.55M 46s
 63200K .......... .......... .......... .......... .......... 11% 5.46M 46s
 63250K .......... .......... .......... .......... .......... 11% 7.64M 46s
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 63350K .......... .......... .......... .......... .......... 11% 5.81M 46s
 63400K .......... .......... .......... .......... .......... 11% 9.90M 46s
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 63700K .......... .......... .......... .......... .......... 11% 5.06M 46s
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 63850K .......... .......... .......... .......... .......... 11% 5.64M 46s
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 63950K .......... .......... .......... .......... .......... 11% 9.66M 46s
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 64100K .......... .......... .......... .......... .......... 11% 8.78M 46s
 64150K .......... .......... .......... .......... .......... 11% 10.7M 46s
 64200K .......... .......... .......... .......... .......... 11% 7.24M 46s
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 67250K .......... .......... .......... .......... .......... 12% 9.34M 46s
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 68200K .......... .......... .......... .......... .......... 12% 11.7M 46s
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 70250K .......... .......... .......... .......... .......... 13% 64.8M 46s
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 70550K .......... .......... .......... .......... .......... 13% 23.0M 45s
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 72150K .......... .......... .......... .......... .......... 13% 6.78M 45s
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 74250K .......... .......... .......... .......... .......... 13% 25.3M 46s
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 75250K .......... .......... .......... .......... .......... 14% 12.0M 45s
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 76300K .......... .......... .......... .......... .......... 14% 13.3M 45s
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 76800K .......... .......... .......... .......... .......... 14% 13.8M 45s
 76850K .......... .......... .......... .......... .......... 14% 24.7M 45s
 76900K .......... .......... .......... .......... .......... 14% 37.3M 45s
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 77050K .......... .......... .......... .......... .......... 14% 51.9M 45s
 77100K .......... .......... .......... .......... .......... 14% 16.0M 45s
 77150K .......... .......... .......... .......... .......... 14% 46.9M 45s
 77200K .......... .......... .......... .......... .......... 14% 20.6M 45s
 77250K .......... .......... .......... .......... .......... 14% 34.4M 45s
 77300K .......... .......... .......... .......... .......... 14% 25.6M 45s
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 78000K .......... .......... .......... .......... .......... 14% 4.26M 45s
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 78150K .......... .......... .......... .......... .......... 14% 35.9M 45s
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 79350K .......... .......... .......... .......... .......... 14% 37.0M 45s
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 82100K .......... .......... .......... .......... .......... 15% 9.77M 44s
 82150K .......... .......... .......... .......... .......... 15% 10.5M 44s
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 82250K .......... .......... .......... .......... .......... 15% 8.56M 44s
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 89250K .......... .......... .......... .......... .......... 16% 9.59M 43s
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 90050K .......... .......... .......... .......... .......... 16% 11.3M 43s
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 90200K .......... .......... .......... .......... .......... 16% 7.51M 43s
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 90300K .......... .......... .......... .......... .......... 16% 7.76M 43s
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 90550K .......... .......... .......... .......... .......... 16% 2.70M 43s
 90600K .......... .......... .......... .......... .......... 16% 25.2M 43s
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 91000K .......... .......... .......... .......... .......... 16% 11.6M 43s
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 91100K .......... .......... .......... .......... .......... 16% 10.2M 43s
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 91200K .......... .......... .......... .......... .......... 16% 8.13M 43s
 91250K .......... .......... .......... .......... .......... 16% 7.80M 43s
 91300K .......... .......... .......... .......... .......... 16% 8.64M 43s
 91350K .......... .......... .......... .......... .......... 17% 8.74M 43s
 91400K .......... .......... .......... .......... .......... 17% 9.38M 43s
 91450K .......... .......... .......... .......... .......... 17% 5.46M 43s
 91500K .......... .......... .......... .......... .......... 17% 6.31M 43s
 91550K .......... .......... .......... .......... .......... 17% 5.36M 43s
 91600K .......... .......... .......... .......... .......... 17% 4.70M 43s
 91650K .......... .......... .......... .......... .......... 17% 4.71M 43s
 91700K .......... .......... .......... .......... .......... 17% 5.42M 43s
 91750K .......... .......... .......... .......... .......... 17% 5.96M 43s
 91800K .......... .......... .......... .......... .......... 17% 6.30M 43s
 91850K .......... .......... .......... .......... .......... 17% 5.52M 43s
 91900K .......... .......... .......... .......... .......... 17% 7.81M 43s
 91950K .......... .......... .......... .......... .......... 17% 12.1M 43s
 92000K .......... .......... .......... .......... .......... 17% 13.3M 43s
 92050K .......... .......... .......... .......... .......... 17% 12.9M 43s
 92100K .......... .......... .......... .......... .......... 17% 10.7M 43s
 92150K .......... .......... .......... .......... .......... 17% 12.3M 43s
 92200K .......... .......... .......... .......... .......... 17% 11.3M 43s
 92250K .......... .......... .......... .......... .......... 17% 13.2M 43s
 92300K .......... .......... .......... .......... .......... 17% 13.6M 43s
 92350K .......... .......... .......... .......... .......... 17% 10.5M 43s
 92400K .......... .......... .......... .......... .......... 17% 13.7M 43s
 92450K .......... .......... .......... .......... .......... 17% 8.68M 43s
 92500K .......... .......... .......... .......... .......... 17% 6.39M 43s
 92550K .......... .......... .......... .......... .......... 17% 9.43M 43s
 92600K .......... .......... .......... .......... .......... 17% 7.23M 43s
 92650K .......... .......... .......... .......... .......... 17% 6.80M 43s
 92700K .......... .......... .......... .......... .......... 17% 9.07M 43s
 92750K .......... .......... .......... .......... .......... 17% 9.11M 43s
 92800K .......... .......... .......... .......... .......... 17% 6.17M 43s
 92850K .......... .......... .......... .......... .......... 17% 7.11M 43s
 92900K .......... .......... .......... .......... .......... 17% 8.14M 43s
 92950K .......... .......... .......... .......... .......... 17% 7.07M 43s
 93000K .......... .......... .......... .......... .......... 17% 8.53M 43s
 93050K .......... .......... .......... .......... .......... 17% 8.52M 43s
 93100K .......... .......... .......... .......... .......... 17% 9.49M 43s
 93150K .......... .......... .......... .......... .......... 17% 20.8M 43s
 93200K .......... .......... .......... .......... .......... 17% 24.3M 43s
 93250K .......... .......... .......... .......... .......... 17% 23.7M 43s
 93300K .......... .......... .......... .......... .......... 17% 21.2M 43s
 93350K .......... .......... .......... .......... .......... 17% 13.8M 43s
 93400K .......... .......... .......... .......... .......... 17% 14.5M 43s
 93450K .......... .......... .......... .......... .......... 17% 14.1M 43s
 93500K .......... .......... .......... .......... .......... 17% 16.7M 43s
 93550K .......... .......... .......... .......... .......... 17% 14.3M 43s
 93600K .......... .......... .......... .......... .......... 17% 13.7M 43s
 93650K .......... .......... .......... .......... .......... 17% 2.74M 43s
 93700K .......... .......... .......... .......... .......... 17%  107M 43s
 93750K .......... .......... .......... .......... .......... 17%  142M 43s
 93800K .......... .......... .......... .......... .......... 17%  178M 43s
 93850K .......... .......... .......... .......... .......... 17% 26.2M 43s
 93900K .......... .......... .......... .......... .......... 17% 41.6M 43s
 93950K .......... .......... .......... .......... .......... 17% 21.2M 43s
 94000K .......... .......... .......... .......... .......... 17% 23.8M 43s
 94050K .......... .......... .......... .......... .......... 17% 32.5M 43s
 94100K .......... .......... .......... .......... .......... 17% 14.8M 43s
 94150K .......... .......... .......... .......... .......... 17% 16.6M 43s
 94200K .......... .......... .......... .......... .......... 17% 14.1M 43s
 94250K .......... .......... .......... .......... .......... 17% 17.7M 43s
 94300K .......... .......... .......... .......... .......... 17% 19.5M 43s
 94350K .......... .......... .......... .......... .......... 17% 11.7M 43s
 94400K .......... .......... .......... .......... .......... 17% 15.6M 43s
 94450K .......... .......... .......... .......... .......... 17% 11.7M 43s
 94500K .......... .......... .......... .......... .......... 17% 16.7M 43s
 94550K .......... .......... .......... .......... .......... 17% 11.4M 43s
 94600K .......... .......... .......... .......... .......... 17% 12.2M 43s
 94650K .......... .......... .......... .......... .......... 17% 12.9M 43s
 94700K .......... .......... .......... .......... .......... 17% 9.56M 43s
 94750K .......... .......... .......... .......... .......... 17% 9.84M 43s
 94800K .......... .......... .......... .......... .......... 17% 12.5M 43s
 94850K .......... .......... .......... .......... .......... 17% 12.5M 43s
 94900K .......... .......... .......... .......... .......... 17% 13.3M 43s
 94950K .......... .......... .......... .......... .......... 17% 11.8M 43s
 95000K .......... .......... .......... .......... .......... 17% 14.5M 43s
 95050K .......... .......... .......... .......... .......... 17% 15.6M 43s
 95100K .......... .......... .......... .......... .......... 17% 10.3M 43s
 95150K .......... .......... .......... .......... .......... 17% 14.3M 43s
 95200K .......... .......... .......... .......... .......... 17% 19.0M 43s
 95250K .......... .......... .......... .......... .......... 17% 18.6M 43s
 95300K .......... .......... .......... .......... .......... 17% 40.7M 43s
 95350K .......... .......... .......... .......... .......... 17% 18.6M 43s
 95400K .......... .......... .......... .......... .......... 17% 22.5M 43s
 95450K .......... .......... .......... .......... .......... 17% 15.2M 43s
 95500K .......... .......... .......... .......... .......... 17% 16.1M 43s
 95550K .......... .......... .......... .......... .......... 17% 15.4M 43s
 95600K .......... .......... .......... .......... .......... 17% 11.5M 43s
 95650K .......... .......... .......... .......... .......... 17%  382K 43s
 95700K .......... .......... .......... .......... .......... 17%  102M 43s
 95750K .......... .......... .......... .......... .......... 17%  114M 43s
 95800K .......... .......... .......... .......... .......... 17% 36.7M 43s
 95850K .......... .......... .......... .......... .......... 17% 6.23M 43s
 95900K .......... .......... .......... .......... .......... 17% 9.65M 43s
 95950K .......... .......... .......... .......... .......... 17% 11.0M 43s
 96000K .......... .......... .......... .......... .......... 17% 9.45M 43s
 96050K .......... .......... .......... .......... .......... 17% 10.9M 43s
 96100K .......... .......... .......... .......... .......... 17% 11.0M 43s
 96150K .......... .......... .......... .......... .......... 17% 8.38M 43s
 96200K .......... .......... .......... .......... .......... 17% 13.1M 43s
 96250K .......... .......... .......... .......... .......... 17% 13.2M 43s
 96300K .......... .......... .......... .......... .......... 17% 11.4M 43s
 96350K .......... .......... .......... .......... .......... 17% 10.5M 43s
 96400K .......... .......... .......... .......... .......... 17% 14.0M 43s
 96450K .......... .......... .......... .......... .......... 17% 10.9M 43s
 96500K .......... .......... .......... .......... .......... 17% 13.3M 43s
 96550K .......... .......... .......... .......... .......... 17% 11.9M 43s
 96600K .......... .......... .......... .......... .......... 17% 11.1M 43s
 96650K .......... .......... .......... .......... .......... 17% 11.8M 43s
 96700K .......... .......... .......... .......... .......... 18% 18.0M 43s
 96750K .......... .......... .......... .......... .......... 18% 16.0M 43s
 96800K .......... .......... .......... .......... .......... 18%  234M 43s
 96850K .......... .......... .......... .......... .......... 18% 24.0M 43s
 96900K .......... .......... .......... .......... .......... 18% 17.8M 43s
 96950K .......... .......... .......... .......... .......... 18% 10.6M 43s
 97000K .......... .......... .......... .......... .......... 18% 14.5M 43s
 97050K .......... .......... .......... .......... .......... 18% 12.8M 43s
 97100K .......... .......... .......... .......... .......... 18% 3.65M 43s
 97150K .......... .......... .......... .......... .......... 18%  168M 43s
 97200K .......... .......... .......... .......... .......... 18% 27.3M 43s
 97250K .......... .......... .......... .......... .......... 18% 9.66M 43s
 97300K .......... .......... .......... .......... .......... 18% 8.32M 43s
 97350K .......... .......... .......... .......... .......... 18% 9.06M 43s
 97400K .......... .......... .......... .......... .......... 18% 10.3M 43s
 97450K .......... .......... .......... .......... .......... 18% 7.70M 43s
 97500K .......... .......... .......... .......... .......... 18% 9.12M 43s
 97550K .......... .......... .......... .......... .......... 18% 8.64M 43s
 97600K .......... .......... .......... .......... .......... 18% 5.88M 43s
 97650K .......... .......... .......... .......... .......... 18% 8.43M 43s
 97700K .......... .......... .......... .......... .......... 18% 6.73M 43s
 97750K .......... .......... .......... .......... .......... 18% 6.46M 43s
 97800K .......... .......... .......... .......... .......... 18% 6.25M 43s
 97850K .......... .......... .......... .......... .......... 18% 4.92M 43s
 97900K .......... .......... .......... .......... .......... 18% 6.49M 43s
 97950K .......... .......... .......... .......... .......... 18% 7.04M 43s
 98000K .......... .......... .......... .......... .......... 18% 23.7M 43s
 98050K .......... .......... .......... .......... .......... 18% 24.0M 43s
 98100K .......... .......... .......... .......... .......... 18% 23.8M 43s
 98150K .......... .......... .......... .......... .......... 18% 21.4M 43s
 98200K .......... .......... .......... .......... .......... 18% 15.9M 43s
 98250K .......... .......... .......... .......... .......... 18% 16.3M 43s
 98300K .......... .......... .......... .......... .......... 18% 11.9M 43s
 98350K .......... .......... .......... .......... .......... 18% 11.8M 43s
 98400K .......... .......... .......... .......... .......... 18% 16.3M 43s
 98450K .......... .......... .......... .......... .......... 18% 9.13M 43s
 98500K .......... .......... .......... .......... .......... 18% 11.7M 43s
 98550K .......... .......... .......... .......... .......... 18% 11.7M 43s
 98600K .......... .......... .......... .......... .......... 18% 11.4M 43s
 98650K .......... .......... .......... .......... .......... 18% 12.7M 43s
 98700K .......... .......... .......... .......... .......... 18% 10.3M 43s
 98750K .......... .......... .......... .......... .......... 18% 12.8M 43s
 98800K .......... .......... .......... .......... .......... 18% 14.5M 43s
 98850K .......... .......... .......... .......... .......... 18% 12.5M 43s
 98900K .......... .......... .......... .......... .......... 18% 23.7M 43s
 98950K .......... .......... .......... .......... .......... 18% 22.1M 43s
 99000K .......... .......... .......... .......... .......... 18%  110M 43s
 99050K .......... .......... .......... .......... .......... 18% 30.4M 43s
 99100K .......... .......... .......... .......... .......... 18% 15.5M 43s
 99150K .......... .......... .......... .......... .......... 18% 38.8M 43s
 99200K .......... .......... .......... .......... .......... 18% 13.0M 43s
 99250K .......... .......... .......... .......... .......... 18% 15.3M 43s
 99300K .......... .......... .......... .......... .......... 18% 11.6M 43s
 99350K .......... .......... .......... .......... .......... 18% 8.93M 43s
 99400K .......... .......... .......... .......... .......... 18% 8.50M 43s
 99450K .......... .......... .......... .......... .......... 18% 9.33M 43s
 99500K .......... .......... .......... .......... .......... 18% 9.83M 43s
 99550K .......... .......... .......... .......... .......... 18% 9.26M 43s
 99600K .......... .......... .......... .......... .......... 18% 8.14M 43s
 99650K .......... .......... .......... .......... .......... 18% 10.2M 43s
 99700K .......... .......... .......... .......... .......... 18% 13.6M 43s
 99750K .......... .......... .......... .......... .......... 18% 9.23M 43s
 99800K .......... .......... .......... .......... .......... 18%  136M 43s
 99850K .......... .......... .......... .......... .......... 18% 19.9M 43s
 99900K .......... .......... .......... .......... .......... 18% 17.9M 43s
 99950K .......... .......... .......... .......... .......... 18% 13.9M 43s
100000K .......... .......... .......... .......... .......... 18% 21.3M 43s
100050K .......... .......... .......... .......... .......... 18% 16.2M 43s
100100K .......... .......... .......... .......... .......... 18% 14.9M 43s
100150K .......... .......... .......... .......... .......... 18% 19.2M 43s
100200K .......... .......... .......... .......... .......... 18% 16.9M 43s
100250K .......... .......... .......... .......... .......... 18% 18.5M 43s
100300K .......... .......... .......... .......... .......... 18% 17.0M 43s
100350K .......... .......... .......... .......... .......... 18% 11.3M 43s
100400K .......... .......... .......... .......... .......... 18% 15.4M 43s
100450K .......... .......... .......... .......... .......... 18% 12.6M 43s
100500K .......... .......... .......... .......... .......... 18% 12.4M 43s
100550K .......... .......... .......... .......... .......... 18% 11.1M 43s
100600K .......... .......... .......... .......... .......... 18% 10.8M 43s
100650K .......... .......... .......... .......... .......... 18% 10.1M 43s
100700K .......... .......... .......... .......... .......... 18% 10.6M 43s
100750K .......... .......... .......... .......... .......... 18% 11.1M 42s
100800K .......... .......... .......... .......... .......... 18% 9.31M 42s
100850K .......... .......... .......... .......... .......... 18% 11.2M 42s
100900K .......... .......... .......... .......... .......... 18% 11.0M 42s
100950K .......... .......... .......... .......... .......... 18% 9.93M 42s
101000K .......... .......... .......... .......... .......... 18% 10.2M 42s
101050K .......... .......... .......... .......... .......... 18% 9.11M 42s
101100K .......... .......... .......... .......... .......... 18% 6.91M 42s
101150K .......... .......... .......... .......... .......... 18% 7.02M 42s
101200K .......... .......... .......... .......... .......... 18% 8.84M 42s
101250K .......... .......... .......... .......... .......... 18% 9.11M 42s
101300K .......... .......... .......... .......... .......... 18% 9.76M 42s
101350K .......... .......... .......... .......... .......... 18% 7.96M 42s
101400K .......... .......... .......... .......... .......... 18% 8.69M 42s
101450K .......... .......... .......... .......... .......... 18% 11.8M 42s
101500K .......... .......... .......... .......... .......... 18% 38.1M 42s
101550K .......... .......... .......... .......... .......... 18% 32.1M 42s
101600K .......... .......... .......... .......... .......... 18% 19.3M 42s
101650K .......... .......... .......... .......... .......... 18% 29.5M 42s
101700K .......... .......... .......... .......... .......... 18% 19.9M 42s
101750K .......... .......... .......... .......... .......... 18% 15.8M 42s
101800K .......... .......... .......... .......... .......... 18% 27.0M 42s
101850K .......... .......... .......... .......... .......... 18% 12.7M 42s
101900K .......... .......... .......... .......... .......... 18% 15.6M 42s
101950K .......... .......... .......... .......... .......... 18% 14.3M 42s
102000K .......... .......... .......... .......... .......... 18% 15.2M 42s
102050K .......... .......... .......... .......... .......... 18% 15.5M 42s
102100K .......... .......... .......... .......... .......... 19% 11.6M 42s
102150K .......... .......... .......... .......... .......... 19% 11.8M 42s
102200K .......... .......... .......... .......... .......... 19% 10.8M 42s
102250K .......... .......... .......... .......... .......... 19% 11.8M 42s
102300K .......... .......... .......... .......... .......... 19% 11.8M 42s
102350K .......... .......... .......... .......... .......... 19% 7.29M 42s
102400K .......... .......... .......... .......... .......... 19% 6.72M 42s
102450K .......... .......... .......... .......... .......... 19% 8.38M 42s
102500K .......... .......... .......... .......... .......... 19% 11.6M 42s
102550K .......... .......... .......... .......... .......... 19% 10.8M 42s
102600K .......... .......... .......... .......... .......... 19% 9.82M 42s
102650K .......... .......... .......... .......... .......... 19% 12.2M 42s
102700K .......... .......... .......... .......... .......... 19% 10.4M 42s
102750K .......... .......... .......... .......... .......... 19% 12.7M 42s
102800K .......... .......... .......... .......... .......... 19% 15.8M 42s
102850K .......... .......... .......... .......... .......... 19% 97.1M 42s
102900K .......... .......... .......... .......... .......... 19% 26.8M 42s
102950K .......... .......... .......... .......... .......... 19% 17.3M 42s
103000K .......... .......... .......... .......... .......... 19% 17.4M 42s
103050K .......... .......... .......... .......... .......... 19% 18.7M 42s
103100K .......... .......... .......... .......... .......... 19% 14.1M 42s
103150K .......... .......... .......... .......... .......... 19% 13.0M 42s
103200K .......... .......... .......... .......... .......... 19% 10.2M 42s
103250K .......... .......... .......... .......... .......... 19% 16.5M 42s
103300K .......... .......... .......... .......... .......... 19% 17.0M 42s
103350K .......... .......... .......... .......... .......... 19% 10.3M 42s
103400K .......... .......... .......... .......... .......... 19% 17.9M 42s
103450K .......... .......... .......... .......... .......... 19% 8.61M 42s
103500K .......... .......... .......... .......... .......... 19% 10.6M 42s
103550K .......... .......... .......... .......... .......... 19% 7.36M 42s
103600K .......... .......... .......... .......... .......... 19% 5.18M 42s
103650K .......... .......... .......... .......... .......... 19% 10.5M 42s
103700K .......... .......... .......... .......... .......... 19% 9.22M 42s
103750K .......... .......... .......... .......... .......... 19% 11.3M 42s
103800K .......... .......... .......... .......... .......... 19% 9.91M 42s
103850K .......... .......... .......... .......... .......... 19% 8.32M 42s
103900K .......... .......... .......... .......... .......... 19% 12.3M 42s
103950K .......... .......... .......... .......... .......... 19% 8.46M 42s
104000K .......... .......... .......... .......... .......... 19% 24.3M 42s
104050K .......... .......... .......... .......... .......... 19% 39.6M 42s
104100K .......... .......... .......... .......... .......... 19% 40.0M 42s
104150K .......... .......... .......... .......... .......... 19% 44.8M 42s
104200K .......... .......... .......... .......... .......... 19% 19.8M 42s
104250K .......... .......... .......... .......... .......... 19% 25.3M 42s
104300K .......... .......... .......... .......... .......... 19% 34.3M 42s
104350K .......... .......... .......... .......... .......... 19% 17.1M 42s
104400K .......... .......... .......... .......... .......... 19% 20.6M 42s
104450K .......... .......... .......... .......... .......... 19% 21.6M 42s
104500K .......... .......... .......... .......... .......... 19% 24.1M 42s
104550K .......... .......... .......... .......... .......... 19% 17.3M 42s
104600K .......... .......... .......... .......... .......... 19% 22.2M 42s
104650K .......... .......... .......... .......... .......... 19% 17.0M 42s
104700K .......... .......... .......... .......... .......... 19% 17.6M 42s
104750K .......... .......... .......... .......... .......... 19% 22.0M 42s
104800K .......... .......... .......... .......... .......... 19% 24.3M 42s
104850K .......... .......... .......... .......... .......... 19% 15.7M 42s
104900K .......... .......... .......... .......... .......... 19% 18.2M 42s
104950K .......... .......... .......... .......... .......... 19% 16.8M 42s
105000K .......... .......... .......... .......... .......... 19% 19.2M 42s
105050K .......... .......... .......... .......... .......... 19% 22.2M 42s
105100K .......... .......... .......... .......... .......... 19% 14.6M 42s
105150K .......... .......... .......... .......... .......... 19% 16.0M 42s
105200K .......... .......... .......... .......... .......... 19% 11.5M 42s
105250K .......... .......... .......... .......... .......... 19% 13.1M 42s
105300K .......... .......... .......... .......... .......... 19% 10.2M 42s
105350K .......... .......... .......... .......... .......... 19% 11.5M 42s
105400K .......... .......... .......... .......... .......... 19% 10.7M 42s
105450K .......... .......... .......... .......... .......... 19% 13.1M 42s
105500K .......... .......... .......... .......... .......... 19% 14.4M 42s
105550K .......... .......... .......... .......... .......... 19% 13.1M 42s
105600K .......... .......... .......... .......... .......... 19% 10.3M 42s
105650K .......... .......... .......... .......... .......... 19% 11.0M 42s
105700K .......... .......... .......... .......... .......... 19% 8.26M 42s
105750K .......... .......... .......... .......... .......... 19% 8.14M 42s
105800K .......... .......... .......... .......... .......... 19% 8.01M 42s
105850K .......... .......... .......... .......... .......... 19% 6.80M 42s
105900K .......... .......... .......... .......... .......... 19% 13.5M 42s
105950K .......... .......... .......... .......... .......... 19% 10.2M 42s
106000K .......... .......... .......... .......... .......... 19% 12.7M 42s
106050K .......... .......... .......... .......... .......... 19% 10.8M 42s
106100K .......... .......... .......... .......... .......... 19% 11.0M 42s
106150K .......... .......... .......... .......... .......... 19% 12.1M 42s
106200K .......... .......... .......... .......... .......... 19% 8.97M 42s
106250K .......... .......... .......... .......... .......... 19% 11.3M 42s
106300K .......... .......... .......... .......... .......... 19% 6.00M 42s
106350K .......... .......... .......... .......... .......... 19% 3.96M 42s
106400K .......... .......... .......... .......... .......... 19% 8.27M 42s
106450K .......... .......... .......... .......... .......... 19% 7.11M 42s
106500K .......... .......... .......... .......... .......... 19% 8.05M 42s
106550K .......... .......... .......... .......... .......... 19% 9.26M 42s
106600K .......... .......... .......... .......... .......... 19% 5.80M 42s
106650K .......... .......... .......... .......... .......... 19% 7.18M 42s
106700K .......... .......... .......... .......... .......... 19% 5.74M 42s
106750K .......... .......... .......... .......... .......... 19% 7.31M 42s
106800K .......... .......... .......... .......... .......... 19% 8.75M 42s
106850K .......... .......... .......... .......... .......... 19% 6.42M 42s
106900K .......... .......... .......... .......... .......... 19% 4.64M 42s
106950K .......... .......... .......... .......... .......... 19% 10.4M 42s
107000K .......... .......... .......... .......... .......... 19% 11.8M 42s
107050K .......... .......... .......... .......... .......... 19% 8.19M 42s
107100K .......... .......... .......... .......... .......... 19% 8.30M 42s
107150K .......... .......... .......... .......... .......... 19% 11.7M 42s
107200K .......... .......... .......... .......... .......... 19% 28.9M 42s
107250K .......... .......... .......... .......... .......... 19% 33.3M 42s
107300K .......... .......... .......... .......... .......... 19% 22.2M 42s
107350K .......... .......... .......... .......... .......... 19% 22.1M 42s
107400K .......... .......... .......... .......... .......... 19% 42.3M 42s
107450K .......... .......... .......... .......... .......... 20% 19.0M 41s
107500K .......... .......... .......... .......... .......... 20% 24.1M 41s
107550K .......... .......... .......... .......... .......... 20% 16.0M 41s
107600K .......... .......... .......... .......... .......... 20% 20.2M 41s
107650K .......... .......... .......... .......... .......... 20% 13.4M 41s
107700K .......... .......... .......... .......... .......... 20% 11.3M 41s
107750K .......... .......... .......... .......... .......... 20% 12.6M 41s
107800K .......... .......... .......... .......... .......... 20% 9.36M 41s
107850K .......... .......... .......... .......... .......... 20% 8.93M 41s
107900K .......... .......... .......... .......... .......... 20% 7.23M 41s
107950K .......... .......... .......... .......... .......... 20% 11.0M 41s
108000K .......... .......... .......... .......... .......... 20% 9.82M 41s
108050K .......... .......... .......... .......... .......... 20% 10.4M 41s
108100K .......... .......... .......... .......... .......... 20% 6.12M 41s
108150K .......... .......... .......... .......... .......... 20% 11.4M 41s
108200K .......... .......... .......... .......... .......... 20% 8.91M 41s
108250K .......... .......... .......... .......... .......... 20% 12.1M 41s
108300K .......... .......... .......... .......... .......... 20% 11.6M 41s
108350K .......... .......... .......... .......... .......... 20% 9.40M 41s
108400K .......... .......... .......... .......... .......... 20% 9.31M 41s
108450K .......... .......... .......... .......... .......... 20% 9.64M 41s
108500K .......... .......... .......... .......... .......... 20% 11.5M 41s
108550K .......... .......... .......... .......... .......... 20% 11.3M 41s
108600K .......... .......... .......... .......... .......... 20% 9.20M 41s
108650K .......... .......... .......... .......... .......... 20% 10.7M 41s
108700K .......... .......... .......... .......... .......... 20% 8.02M 41s
108750K .......... .......... .......... .......... .......... 20% 8.68M 41s
108800K .......... .......... .......... .......... .......... 20% 6.47M 41s
108850K .......... .......... .......... .......... .......... 20% 7.68M 41s
108900K .......... .......... .......... .......... .......... 20% 10.7M 41s
108950K .......... .......... .......... .......... .......... 20% 7.07M 41s
109000K .......... .......... .......... .......... .......... 20% 9.25M 41s
109050K .......... .......... .......... .......... .......... 20% 7.60M 41s
109100K .......... .......... .......... .......... .......... 20% 8.13M 41s
109150K .......... .......... .......... .......... .......... 20% 11.6M 41s
109200K .......... .......... .......... .......... .......... 20% 7.23M 41s
109250K .......... .......... .......... .......... .......... 20% 6.81M 41s
109300K .......... .......... .......... .......... .......... 20% 5.66M 41s
109350K .......... .......... .......... .......... .......... 20% 4.76M 41s
109400K .......... .......... .......... .......... .......... 20% 8.71M 41s
109450K .......... .......... .......... .......... .......... 20% 7.32M 41s
109500K .......... .......... .......... .......... .......... 20% 11.1M 41s
109550K .......... .......... .......... .......... .......... 20% 9.43M 41s
109600K .......... .......... .......... .......... .......... 20% 11.9M 41s
109650K .......... .......... .......... .......... .......... 20% 10.6M 41s
109700K .......... .......... .......... .......... .......... 20% 11.6M 41s
109750K .......... .......... .......... .......... .......... 20% 10.5M 41s
109800K .......... .......... .......... .......... .......... 20% 8.53M 41s
109850K .......... .......... .......... .......... .......... 20% 9.24M 41s
109900K .......... .......... .......... .......... .......... 20% 9.31M 41s
109950K .......... .......... .......... .......... .......... 20% 6.89M 41s
110000K .......... .......... .......... .......... .......... 20% 8.48M 41s
110050K .......... .......... .......... .......... .......... 20% 9.19M 41s
110100K .......... .......... .......... .......... .......... 20% 12.0M 41s
110150K .......... .......... .......... .......... .......... 20% 27.5M 41s
110200K .......... .......... .......... .......... .......... 20% 43.1M 41s
110250K .......... .......... .......... .......... .......... 20% 30.9M 41s
110300K .......... .......... .......... .......... .......... 20% 52.1M 41s
110350K .......... .......... .......... .......... .......... 20% 24.5M 41s
110400K .......... .......... .......... .......... .......... 20% 21.5M 41s
110450K .......... .......... .......... .......... .......... 20% 22.5M 41s
110500K .......... .......... .......... .......... .......... 20% 22.1M 41s
110550K .......... .......... .......... .......... .......... 20% 31.1M 41s
110600K .......... .......... .......... .......... .......... 20% 21.6M 41s
110650K .......... .......... .......... .......... .......... 20% 18.2M 41s
110700K .......... .......... .......... .......... .......... 20% 20.0M 41s
110750K .......... .......... .......... .......... .......... 20% 21.9M 41s
110800K .......... .......... .......... .......... .......... 20% 18.7M 41s
110850K .......... .......... .......... .......... .......... 20% 18.1M 41s
110900K .......... .......... .......... .......... .......... 20% 19.4M 41s
110950K .......... .......... .......... .......... .......... 20% 15.4M 41s
111000K .......... .......... .......... .......... .......... 20% 22.4M 41s
111050K .......... .......... .......... .......... .......... 20% 22.0M 41s
111100K .......... .......... .......... .......... .......... 20% 10.9M 41s
111150K .......... .......... .......... .......... .......... 20% 20.8M 41s
111200K .......... .......... .......... .......... .......... 20% 12.0M 41s
111250K .......... .......... .......... .......... .......... 20% 16.0M 41s
111300K .......... .......... .......... .......... .......... 20% 13.5M 41s
111350K .......... .......... .......... .......... .......... 20% 9.56M 41s
111400K .......... .......... .......... .......... .......... 20% 8.69M 41s
111450K .......... .......... .......... .......... .......... 20% 6.42M 41s
111500K .......... .......... .......... .......... .......... 20% 8.82M 41s
111550K .......... .......... .......... .......... .......... 20% 9.68M 41s
111600K .......... .......... .......... .......... .......... 20% 8.31M 41s
111650K .......... .......... .......... .......... .......... 20% 8.15M 41s
111700K .......... .......... .......... .......... .......... 20% 8.28M 41s
111750K .......... .......... .......... .......... .......... 20% 20.5M 41s
111800K .......... .......... .......... .......... .......... 20% 24.3M 41s
111850K .......... .......... .......... .......... .......... 20% 12.6M 41s
111900K .......... .......... .......... .......... .......... 20% 36.2M 41s
111950K .......... .......... .......... .......... .......... 20% 15.3M 41s
112000K .......... .......... .......... .......... .......... 20% 13.2M 41s
112050K .......... .......... .......... .......... .......... 20% 16.3M 41s
112100K .......... .......... .......... .......... .......... 20% 15.0M 41s
112150K .......... .......... .......... .......... .......... 20% 16.5M 41s
112200K .......... .......... .......... .......... .......... 20% 16.7M 41s
112250K .......... .......... .......... .......... .......... 20% 14.7M 41s
112300K .......... .......... .......... .......... .......... 20% 14.9M 41s
112350K .......... .......... .......... .......... .......... 20% 14.4M 41s
112400K .......... .......... .......... .......... .......... 20% 15.0M 41s
112450K .......... .......... .......... .......... .......... 20% 31.0M 41s
112500K .......... .......... .......... .......... .......... 20% 27.2M 41s
112550K .......... .......... .......... .......... .......... 20% 69.7M 41s
112600K .......... .......... .......... .......... .......... 20% 22.6M 41s
112650K .......... .......... .......... .......... .......... 20% 74.2M 41s
112700K .......... .......... .......... .......... .......... 20% 18.1M 41s
112750K .......... .......... .......... .......... .......... 20%  122M 41s
112800K .......... .......... .......... .......... .......... 20% 28.8M 41s
112850K .......... .......... .......... .......... .......... 21% 22.8M 41s
112900K .......... .......... .......... .......... .......... 21% 27.2M 41s
112950K .......... .......... .......... .......... .......... 21% 16.6M 41s
113000K .......... .......... .......... .......... .......... 21% 20.1M 41s
113050K .......... .......... .......... .......... .......... 21% 17.7M 41s
113100K .......... .......... .......... .......... .......... 21% 15.9M 41s
113150K .......... .......... .......... .......... .......... 21% 17.9M 41s
113200K .......... .......... .......... .......... .......... 21% 11.8M 41s
113250K .......... .......... .......... .......... .......... 21% 12.0M 41s
113300K .......... .......... .......... .......... .......... 21% 17.1M 41s
113350K .......... .......... .......... .......... .......... 21% 9.76M 41s
113400K .......... .......... .......... .......... .......... 21% 12.9M 41s
113450K .......... .......... .......... .......... .......... 21% 6.32M 41s
113500K .......... .......... .......... .......... .......... 21% 9.16M 41s
113550K .......... .......... .......... .......... .......... 21% 9.39M 41s
113600K .......... .......... .......... .......... .......... 21% 6.67M 41s
113650K .......... .......... .......... .......... .......... 21% 14.7M 41s
113700K .......... .......... .......... .......... .......... 21% 10.1M 41s
113750K .......... .......... .......... .......... .......... 21% 9.15M 41s
113800K .......... .......... .......... .......... .......... 21% 10.3M 41s
113850K .......... .......... .......... .......... .......... 21% 9.84M 41s
113900K .......... .......... .......... .......... .......... 21% 11.1M 41s
113950K .......... .......... .......... .......... .......... 21% 6.76M 41s
114000K .......... .......... .......... .......... .......... 21% 7.39M 41s
114050K .......... .......... .......... .......... .......... 21% 8.55M 41s
114100K .......... .......... .......... .......... .......... 21% 7.07M 41s
114150K .......... .......... .......... .......... .......... 21% 10.4M 41s
114200K .......... .......... .......... .......... .......... 21% 6.05M 41s
114250K .......... .......... .......... .......... .......... 21% 7.68M 41s
114300K .......... .......... .......... .......... .......... 21% 7.17M 41s
114350K .......... .......... .......... .......... .......... 21% 5.31M 41s
114400K .......... .......... .......... .......... .......... 21% 4.77M 41s
114450K .......... .......... .......... .......... .......... 21% 3.56M 41s
114500K .......... .......... .......... .......... .......... 21% 3.50M 41s
114550K .......... .......... .......... .......... .......... 21% 2.60M 41s
114600K .......... .......... .......... .......... .......... 21% 2.06M 41s
114650K .......... .......... .......... .......... .......... 21% 2.92M 41s
114700K .......... .......... .......... .......... .......... 21% 5.78M 41s
114750K .......... .......... .......... .......... .......... 21% 12.1M 41s
114800K .......... .......... .......... .......... .......... 21% 11.4M 41s
114850K .......... .......... .......... .......... .......... 21% 9.58M 41s
114900K .......... .......... .......... .......... .......... 21% 13.1M 41s
114950K .......... .......... .......... .......... .......... 21% 12.2M 41s
115000K .......... .......... .......... .......... .......... 21% 13.1M 41s
115050K .......... .......... .......... .......... .......... 21% 7.59M 41s
115100K .......... .......... .......... .......... .......... 21% 7.14M 41s
115150K .......... .......... .......... .......... .......... 21% 7.42M 41s
115200K .......... .......... .......... .......... .......... 21% 11.6M 41s
115250K .......... .......... .......... .......... .......... 21% 8.63M 41s
115300K .......... .......... .......... .......... .......... 21% 11.0M 41s
115350K .......... .......... .......... .......... .......... 21% 10.3M 41s
115400K .......... .......... .......... .......... .......... 21% 10.2M 41s
115450K .......... .......... .......... .......... .......... 21% 11.5M 41s
115500K .......... .......... .......... .......... .......... 21% 9.18M 41s
115550K .......... .......... .......... .......... .......... 21% 12.1M 41s
115600K .......... .......... .......... .......... .......... 21% 9.90M 41s
115650K .......... .......... .......... .......... .......... 21% 9.56M 41s
115700K .......... .......... .......... .......... .......... 21% 10.3M 41s
115750K .......... .......... .......... .......... .......... 21% 12.5M 41s
115800K .......... .......... .......... .......... .......... 21% 11.3M 41s
115850K .......... .......... .......... .......... .......... 21% 8.84M 41s
115900K .......... .......... .......... .......... .......... 21% 10.4M 41s
115950K .......... .......... .......... .......... .......... 21% 11.1M 41s
116000K .......... .......... .......... .......... .......... 21% 12.0M 41s
116050K .......... .......... .......... .......... .......... 21% 12.3M 41s
116100K .......... .......... .......... .......... .......... 21% 11.0M 41s
116150K .......... .......... .......... .......... .......... 21% 13.2M 41s
116200K .......... .......... .......... .......... .......... 21% 11.2M 41s
116250K .......... .......... .......... .......... .......... 21% 9.50M 41s
116300K .......... .......... .......... .......... .......... 21% 16.3M 41s
116350K .......... .......... .......... .......... .......... 21% 17.8M 41s
116400K .......... .......... .......... .......... .......... 21%  120M 41s
116450K .......... .......... .......... .......... .......... 21% 16.4M 41s
116500K .......... .......... .......... .......... .......... 21% 45.8M 41s
116550K .......... .......... .......... .......... .......... 21% 14.6M 41s
116600K .......... .......... .......... .......... .......... 21% 33.5M 41s
116650K .......... .......... .......... .......... .......... 21% 18.0M 41s
116700K .......... .......... .......... .......... .......... 21% 16.7M 40s
116750K .......... .......... .......... .......... .......... 21% 19.2M 40s
116800K .......... .......... .......... .......... .......... 21% 18.0M 40s
116850K .......... .......... .......... .......... .......... 21% 15.2M 40s
116900K .......... .......... .......... .......... .......... 21% 18.8M 40s
116950K .......... .......... .......... .......... .......... 21% 20.2M 40s
117000K .......... .......... .......... .......... .......... 21% 21.2M 40s
117050K .......... .......... .......... .......... .......... 21% 20.7M 40s
117100K .......... .......... .......... .......... .......... 21% 16.2M 40s
117150K .......... .......... .......... .......... .......... 21% 20.8M 40s
117200K .......... .......... .......... .......... .......... 21% 15.4M 40s
117250K .......... .......... .......... .......... .......... 21% 17.8M 40s
117300K .......... .......... .......... .......... .......... 21% 29.8M 40s
117350K .......... .......... .......... .......... .......... 21% 13.2M 40s
117400K .......... .......... .......... .......... .......... 21% 22.8M 40s
117450K .......... .......... .......... .......... .......... 21% 14.5M 40s
117500K .......... .......... .......... .......... .......... 21% 16.0M 40s
117550K .......... .......... .......... .......... .......... 21% 15.9M 40s
117600K .......... .......... .......... .......... .......... 21% 11.6M 40s
117650K .......... .......... .......... .......... .......... 21% 14.8M 40s
117700K .......... .......... .......... .......... .......... 21% 12.6M 40s
117750K .......... .......... .......... .......... .......... 21% 14.2M 40s
117800K .......... .......... .......... .......... .......... 21% 11.8M 40s
117850K .......... .......... .......... .......... .......... 21% 15.0M 40s
117900K .......... .......... .......... .......... .......... 21% 11.7M 40s
117950K .......... .......... .......... .......... .......... 21% 14.3M 40s
118000K .......... .......... .......... .......... .......... 21% 15.7M 40s
118050K .......... .......... .......... .......... .......... 21% 14.6M 40s
118100K .......... .......... .......... .......... .......... 21% 9.14M 40s
118150K .......... .......... .......... .......... .......... 21% 11.4M 40s
118200K .......... .......... .......... .......... .......... 22% 9.01M 40s
118250K .......... .......... .......... .......... .......... 22% 12.4M 40s
118300K .......... .......... .......... .......... .......... 22% 10.9M 40s
118350K .......... .......... .......... .......... .......... 22% 6.37M 40s
118400K .......... .......... .......... .......... .......... 22% 10.8M 40s
118450K .......... .......... .......... .......... .......... 22% 6.29M 40s
118500K .......... .......... .......... .......... .......... 22% 6.58M 40s
118550K .......... .......... .......... .......... .......... 22% 6.74M 40s
118600K .......... .......... .......... .......... .......... 22% 5.75M 40s
118650K .......... .......... .......... .......... .......... 22% 6.49M 40s
118700K .......... .......... .......... .......... .......... 22% 14.8M 40s
118750K .......... .......... .......... .......... .......... 22% 36.0M 40s
118800K .......... .......... .......... .......... .......... 22% 25.8M 40s
118850K .......... .......... .......... .......... .......... 22% 32.4M 40s
118900K .......... .......... .......... .......... .......... 22% 29.9M 40s
118950K .......... .......... .......... .......... .......... 22% 28.7M 40s
119000K .......... .......... .......... .......... .......... 22% 32.7M 40s
119050K .......... .......... .......... .......... .......... 22% 37.4M 40s
119100K .......... .......... .......... .......... .......... 22% 24.0M 40s
119150K .......... .......... .......... .......... .......... 22% 33.9M 40s
119200K .......... .......... .......... .......... .......... 22% 31.3M 40s
119250K .......... .......... .......... .......... .......... 22% 27.1M 40s
119300K .......... .......... .......... .......... .......... 22% 28.8M 40s
119350K .......... .......... .......... .......... .......... 22% 17.8M 40s
119400K .......... .......... .......... .......... .......... 22% 15.5M 40s
119450K .......... .......... .......... .......... .......... 22% 12.5M 40s
119500K .......... .......... .......... .......... .......... 22% 19.5M 40s
119550K .......... .......... .......... .......... .......... 22% 12.3M 40s
119600K .......... .......... .......... .......... .......... 22% 12.2M 40s
119650K .......... .......... .......... .......... .......... 22% 15.5M 40s
119700K .......... .......... .......... .......... .......... 22% 14.3M 40s
119750K .......... .......... .......... .......... .......... 22% 14.6M 40s
119800K .......... .......... .......... .......... .......... 22% 17.7M 40s
119850K .......... .......... .......... .......... .......... 22% 9.98M 40s
119900K .......... .......... .......... .......... .......... 22% 22.0M 40s
119950K .......... .......... .......... .......... .......... 22% 10.5M 40s
120000K .......... .......... .......... .......... .......... 22% 13.5M 40s
120050K .......... .......... .......... .......... .......... 22% 13.8M 40s
120100K .......... .......... .......... .......... .......... 22% 10.8M 40s
120150K .......... .......... .......... .......... .......... 22% 13.0M 40s
120200K .......... .......... .......... .......... .......... 22% 11.7M 40s
120250K .......... .......... .......... .......... .......... 22% 9.18M 40s
120300K .......... .......... .......... .......... .......... 22% 15.1M 40s
120350K .......... .......... .......... .......... .......... 22% 10.5M 40s
120400K .......... .......... .......... .......... .......... 22% 12.6M 40s
120450K .......... .......... .......... .......... .......... 22% 11.8M 40s
120500K .......... .......... .......... .......... .......... 22% 11.1M 40s
120550K .......... .......... .......... .......... .......... 22% 15.0M 40s
120600K .......... .......... .......... .......... .......... 22% 10.8M 40s
120650K .......... .......... .......... .......... .......... 22% 11.2M 40s
120700K .......... .......... .......... .......... .......... 22% 12.6M 40s
120750K .......... .......... .......... .......... .......... 22% 34.9M 40s
120800K .......... .......... .......... .......... .......... 22% 41.6M 40s
120850K .......... .......... .......... .......... .......... 22% 32.4M 40s
120900K .......... .......... .......... .......... .......... 22% 20.5M 40s
120950K .......... .......... .......... .......... .......... 22% 84.9M 40s
121000K .......... .......... .......... .......... .......... 22% 26.6M 40s
121050K .......... .......... .......... .......... .......... 22% 40.3M 40s
121100K .......... .......... .......... .......... .......... 22% 17.0M 40s
121150K .......... .......... .......... .......... .......... 22% 20.3M 40s
121200K .......... .......... .......... .......... .......... 22% 19.8M 40s
121250K .......... .......... .......... .......... .......... 22% 18.9M 40s
121300K .......... .......... .......... .......... .......... 22% 14.4M 40s
121350K .......... .......... .......... .......... .......... 22% 21.1M 40s
121400K .......... .......... .......... .......... .......... 22% 21.4M 40s
121450K .......... .......... .......... .......... .......... 22% 15.4M 40s
121500K .......... .......... .......... .......... .......... 22% 13.9M 40s
121550K .......... .......... .......... .......... .......... 22% 14.8M 40s
121600K .......... .......... .......... .......... .......... 22% 13.6M 40s
121650K .......... .......... .......... .......... .......... 22% 17.2M 40s
121700K .......... .......... .......... .......... .......... 22% 13.5M 40s
121750K .......... .......... .......... .......... .......... 22% 14.5M 40s
121800K .......... .......... .......... .......... .......... 22% 16.5M 39s
121850K .......... .......... .......... .......... .......... 22% 10.5M 39s
121900K .......... .......... .......... .......... .......... 22% 16.4M 39s
121950K .......... .......... .......... .......... .......... 22% 12.4M 39s
122000K .......... .......... .......... .......... .......... 22% 11.2M 39s
122050K .......... .......... .......... .......... .......... 22% 11.7M 39s
122100K .......... .......... .......... .......... .......... 22% 9.75M 39s
122150K .......... .......... .......... .......... .......... 22% 8.89M 39s
122200K .......... .......... .......... .......... .......... 22% 6.82M 39s
122250K .......... .......... .......... .......... .......... 22% 6.26M 39s
122300K .......... .......... .......... .......... .......... 22% 8.80M 39s
122350K .......... .......... .......... .......... .......... 22% 6.06M 39s
122400K .......... .......... .......... .......... .......... 22% 6.32M 39s
122450K .......... .......... .......... .......... .......... 22% 6.60M 39s
122500K .......... .......... .......... .......... .......... 22% 8.37M 39s
122550K .......... .......... .......... .......... .......... 22% 8.27M 39s
122600K .......... .......... .......... .......... .......... 22% 6.92M 39s
122650K .......... .......... .......... .......... .......... 22% 9.40M 39s
122700K .......... .......... .......... .......... .......... 22% 20.8M 39s
122750K .......... .......... .......... .......... .......... 22% 22.4M 39s
122800K .......... .......... .......... .......... .......... 22% 14.6M 39s
122850K .......... .......... .......... .......... .......... 22% 29.1M 39s
122900K .......... .......... .......... .......... .......... 22% 14.0M 39s
122950K .......... .......... .......... .......... .......... 22% 9.98M 39s
123000K .......... .......... .......... .......... .......... 22% 15.4M 39s
123050K .......... .......... .......... .......... .......... 22% 11.9M 39s
123100K .......... .......... .......... .......... .......... 22% 10.3M 39s
123150K .......... .......... .......... .......... .......... 22% 11.7M 39s
123200K .......... .......... .......... .......... .......... 22% 8.92M 39s
123250K .......... .......... .......... .......... .......... 22% 11.1M 39s
123300K .......... .......... .......... .......... .......... 22% 12.2M 39s
123350K .......... .......... .......... .......... .......... 22% 8.93M 39s
123400K .......... .......... .......... .......... .......... 22% 12.3M 39s
123450K .......... .......... .......... .......... .......... 22% 11.1M 39s
123500K .......... .......... .......... .......... .......... 22% 11.4M 39s
123550K .......... .......... .......... .......... .......... 22% 13.6M 39s
123600K .......... .......... .......... .......... .......... 23% 9.29M 39s
123650K .......... .......... .......... .......... .......... 23% 10.8M 39s
123700K .......... .......... .......... .......... .......... 23% 8.41M 39s
123750K .......... .......... .......... .......... .......... 23% 8.94M 39s
123800K .......... .......... .......... .......... .......... 23% 7.71M 39s
123850K .......... .......... .......... .......... .......... 23% 5.49M 39s
123900K .......... .......... .......... .......... .......... 23% 7.55M 39s
123950K .......... .......... .......... .......... .......... 23% 5.53M 39s
124000K .......... .......... .......... .......... .......... 23% 6.74M 39s
124050K .......... .......... .......... .......... .......... 23% 12.3M 39s
124100K .......... .......... .......... .......... .......... 23% 17.6M 39s
124150K .......... .......... .......... .......... .......... 23% 43.0M 39s
124200K .......... .......... .......... .......... .......... 23% 15.2M 39s
124250K .......... .......... .......... .......... .......... 23% 21.5M 39s
124300K .......... .......... .......... .......... .......... 23% 20.0M 39s
124350K .......... .......... .......... .......... .......... 23% 16.9M 39s
124400K .......... .......... .......... .......... .......... 23% 21.5M 39s
124450K .......... .......... .......... .......... .......... 23% 14.3M 39s
124500K .......... .......... .......... .......... .......... 23% 21.5M 39s
124550K .......... .......... .......... .......... .......... 23% 21.9M 39s
124600K .......... .......... .......... .......... .......... 23% 15.3M 39s
124650K .......... .......... .......... .......... .......... 23% 22.6M 39s
124700K .......... .......... .......... .......... .......... 23% 16.5M 39s
124750K .......... .......... .......... .......... .......... 23% 22.4M 39s
124800K .......... .......... .......... .......... .......... 23% 17.5M 39s
124850K .......... .......... .......... .......... .......... 23% 23.9M 39s
124900K .......... .......... .......... .......... .......... 23% 15.8M 39s
124950K .......... .......... .......... .......... .......... 23% 26.5M 39s
125000K .......... .......... .......... .......... .......... 23% 21.8M 39s
125050K .......... .......... .......... .......... .......... 23% 21.0M 39s
125100K .......... .......... .......... .......... .......... 23% 21.1M 39s
125150K .......... .......... .......... .......... .......... 23% 17.7M 39s
125200K .......... .......... .......... .......... .......... 23% 32.2M 39s
125250K .......... .......... .......... .......... .......... 23% 22.8M 39s
125300K .......... .......... .......... .......... .......... 23% 23.2M 39s
125350K .......... .......... .......... .......... .......... 23% 14.1M 39s
125400K .......... .......... .......... .......... .......... 23% 55.0M 39s
125450K .......... .......... .......... .......... .......... 23% 18.4M 39s
125500K .......... .......... .......... .......... .......... 23% 25.1M 39s
125550K .......... .......... .......... .......... .......... 23% 21.3M 39s
125600K .......... .......... .......... .......... .......... 23% 16.8M 39s
125650K .......... .......... .......... .......... .......... 23% 17.7M 39s
125700K .......... .......... .......... .......... .......... 23% 17.5M 39s
125750K .......... .......... .......... .......... .......... 23% 16.8M 39s
125800K .......... .......... .......... .......... .......... 23% 17.0M 39s
125850K .......... .......... .......... .......... .......... 23% 11.2M 39s
125900K .......... .......... .......... .......... .......... 23% 7.26M 39s
125950K .......... .......... .......... .......... .......... 23% 8.79M 39s
126000K .......... .......... .......... .......... .......... 23% 9.31M 39s
126050K .......... .......... .......... .......... .......... 23% 9.82M 39s
126100K .......... .......... .......... .......... .......... 23% 9.39M 39s
126150K .......... .......... .......... .......... .......... 23% 10.9M 39s
126200K .......... .......... .......... .......... .......... 23% 9.55M 39s
126250K .......... .......... .......... .......... .......... 23% 7.33M 39s
126300K .......... .......... .......... .......... .......... 23% 8.38M 39s
126350K .......... .......... .......... .......... .......... 23% 7.00M 39s
126400K .......... .......... .......... .......... .......... 23% 6.12M 39s
126450K .......... .......... .......... .......... .......... 23% 5.74M 39s
126500K .......... .......... .......... .......... .......... 23% 8.61M 39s
126550K .......... .......... .......... .......... .......... 23% 15.2M 39s
126600K .......... .......... .......... .......... .......... 23% 13.8M 39s
126650K .......... .......... .......... .......... .......... 23% 16.4M 39s
126700K .......... .......... .......... .......... .......... 23% 12.1M 39s
126750K .......... .......... .......... .......... .......... 23% 8.46M 39s
126800K .......... .......... .......... .......... .......... 23% 6.71M 39s
126850K .......... .......... .......... .......... .......... 23% 4.44M 39s
126900K .......... .......... .......... .......... .......... 23% 14.9M 39s
126950K .......... .......... .......... .......... .......... 23% 12.2M 39s
127000K .......... .......... .......... .......... .......... 23% 16.0M 39s
127050K .......... .......... .......... .......... .......... 23% 13.5M 39s
127100K .......... .......... .......... .......... .......... 23% 8.91M 39s
127150K .......... .......... .......... .......... .......... 23% 15.5M 39s
127200K .......... .......... .......... .......... .......... 23% 12.9M 39s
127250K .......... .......... .......... .......... .......... 23% 10.3M 39s
127300K .......... .......... .......... .......... .......... 23% 6.39M 39s
127350K .......... .......... .......... .......... .......... 23% 14.7M 39s
127400K .......... .......... .......... .......... .......... 23% 14.4M 39s
127450K .......... .......... .......... .......... .......... 23% 9.83M 39s
127500K .......... .......... .......... .......... .......... 23% 13.4M 39s
127550K .......... .......... .......... .......... .......... 23% 14.3M 39s
127600K .......... .......... .......... .......... .......... 23% 12.7M 39s
127650K .......... .......... .......... .......... .......... 23% 13.4M 39s
127700K .......... .......... .......... .......... .......... 23% 13.0M 39s
127750K .......... .......... .......... .......... .......... 23% 14.6M 39s
127800K .......... .......... .......... .......... .......... 23% 17.6M 39s
127850K .......... .......... .......... .......... .......... 23% 25.1M 39s
127900K .......... .......... .......... .......... .......... 23% 46.9M 39s
127950K .......... .......... .......... .......... .......... 23% 29.5M 39s
128000K .......... .......... .......... .......... .......... 23% 44.7M 39s
128050K .......... .......... .......... .......... .......... 23%  140M 39s
128100K .......... .......... .......... .......... .......... 23% 17.5M 39s
128150K .......... .......... .......... .......... .......... 23% 57.9M 39s
128200K .......... .......... .......... .......... .......... 23% 18.1M 39s
128250K .......... .......... .......... .......... .......... 23% 21.7M 39s
128300K .......... .......... .......... .......... .......... 23% 22.1M 39s
128350K .......... .......... .......... .......... .......... 23% 16.4M 39s
128400K .......... .......... .......... .......... .......... 23% 14.3M 39s
128450K .......... .......... .......... .......... .......... 23% 20.0M 39s
128500K .......... .......... .......... .......... .......... 23% 12.9M 39s
128550K .......... .......... .......... .......... .......... 23% 23.3M 39s
128600K .......... .......... .......... .......... .......... 23% 15.0M 39s
128650K .......... .......... .......... .......... .......... 23% 20.6M 39s
128700K .......... .......... .......... .......... .......... 23% 16.4M 39s
128750K .......... .......... .......... .......... .......... 23% 16.4M 38s
128800K .......... .......... .......... .......... .......... 23% 13.2M 38s
128850K .......... .......... .......... .......... .......... 23% 10.7M 38s
128900K .......... .......... .......... .......... .......... 23% 11.5M 38s
128950K .......... .......... .......... .......... .......... 24% 10.1M 38s
129000K .......... .......... .......... .......... .......... 24% 12.7M 38s
129050K .......... .......... .......... .......... .......... 24% 6.21M 38s
129100K .......... .......... .......... .......... .......... 24% 5.26M 38s
129150K .......... .......... .......... .......... .......... 24% 7.05M 38s
129200K .......... .......... .......... .......... .......... 24% 5.50M 38s
129250K .......... .......... .......... .......... .......... 24% 6.80M 38s
129300K .......... .......... .......... .......... .......... 24% 6.95M 38s
129350K .......... .......... .......... .......... .......... 24% 7.84M 38s
129400K .......... .......... .......... .......... .......... 24% 7.12M 39s
129450K .......... .......... .......... .......... .......... 24% 8.03M 39s
129500K .......... .......... .......... .......... .......... 24% 9.34M 38s
129550K .......... .......... .......... .......... .......... 24% 8.16M 38s
129600K .......... .......... .......... .......... .......... 24% 12.8M 38s
129650K .......... .......... .......... .......... .......... 24% 19.5M 38s
129700K .......... .......... .......... .......... .......... 24% 23.2M 38s
129750K .......... .......... .......... .......... .......... 24% 42.9M 38s
129800K .......... .......... .......... .......... .......... 24% 19.4M 38s
129850K .......... .......... .......... .......... .......... 24% 20.2M 38s
129900K .......... .......... .......... .......... .......... 24% 15.2M 38s
129950K .......... .......... .......... .......... .......... 24% 21.6M 38s
130000K .......... .......... .......... .......... .......... 24% 19.1M 38s
130050K .......... .......... .......... .......... .......... 24% 15.5M 38s
130100K .......... .......... .......... .......... .......... 24% 7.12M 38s
130150K .......... .......... .......... .......... .......... 24% 7.38M 38s
130200K .......... .......... .......... .......... .......... 24% 4.60M 38s
130250K .......... .......... .......... .......... .......... 24% 6.07M 38s
130300K .......... .......... .......... .......... .......... 24% 12.3M 38s
130350K .......... .......... .......... .......... .......... 24% 8.79M 38s
130400K .......... .......... .......... .......... .......... 24% 12.2M 38s
130450K .......... .......... .......... .......... .......... 24% 8.09M 38s
130500K .......... .......... .......... .......... .......... 24% 7.32M 38s
130550K .......... .......... .......... .......... .......... 24% 11.4M 38s
130600K .......... .......... .......... .......... .......... 24% 9.43M 38s
130650K .......... .......... .......... .......... .......... 24% 7.11M 38s
130700K .......... .......... .......... .......... .......... 24% 7.27M 38s
130750K .......... .......... .......... .......... .......... 24% 7.43M 38s
130800K .......... .......... .......... .......... .......... 24% 7.86M 38s
130850K .......... .......... .......... .......... .......... 24% 6.44M 38s
130900K .......... .......... .......... .......... .......... 24% 4.20M 38s
130950K .......... .......... .......... .......... .......... 24% 9.80M 38s
131000K .......... .......... .......... .......... .......... 24% 13.6M 38s
131050K .......... .......... .......... .......... .......... 24% 10.5M 38s
131100K .......... .......... .......... .......... .......... 24% 9.94M 38s
131150K .......... .......... .......... .......... .......... 24% 11.6M 38s
131200K .......... .......... .......... .......... .......... 24% 9.84M 38s
131250K .......... .......... .......... .......... .......... 24% 11.6M 38s
131300K .......... .......... .......... .......... .......... 24% 14.2M 38s
131350K .......... .......... .......... .......... .......... 24% 9.04M 38s
131400K .......... .......... .......... .......... .......... 24% 12.4M 38s
131450K .......... .......... .......... .......... .......... 24% 8.51M 38s
131500K .......... .......... .......... .......... .......... 24% 9.19M 38s
131550K .......... .......... .......... .......... .......... 24% 34.0M 38s
131600K .......... .......... .......... .......... .......... 24% 13.6M 38s
131650K .......... .......... .......... .......... .......... 24% 10.6M 38s
131700K .......... .......... .......... .......... .......... 24% 8.27M 38s
131750K .......... .......... .......... .......... .......... 24% 11.7M 38s
131800K .......... .......... .......... .......... .......... 24% 11.2M 38s
131850K .......... .......... .......... .......... .......... 24% 8.01M 38s
131900K .......... .......... .......... .......... .......... 24% 10.0M 38s
131950K .......... .......... .......... .......... .......... 24% 9.11M 38s
132000K .......... .......... .......... .......... .......... 24% 11.2M 38s
132050K .......... .......... .......... .......... .......... 24% 14.2M 38s
132100K .......... .......... .......... .......... .......... 24% 10.8M 38s
132150K .......... .......... .......... .......... .......... 24% 11.9M 38s
132200K .......... .......... .......... .......... .......... 24% 9.91M 38s
132250K .......... .......... .......... .......... .......... 24% 10.9M 38s
132300K .......... .......... .......... .......... .......... 24% 13.0M 38s
132350K .......... .......... .......... .......... .......... 24% 12.6M 38s
132400K .......... .......... .......... .......... .......... 24% 30.1M 38s
132450K .......... .......... .......... .......... .......... 24% 23.7M 38s
132500K .......... .......... .......... .......... .......... 24% 18.9M 38s
132550K .......... .......... .......... .......... .......... 24% 21.0M 38s
132600K .......... .......... .......... .......... .......... 24% 19.0M 38s
132650K .......... .......... .......... .......... .......... 24% 14.5M 38s
132700K .......... .......... .......... .......... .......... 24% 11.5M 38s
132750K .......... .......... .......... .......... .......... 24% 12.1M 38s
132800K .......... .......... .......... .......... .......... 24% 14.1M 38s
132850K .......... .......... .......... .......... .......... 24% 12.3M 38s
132900K .......... .......... .......... .......... .......... 24% 10.9M 38s
132950K .......... .......... .......... .......... .......... 24% 11.7M 38s
133000K .......... .......... .......... .......... .......... 24% 10.8M 38s
133050K .......... .......... .......... .......... .......... 24% 12.3M 38s
133100K .......... .......... .......... .......... .......... 24% 8.35M 38s
133150K .......... .......... .......... .......... .......... 24% 8.26M 38s
133200K .......... .......... .......... .......... .......... 24% 9.37M 38s
133250K .......... .......... .......... .......... .......... 24% 10.1M 38s
133300K .......... .......... .......... .......... .......... 24% 8.40M 38s
133350K .......... .......... .......... .......... .......... 24% 6.61M 38s
133400K .......... .......... .......... .......... .......... 24% 8.08M 38s
133450K .......... .......... .......... .......... .......... 24% 7.93M 38s
133500K .......... .......... .......... .......... .......... 24% 10.0M 38s
133550K .......... .......... .......... .......... .......... 24% 10.1M 38s
133600K .......... .......... .......... .......... .......... 24% 8.27M 38s
133650K .......... .......... .......... .......... .......... 24% 12.4M 38s
133700K .......... .......... .......... .......... .......... 24% 22.0M 38s
133750K .......... .......... .......... .......... .......... 24% 21.0M 38s
133800K .......... .......... .......... .......... .......... 24% 23.4M 38s
133850K .......... .......... .......... .......... .......... 24% 88.3M 38s
133900K .......... .......... .......... .......... .......... 24% 27.0M 38s
133950K .......... .......... .......... .......... .......... 24% 21.8M 38s
134000K .......... .......... .......... .......... .......... 24% 27.8M 38s
134050K .......... .......... .......... .......... .......... 24% 40.4M 38s
134100K .......... .......... .......... .......... .......... 24% 27.2M 38s
134150K .......... .......... .......... .......... .......... 24% 26.2M 38s
134200K .......... .......... .......... .......... .......... 24% 20.5M 38s
134250K .......... .......... .......... .......... .......... 24% 37.9M 38s
134300K .......... .......... .......... .......... .......... 25% 25.6M 38s
134350K .......... .......... .......... .......... .......... 25% 25.5M 38s
134400K .......... .......... .......... .......... .......... 25% 39.0M 38s
134450K .......... .......... .......... .......... .......... 25% 25.1M 38s
134500K .......... .......... .......... .......... .......... 25% 25.9M 38s
134550K .......... .......... .......... .......... .......... 25% 25.4M 38s
134600K .......... .......... .......... .......... .......... 25% 32.7M 38s
134650K .......... .......... .......... .......... .......... 25% 25.1M 38s
134700K .......... .......... .......... .......... .......... 25% 25.9M 38s
134750K .......... .......... .......... .......... .......... 25% 32.6M 38s
134800K .......... .......... .......... .......... .......... 25% 36.4M 38s
134850K .......... .......... .......... .......... .......... 25% 24.1M 38s
134900K .......... .......... .......... .......... .......... 25% 40.8M 38s
134950K .......... .......... .......... .......... .......... 25% 46.4M 38s
135000K .......... .......... .......... .......... .......... 25% 22.7M 38s
135050K .......... .......... .......... .......... .......... 25% 70.2M 38s
135100K .......... .......... .......... .......... .......... 25%  163M 38s
135150K .......... .......... .......... .......... .......... 25% 62.9M 38s
135200K .......... .......... .......... .......... .......... 25%  122M 38s
135250K .......... .......... .......... .......... .......... 25% 49.0M 38s
135300K .......... .......... .......... .......... .......... 25% 21.8M 38s
135350K .......... .......... .......... .......... .......... 25% 19.1M 38s
135400K .......... .......... .......... .......... .......... 25%  114M 38s
135450K .......... .......... .......... .......... .......... 25% 22.2M 38s
135500K .......... .......... .......... .......... .......... 25% 24.3M 38s
135550K .......... .......... .......... .......... .......... 25% 22.8M 38s
135600K .......... .......... .......... .......... .......... 25% 15.6M 38s
135650K .......... .......... .......... .......... .......... 25% 17.2M 38s
135700K .......... .......... .......... .......... .......... 25% 17.5M 38s
135750K .......... .......... .......... .......... .......... 25% 14.5M 38s
135800K .......... .......... .......... .......... .......... 25% 14.7M 38s
135850K .......... .......... .......... .......... .......... 25% 13.2M 38s
135900K .......... .......... .......... .......... .......... 25% 13.2M 38s
135950K .......... .......... .......... .......... .......... 25% 8.29M 38s
136000K .......... .......... .......... .......... .......... 25% 6.77M 38s
136050K .......... .......... .......... .......... .......... 25% 10.1M 38s
136100K .......... .......... .......... .......... .......... 25% 6.84M 38s
136150K .......... .......... .......... .......... .......... 25% 7.31M 38s
136200K .......... .......... .......... .......... .......... 25% 6.88M 38s
136250K .......... .......... .......... .......... .......... 25% 8.17M 38s
136300K .......... .......... .......... .......... .......... 25% 6.36M 38s
136350K .......... .......... .......... .......... .......... 25% 8.64M 38s
136400K .......... .......... .......... .......... .......... 25% 8.56M 38s
136450K .......... .......... .......... .......... .......... 25% 6.96M 38s
136500K .......... .......... .......... .......... .......... 25% 8.86M 38s
136550K .......... .......... .......... .......... .......... 25% 5.34M 38s
136600K .......... .......... .......... .......... .......... 25% 3.58M 38s
136650K .......... .......... .......... .......... .......... 25% 5.15M 38s
136700K .......... .......... .......... .......... .......... 25% 4.57M 38s
136750K .......... .......... .......... .......... .......... 25% 4.75M 38s
136800K .......... .......... .......... .......... .......... 25% 5.73M 38s
136850K .......... .......... .......... .......... .......... 25% 4.38M 38s
136900K .......... .......... .......... .......... .......... 25% 5.72M 38s
136950K .......... .......... .......... .......... .......... 25% 8.74M 38s
137000K .......... .......... .......... .......... .......... 25% 36.5M 38s
137050K .......... .......... .......... .......... .......... 25% 12.6M 38s
137100K .......... .......... .......... .......... .......... 25% 10.7M 38s
137150K .......... .......... .......... .......... .......... 25% 11.2M 38s
137200K .......... .......... .......... .......... .......... 25% 10.2M 38s
137250K .......... .......... .......... .......... .......... 25% 9.41M 38s
137300K .......... .......... .......... .......... .......... 25% 10.4M 38s
137350K .......... .......... .......... .......... .......... 25% 8.86M 38s
137400K .......... .......... .......... .......... .......... 25% 9.38M 38s
137450K .......... .......... .......... .......... .......... 25% 8.72M 38s
137500K .......... .......... .......... .......... .......... 25% 8.90M 38s
137550K .......... .......... .......... .......... .......... 25% 9.31M 38s
137600K .......... .......... .......... .......... .......... 25% 10.4M 38s
137650K .......... .......... .......... .......... .......... 25% 30.8M 38s
137700K .......... .......... .......... .......... .......... 25% 15.4M 38s
137750K .......... .......... .......... .......... .......... 25% 25.6M 38s
137800K .......... .......... .......... .......... .......... 25% 32.3M 37s
137850K .......... .......... .......... .......... .......... 25% 17.5M 37s
137900K .......... .......... .......... .......... .......... 25% 15.3M 37s
137950K .......... .......... .......... .......... .......... 25% 10.3M 37s
138000K .......... .......... .......... .......... .......... 25% 12.8M 37s
138050K .......... .......... .......... .......... .......... 25% 7.40M 37s
138100K .......... .......... .......... .......... .......... 25% 8.11M 37s
138150K .......... .......... .......... .......... .......... 25% 7.65M 37s
138200K .......... .......... .......... .......... .......... 25% 8.12M 37s
138250K .......... .......... .......... .......... .......... 25% 7.52M 37s
138300K .......... .......... .......... .......... .......... 25% 19.1M 37s
138350K .......... .......... .......... .......... .......... 25% 20.9M 37s
138400K .......... .......... .......... .......... .......... 25% 44.7M 37s
138450K .......... .......... .......... .......... .......... 25% 37.5M 37s
138500K .......... .......... .......... .......... .......... 25% 28.8M 37s
138550K .......... .......... .......... .......... .......... 25% 19.9M 37s
138600K .......... .......... .......... .......... .......... 25% 49.6M 37s
138650K .......... .......... .......... .......... .......... 25% 19.5M 37s
138700K .......... .......... .......... .......... .......... 25% 16.5M 37s
138750K .......... .......... .......... .......... .......... 25% 21.6M 37s
138800K .......... .......... .......... .......... .......... 25% 17.7M 37s
138850K .......... .......... .......... .......... .......... 25% 10.8M 37s
138900K .......... .......... .......... .......... .......... 25% 20.9M 37s
138950K .......... .......... .......... .......... .......... 25% 12.6M 37s
139000K .......... .......... .......... .......... .......... 25% 15.2M 37s
139050K .......... .......... .......... .......... .......... 25% 20.4M 37s
139100K .......... .......... .......... .......... .......... 25% 9.64M 37s
139150K .......... .......... .......... .......... .......... 25% 12.9M 37s
139200K .......... .......... .......... .......... .......... 25% 11.5M 37s
139250K .......... .......... .......... .......... .......... 25% 13.2M 37s
139300K .......... .......... .......... .......... .......... 25% 15.0M 37s
139350K .......... .......... .......... .......... .......... 25% 11.8M 37s
139400K .......... .......... .......... .......... .......... 25% 15.4M 37s
139450K .......... .......... .......... .......... .......... 25% 13.8M 37s
139500K .......... .......... .......... .......... .......... 25% 12.5M 37s
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139600K .......... .......... .......... .......... .......... 25% 14.8M 37s
139650K .......... .......... .......... .......... .......... 25% 17.0M 37s
139700K .......... .......... .......... .......... .......... 26% 9.25M 37s
139750K .......... .......... .......... .......... .......... 26% 21.9M 37s
139800K .......... .......... .......... .......... .......... 26% 15.4M 37s
139850K .......... .......... .......... .......... .......... 26% 11.0M 37s
139900K .......... .......... .......... .......... .......... 26% 11.3M 37s
139950K .......... .......... .......... .......... .......... 26% 8.95M 37s
140000K .......... .......... .......... .......... .......... 26% 11.0M 37s
140050K .......... .......... .......... .......... .......... 26% 9.01M 37s
140100K .......... .......... .......... .......... .......... 26% 7.92M 37s
140150K .......... .......... .......... .......... .......... 26% 8.75M 37s
140200K .......... .......... .......... .......... .......... 26% 8.28M 37s
140250K .......... .......... .......... .......... .......... 26% 9.48M 37s
140300K .......... .......... .......... .......... .......... 26% 8.92M 37s
140350K .......... .......... .......... .......... .......... 26% 6.81M 37s
140400K .......... .......... .......... .......... .......... 26% 9.11M 37s
140450K .......... .......... .......... .......... .......... 26% 7.64M 37s
140500K .......... .......... .......... .......... .......... 26% 13.6M 37s
140550K .......... .......... .......... .......... .......... 26% 9.57M 37s
140600K .......... .......... .......... .......... .......... 26% 6.65M 37s
140650K .......... .......... .......... .......... .......... 26% 9.70M 37s
140700K .......... .......... .......... .......... .......... 26% 7.35M 37s
140750K .......... .......... .......... .......... .......... 26% 9.60M 37s
140800K .......... .......... .......... .......... .......... 26% 8.69M 37s
140850K .......... .......... .......... .......... .......... 26% 17.2M 37s
140900K .......... .......... .......... .......... .......... 26% 44.5M 37s
140950K .......... .......... .......... .......... .......... 26% 23.9M 37s
141000K .......... .......... .......... .......... .......... 26% 30.1M 37s
141050K .......... .......... .......... .......... .......... 26% 22.6M 37s
141100K .......... .......... .......... .......... .......... 26% 27.2M 37s
141150K .......... .......... .......... .......... .......... 26% 28.0M 37s
141200K .......... .......... .......... .......... .......... 26% 20.4M 37s
141250K .......... .......... .......... .......... .......... 26% 29.8M 37s
141300K .......... .......... .......... .......... .......... 26% 24.7M 37s
141350K .......... .......... .......... .......... .......... 26% 12.9M 37s
141400K .......... .......... .......... .......... .......... 26% 36.9M 37s
141450K .......... .......... .......... .......... .......... 26% 15.5M 37s
141500K .......... .......... .......... .......... .......... 26% 21.6M 37s
141550K .......... .......... .......... .......... .......... 26% 20.0M 37s
141600K .......... .......... .......... .......... .......... 26% 16.4M 37s
141650K .......... .......... .......... .......... .......... 26% 19.1M 37s
141700K .......... .......... .......... .......... .......... 26% 15.2M 37s
141750K .......... .......... .......... .......... .......... 26% 14.8M 37s
141800K .......... .......... .......... .......... .......... 26% 13.8M 37s
141850K .......... .......... .......... .......... .......... 26% 12.9M 37s
141900K .......... .......... .......... .......... .......... 26% 14.8M 37s
141950K .......... .......... .......... .......... .......... 26% 10.5M 37s
142000K .......... .......... .......... .......... .......... 26% 10.7M 37s
142050K .......... .......... .......... .......... .......... 26% 10.5M 37s
142100K .......... .......... .......... .......... .......... 26% 8.34M 37s
142150K .......... .......... .......... .......... .......... 26% 7.11M 37s
142200K .......... .......... .......... .......... .......... 26% 6.81M 37s
142250K .......... .......... .......... .......... .......... 26% 8.04M 37s
142300K .......... .......... .......... .......... .......... 26% 8.84M 37s
142350K .......... .......... .......... .......... .......... 26% 6.36M 37s
142400K .......... .......... .......... .......... .......... 26% 8.57M 37s
142450K .......... .......... .......... .......... .......... 26% 7.70M 37s
142500K .......... .......... .......... .......... .......... 26% 7.84M 37s
142550K .......... .......... .......... .......... .......... 26% 21.3M 37s
142600K .......... .......... .......... .......... .......... 26% 16.6M 37s
142650K .......... .......... .......... .......... .......... 26% 13.0M 37s
142700K .......... .......... .......... .......... .......... 26% 13.9M 37s
142750K .......... .......... .......... .......... .......... 26% 13.3M 37s
142800K .......... .......... .......... .......... .......... 26% 21.5M 37s
142850K .......... .......... .......... .......... .......... 26% 11.1M 37s
142900K .......... .......... .......... .......... .......... 26% 21.0M 37s
142950K .......... .......... .......... .......... .......... 26% 11.8M 37s
143000K .......... .......... .......... .......... .......... 26% 13.2M 37s
143050K .......... .......... .......... .......... .......... 26% 7.73M 37s
143100K .......... .......... .......... .......... .......... 26% 6.30M 37s
143150K .......... .......... .......... .......... .......... 26% 7.86M 37s
143200K .......... .......... .......... .......... .......... 26% 6.53M 37s
143250K .......... .......... .......... .......... .......... 26% 6.97M 37s
143300K .......... .......... .......... .......... .......... 26% 5.81M 37s
143350K .......... .......... .......... .......... .......... 26% 5.95M 37s
143400K .......... .......... .......... .......... .......... 26% 7.15M 37s
143450K .......... .......... .......... .......... .......... 26% 4.81M 37s
143500K .......... .......... .......... .......... .......... 26% 6.23M 37s
143550K .......... .......... .......... .......... .......... 26% 6.89M 37s
143600K .......... .......... .......... .......... .......... 26% 5.89M 37s
143650K .......... .......... .......... .......... .......... 26% 6.11M 37s
143700K .......... .......... .......... .......... .......... 26% 7.45M 37s
143750K .......... .......... .......... .......... .......... 26% 18.5M 37s
143800K .......... .......... .......... .......... .......... 26% 26.7M 37s
143850K .......... .......... .......... .......... .......... 26% 19.0M 37s
143900K .......... .......... .......... .......... .......... 26% 13.9M 37s
143950K .......... .......... .......... .......... .......... 26% 16.2M 37s
144000K .......... .......... .......... .......... .......... 26% 8.10M 37s
144050K .......... .......... .......... .......... .......... 26% 8.88M 37s
144100K .......... .......... .......... .......... .......... 26% 5.46M 37s
144150K .......... .......... .......... .......... .......... 26% 8.28M 37s
144200K .......... .......... .......... .......... .......... 26% 6.71M 37s
144250K .......... .......... .......... .......... .......... 26% 11.5M 37s
144300K .......... .......... .......... .......... .......... 26% 24.8M 37s
144350K .......... .......... .......... .......... .......... 26% 31.0M 37s
144400K .......... .......... .......... .......... .......... 26% 23.8M 37s
144450K .......... .......... .......... .......... .......... 26% 18.0M 37s
144500K .......... .......... .......... .......... .......... 26% 17.8M 37s
144550K .......... .......... .......... .......... .......... 26% 15.5M 37s
144600K .......... .......... .......... .......... .......... 26% 16.2M 37s
144650K .......... .......... .......... .......... .......... 26% 14.9M 37s
144700K .......... .......... .......... .......... .......... 26% 14.5M 37s
144750K .......... .......... .......... .......... .......... 26% 12.0M 37s
144800K .......... .......... .......... .......... .......... 26% 13.7M 37s
144850K .......... .......... .......... .......... .......... 26% 7.10M 37s
144900K .......... .......... .......... .......... .......... 26% 8.57M 37s
144950K .......... .......... .......... .......... .......... 26% 7.38M 37s
145000K .......... .......... .......... .......... .......... 26% 5.96M 37s
145050K .......... .......... .......... .......... .......... 27% 7.54M 37s
145100K .......... .......... .......... .......... .......... 27% 10.5M 37s
145150K .......... .......... .......... .......... .......... 27% 22.3M 37s
145200K .......... .......... .......... .......... .......... 27% 21.3M 37s
145250K .......... .......... .......... .......... .......... 27% 17.1M 37s
145300K .......... .......... .......... .......... .......... 27% 12.2M 37s
145350K .......... .......... .......... .......... .......... 27% 13.1M 37s
145400K .......... .......... .......... .......... .......... 27% 11.0M 37s
145450K .......... .......... .......... .......... .......... 27% 6.76M 37s
145500K .......... .......... .......... .......... .......... 27% 8.24M 37s
145550K .......... .......... .......... .......... .......... 27% 5.75M 37s
145600K .......... .......... .......... .......... .......... 27% 5.83M 37s
145650K .......... .......... .......... .......... .......... 27% 7.04M 37s
145700K .......... .......... .......... .......... .......... 27% 6.52M 37s
145750K .......... .......... .......... .......... .......... 27% 20.5M 37s
145800K .......... .......... .......... .......... .......... 27% 35.6M 37s
145850K .......... .......... .......... .......... .......... 27% 16.9M 37s
145900K .......... .......... .......... .......... .......... 27% 20.2M 37s
145950K .......... .......... .......... .......... .......... 27% 10.8M 37s
146000K .......... .......... .......... .......... .......... 27% 8.48M 37s
146050K .......... .......... .......... .......... .......... 27% 7.33M 37s
146100K .......... .......... .......... .......... .......... 27% 6.47M 37s
146150K .......... .......... .......... .......... .......... 27% 7.87M 37s
146200K .......... .......... .......... .......... .......... 27% 4.99M 37s
146250K .......... .......... .......... .......... .......... 27% 6.31M 37s
146300K .......... .......... .......... .......... .......... 27% 6.92M 37s
146350K .......... .......... .......... .......... .......... 27% 4.73M 37s
146400K .......... .......... .......... .......... .......... 27% 6.38M 37s
146450K .......... .......... .......... .......... .......... 27% 18.5M 37s
146500K .......... .......... .......... .......... .......... 27% 41.1M 37s
146550K .......... .......... .......... .......... .......... 27% 37.3M 37s
146600K .......... .......... .......... .......... .......... 27% 26.5M 37s
146650K .......... .......... .......... .......... .......... 27% 17.4M 37s
146700K .......... .......... .......... .......... .......... 27% 49.7M 37s
146750K .......... .......... .......... .......... .......... 27% 21.3M 37s
146800K .......... .......... .......... .......... .......... 27% 26.7M 37s
146850K .......... .......... .......... .......... .......... 27% 18.8M 37s
146900K .......... .......... .......... .......... .......... 27% 39.1M 36s
146950K .......... .......... .......... .......... .......... 27% 23.4M 36s
147000K .......... .......... .......... .......... .......... 27% 21.0M 36s
147050K .......... .......... .......... .......... .......... 27% 24.9M 36s
147100K .......... .......... .......... .......... .......... 27% 18.0M 36s
147150K .......... .......... .......... .......... .......... 27% 22.1M 36s
147200K .......... .......... .......... .......... .......... 27% 11.6M 36s
147250K .......... .......... .......... .......... .......... 27% 11.2M 36s
147300K .......... .......... .......... .......... .......... 27% 10.6M 36s
147350K .......... .......... .......... .......... .......... 27% 12.3M 36s
147400K .......... .......... .......... .......... .......... 27% 15.2M 36s
147450K .......... .......... .......... .......... .......... 27% 11.3M 36s
147500K .......... .......... .......... .......... .......... 27% 12.1M 36s
147550K .......... .......... .......... .......... .......... 27% 15.3M 36s
147600K .......... .......... .......... .......... .......... 27% 11.6M 36s
147650K .......... .......... .......... .......... .......... 27% 11.1M 36s
147700K .......... .......... .......... .......... .......... 27% 7.12M 36s
147750K .......... .......... .......... .......... .......... 27% 8.72M 36s
147800K .......... .......... .......... .......... .......... 27% 8.03M 36s
147850K .......... .......... .......... .......... .......... 27% 8.04M 36s
147900K .......... .......... .......... .......... .......... 27% 5.97M 36s
147950K .......... .......... .......... .......... .......... 27% 5.27M 36s
148000K .......... .......... .......... .......... .......... 27% 6.80M 36s
148050K .......... .......... .......... .......... .......... 27% 6.32M 36s
148100K .......... .......... .......... .......... .......... 27% 5.51M 36s
148150K .......... .......... .......... .......... .......... 27% 6.24M 36s
148200K .......... .......... .......... .......... .......... 27% 5.63M 36s
148250K .......... .......... .......... .......... .......... 27% 23.7M 36s
148300K .......... .......... .......... .......... .......... 27% 24.1M 36s
148350K .......... .......... .......... .......... .......... 27% 13.0M 36s
148400K .......... .......... .......... .......... .......... 27% 29.2M 36s
148450K .......... .......... .......... .......... .......... 27% 7.56M 36s
148500K .......... .......... .......... .......... .......... 27% 10.0M 36s
148550K .......... .......... .......... .......... .......... 27% 10.3M 36s
148600K .......... .......... .......... .......... .......... 27% 7.32M 36s
148650K .......... .......... .......... .......... .......... 27% 8.71M 36s
148700K .......... .......... .......... .......... .......... 27% 7.49M 36s
148750K .......... .......... .......... .......... .......... 27% 10.1M 36s
148800K .......... .......... .......... .......... .......... 27% 14.6M 36s
148850K .......... .......... .......... .......... .......... 27% 23.2M 36s
148900K .......... .......... .......... .......... .......... 27% 14.9M 36s
148950K .......... .......... .......... .......... .......... 27% 15.9M 36s
149000K .......... .......... .......... .......... .......... 27% 14.3M 36s
149050K .......... .......... .......... .......... .......... 27% 11.6M 36s
149100K .......... .......... .......... .......... .......... 27% 8.71M 36s
149150K .......... .......... .......... .......... .......... 27% 12.0M 36s
149200K .......... .......... .......... .......... .......... 27% 7.72M 36s
149250K .......... .......... .......... .......... .......... 27% 11.8M 36s
149300K .......... .......... .......... .......... .......... 27% 11.4M 36s
149350K .......... .......... .......... .......... .......... 27% 8.96M 36s
149400K .......... .......... .......... .......... .......... 27% 11.7M 36s
149450K .......... .......... .......... .......... .......... 27% 9.14M 36s
149500K .......... .......... .......... .......... .......... 27% 8.22M 36s
149550K .......... .......... .......... .......... .......... 27% 9.65M 36s
149600K .......... .......... .......... .......... .......... 27% 6.64M 36s
149650K .......... .......... .......... .......... .......... 27% 9.11M 36s
149700K .......... .......... .......... .......... .......... 27% 6.98M 36s
149750K .......... .......... .......... .......... .......... 27% 11.6M 36s
149800K .......... .......... .......... .......... .......... 27% 22.7M 36s
149850K .......... .......... .......... .......... .......... 27% 27.4M 36s
149900K .......... .......... .......... .......... .......... 27% 18.7M 36s
149950K .......... .......... .......... .......... .......... 27% 32.4M 36s
150000K .......... .......... .......... .......... .......... 27% 14.2M 36s
150050K .......... .......... .......... .......... .......... 27% 9.78M 36s
150100K .......... .......... .......... .......... .......... 27% 10.0M 36s
150150K .......... .......... .......... .......... .......... 27% 11.5M 36s
150200K .......... .......... .......... .......... .......... 27% 10.9M 36s
150250K .......... .......... .......... .......... .......... 27% 9.97M 36s
150300K .......... .......... .......... .......... .......... 27% 6.76M 36s
150350K .......... .......... .......... .......... .......... 27% 9.19M 36s
150400K .......... .......... .......... .......... .......... 27% 9.59M 36s
150450K .......... .......... .......... .......... .......... 28% 10.3M 36s
150500K .......... .......... .......... .......... .......... 28% 7.74M 36s
150550K .......... .......... .......... .......... .......... 28% 9.12M 36s
150600K .......... .......... .......... .......... .......... 28% 6.22M 36s
150650K .......... .......... .......... .......... .......... 28% 9.52M 36s
150700K .......... .......... .......... .......... .......... 28% 5.88M 36s
150750K .......... .......... .......... .......... .......... 28% 8.96M 36s
150800K .......... .......... .......... .......... .......... 28% 11.6M 36s
150850K .......... .......... .......... .......... .......... 28% 7.78M 36s
150900K .......... .......... .......... .......... .......... 28% 7.04M 36s
150950K .......... .......... .......... .......... .......... 28% 5.36M 36s
151000K .......... .......... .......... .......... .......... 28% 5.53M 36s
151050K .......... .......... .......... .......... .......... 28% 6.06M 36s
151100K .......... .......... .......... .......... .......... 28% 7.93M 36s
151150K .......... .......... .......... .......... .......... 28% 33.2M 36s
151200K .......... .......... .......... .......... .......... 28% 21.2M 36s
151250K .......... .......... .......... .......... .......... 28% 27.3M 36s
151300K .......... .......... .......... .......... .......... 28% 22.7M 36s
151350K .......... .......... .......... .......... .......... 28% 24.4M 36s
151400K .......... .......... .......... .......... .......... 28% 25.5M 36s
151450K .......... .......... .......... .......... .......... 28% 15.2M 36s
151500K .......... .......... .......... .......... .......... 28% 19.8M 36s
151550K .......... .......... .......... .......... .......... 28% 13.4M 36s
151600K .......... .......... .......... .......... .......... 28% 22.3M 36s
151650K .......... .......... .......... .......... .......... 28% 19.8M 36s
151700K .......... .......... .......... .......... .......... 28% 15.2M 36s
151750K .......... .......... .......... .......... .......... 28% 16.6M 36s
151800K .......... .......... .......... .......... .......... 28% 14.3M 36s
151850K .......... .......... .......... .......... .......... 28% 13.0M 36s
151900K .......... .......... .......... .......... .......... 28% 14.1M 36s
151950K .......... .......... .......... .......... .......... 28% 12.8M 36s
152000K .......... .......... .......... .......... .......... 28% 14.2M 36s
152050K .......... .......... .......... .......... .......... 28% 10.8M 36s
152100K .......... .......... .......... .......... .......... 28% 8.84M 36s
152150K .......... .......... .......... .......... .......... 28% 12.8M 36s
152200K .......... .......... .......... .......... .......... 28% 9.36M 36s
152250K .......... .......... .......... .......... .......... 28% 8.91M 36s
152300K .......... .......... .......... .......... .......... 28% 8.05M 36s
152350K .......... .......... .......... .......... .......... 28% 7.54M 36s
152400K .......... .......... .......... .......... .......... 28% 7.67M 36s
152450K .......... .......... .......... .......... .......... 28% 6.64M 36s
152500K .......... .......... .......... .......... .......... 28% 7.69M 36s
152550K .......... .......... .......... .......... .......... 28% 6.63M 36s
152600K .......... .......... .......... .......... .......... 28% 9.54M 36s
152650K .......... .......... .......... .......... .......... 28% 11.5M 36s
152700K .......... .......... .......... .......... .......... 28% 9.65M 36s
152750K .......... .......... .......... .......... .......... 28% 11.3M 36s
152800K .......... .......... .......... .......... .......... 28% 14.3M 36s
152850K .......... .......... .......... .......... .......... 28% 5.65M 36s
152900K .......... .......... .......... .......... .......... 28% 6.79M 36s
152950K .......... .......... .......... .......... .......... 28% 4.89M 36s
153000K .......... .......... .......... .......... .......... 28% 3.74M 36s
153050K .......... .......... .......... .......... .......... 28% 5.76M 36s
153100K .......... .......... .......... .......... .......... 28% 6.07M 36s
153150K .......... .......... .......... .......... .......... 28% 9.46M 36s
153200K .......... .......... .......... .......... .......... 28% 11.8M 36s
153250K .......... .......... .......... .......... .......... 28% 11.3M 36s
153300K .......... .......... .......... .......... .......... 28% 14.1M 36s
153350K .......... .......... .......... .......... .......... 28% 17.3M 36s
153400K .......... .......... .......... .......... .......... 28% 41.9M 36s
153450K .......... .......... .......... .......... .......... 28% 36.2M 36s
153500K .......... .......... .......... .......... .......... 28% 38.5M 36s
153550K .......... .......... .......... .......... .......... 28% 41.5M 36s
153600K .......... .......... .......... .......... .......... 28% 28.5M 36s
153650K .......... .......... .......... .......... .......... 28% 35.1M 36s
153700K .......... .......... .......... .......... .......... 28% 35.1M 36s
153750K .......... .......... .......... .......... .......... 28% 29.1M 36s
153800K .......... .......... .......... .......... .......... 28% 26.0M 36s
153850K .......... .......... .......... .......... .......... 28% 16.0M 36s
153900K .......... .......... .......... .......... .......... 28% 21.2M 36s
153950K .......... .......... .......... .......... .......... 28% 21.7M 36s
154000K .......... .......... .......... .......... .......... 28% 19.6M 36s
154050K .......... .......... .......... .......... .......... 28% 10.8M 36s
154100K .......... .......... .......... .......... .......... 28% 25.4M 36s
154150K .......... .......... .......... .......... .......... 28% 26.2M 36s
154200K .......... .......... .......... .......... .......... 28% 16.9M 36s
154250K .......... .......... .......... .......... .......... 28% 11.2M 36s
154300K .......... .......... .......... .......... .......... 28% 21.3M 36s
154350K .......... .......... .......... .......... .......... 28% 17.0M 36s
154400K .......... .......... .......... .......... .......... 28% 13.0M 36s
154450K .......... .......... .......... .......... .......... 28% 15.5M 36s
154500K .......... .......... .......... .......... .......... 28% 38.9M 36s
154550K .......... .......... .......... .......... .......... 28% 15.8M 36s
154600K .......... .......... .......... .......... .......... 28% 15.9M 36s
154650K .......... .......... .......... .......... .......... 28% 17.3M 36s
154700K .......... .......... .......... .......... .......... 28% 20.8M 36s
154750K .......... .......... .......... .......... .......... 28% 17.7M 36s
154800K .......... .......... .......... .......... .......... 28% 16.1M 36s
154850K .......... .......... .......... .......... .......... 28% 13.1M 36s
154900K .......... .......... .......... .......... .......... 28% 18.9M 36s
154950K .......... .......... .......... .......... .......... 28% 17.5M 36s
155000K .......... .......... .......... .......... .......... 28% 17.1M 36s
155050K .......... .......... .......... .......... .......... 28% 15.7M 36s
155100K .......... .......... .......... .......... .......... 28% 16.6M 36s
155150K .......... .......... .......... .......... .......... 28% 16.1M 36s
155200K .......... .......... .......... .......... .......... 28% 15.4M 36s
155250K .......... .......... .......... .......... .......... 28% 15.2M 36s
155300K .......... .......... .......... .......... .......... 28% 19.4M 36s
155350K .......... .......... .......... .......... .......... 28% 11.6M 36s
155400K .......... .......... .......... .......... .......... 28% 20.5M 36s
155450K .......... .......... .......... .......... .......... 28% 11.6M 36s
155500K .......... .......... .......... .......... .......... 28% 15.1M 36s
155550K .......... .......... .......... .......... .......... 28% 16.1M 36s
155600K .......... .......... .......... .......... .......... 28% 13.8M 36s
155650K .......... .......... .......... .......... .......... 28% 15.4M 36s
155700K .......... .......... .......... .......... .......... 28% 17.0M 36s
155750K .......... .......... .......... .......... .......... 28% 14.7M 36s
155800K .......... .......... .......... .......... .......... 29% 17.1M 36s
155850K .......... .......... .......... .......... .......... 29% 17.5M 35s
155900K .......... .......... .......... .......... .......... 29% 18.3M 35s
155950K .......... .......... .......... .......... .......... 29% 14.8M 35s
156000K .......... .......... .......... .......... .......... 29% 16.4M 35s
156050K .......... .......... .......... .......... .......... 29% 26.0M 35s
156100K .......... .......... .......... .......... .......... 29% 14.6M 35s
156150K .......... .......... .......... .......... .......... 29% 20.2M 35s
156200K .......... .......... .......... .......... .......... 29% 11.3M 35s
156250K .......... .......... .......... .......... .......... 29% 17.6M 35s
156300K .......... .......... .......... .......... .......... 29% 17.7M 35s
156350K .......... .......... .......... .......... .......... 29% 18.5M 35s
156400K .......... .......... .......... .......... .......... 29% 21.1M 35s
156450K .......... .......... .......... .......... .......... 29% 15.2M 35s
156500K .......... .......... .......... .......... .......... 29% 59.5M 35s
156550K .......... .......... .......... .......... .......... 29% 10.1M 35s
156600K .......... .......... .......... .......... .......... 29% 14.0M 35s
156650K .......... .......... .......... .......... .......... 29% 56.4M 35s
156700K .......... .......... .......... .......... .......... 29% 16.0M 35s
156750K .......... .......... .......... .......... .......... 29% 13.1M 35s
156800K .......... .......... .......... .......... .......... 29% 20.1M 35s
156850K .......... .......... .......... .......... .......... 29% 12.5M 35s
156900K .......... .......... .......... .......... .......... 29% 18.6M 35s
156950K .......... .......... .......... .......... .......... 29% 21.0M 35s
157000K .......... .......... .......... .......... .......... 29% 14.7M 35s
157050K .......... .......... .......... .......... .......... 29% 18.1M 35s
157100K .......... .......... .......... .......... .......... 29% 11.8M 35s
157150K .......... .......... .......... .......... .......... 29% 18.7M 35s
157200K .......... .......... .......... .......... .......... 29% 11.1M 35s
157250K .......... .......... .......... .......... .......... 29% 15.3M 35s
157300K .......... .......... .......... .......... .......... 29% 13.0M 35s
157350K .......... .......... .......... .......... .......... 29%  239K 36s
157400K .......... .......... .......... .......... .......... 29% 13.3M 36s
157450K .......... .......... .......... .......... .......... 29% 10.9M 36s
157500K .......... .......... .......... .......... .......... 29% 14.5M 36s
157550K .......... .......... .......... .......... .......... 29% 13.5M 36s
157600K .......... .......... .......... .......... .......... 29% 16.3M 36s
157650K .......... .......... .......... .......... .......... 29% 14.9M 36s
157700K .......... .......... .......... .......... .......... 29% 17.0M 36s
157750K .......... .......... .......... .......... .......... 29% 17.7M 36s
157800K .......... .......... .......... .......... .......... 29% 18.4M 36s
157850K .......... .......... .......... .......... .......... 29% 14.4M 36s
157900K .......... .......... .......... .......... .......... 29% 17.0M 36s
157950K .......... .......... .......... .......... .......... 29% 16.6M 36s
158000K .......... .......... .......... .......... .......... 29% 13.5M 36s
158050K .......... .......... .......... .......... .......... 29% 18.1M 36s
158100K .......... .......... .......... .......... .......... 29% 12.4M 36s
158150K .......... .......... .......... .......... .......... 29% 21.3M 36s
158200K .......... .......... .......... .......... .......... 29% 16.7M 36s
158250K .......... .......... .......... .......... .......... 29% 23.6M 36s
158300K .......... .......... .......... .......... .......... 29% 25.2M 36s
158350K .......... .......... .......... .......... .......... 29% 15.0M 36s
158400K .......... .......... .......... .......... .......... 29% 19.9M 36s
158450K .......... .......... .......... .......... .......... 29% 44.5M 36s
158500K .......... .......... .......... .......... .......... 29% 76.1M 36s
158550K .......... .......... .......... .......... .......... 29% 23.6M 36s
158600K .......... .......... .......... .......... .......... 29% 20.9M 36s
158650K .......... .......... .......... .......... .......... 29% 23.0M 35s
158700K .......... .......... .......... .......... .......... 29% 15.5M 35s
158750K .......... .......... .......... .......... .......... 29% 27.2M 35s
158800K .......... .......... .......... .......... .......... 29% 16.7M 35s
158850K .......... .......... .......... .......... .......... 29% 18.1M 35s
158900K .......... .......... .......... .......... .......... 29% 19.9M 35s
158950K .......... .......... .......... .......... .......... 29% 16.4M 35s
159000K .......... .......... .......... .......... .......... 29% 15.1M 35s
159050K .......... .......... .......... .......... .......... 29% 23.0M 35s
159100K .......... .......... .......... .......... .......... 29% 13.7M 35s
159150K .......... .......... .......... .......... .......... 29% 5.69M 35s
159200K .......... .......... .......... .......... .......... 29%  171M 35s
159250K .......... .......... .......... .......... .......... 29%  136M 35s
159300K .......... .......... .......... .......... .......... 29% 26.3M 35s
159350K .......... .......... .......... .......... .......... 29% 16.7M 35s
159400K .......... .......... .......... .......... .......... 29% 16.1M 35s
159450K .......... .......... .......... .......... .......... 29% 16.6M 35s
159500K .......... .......... .......... .......... .......... 29% 20.5M 35s
159550K .......... .......... .......... .......... .......... 29% 16.3M 35s
159600K .......... .......... .......... .......... .......... 29% 24.3M 35s
159650K .......... .......... .......... .......... .......... 29% 18.2M 35s
159700K .......... .......... .......... .......... .......... 29%  123M 35s
159750K .......... .......... .......... .......... .......... 29% 20.8M 35s
159800K .......... .......... .......... .......... .......... 29% 26.3M 35s
159850K .......... .......... .......... .......... .......... 29% 20.3M 35s
159900K .......... .......... .......... .......... .......... 29% 11.5M 35s
159950K .......... .......... .......... .......... .......... 29% 8.85M 35s
160000K .......... .......... .......... .......... .......... 29% 8.20M 35s
160050K .......... .......... .......... .......... .......... 29% 5.01M 35s
160100K .......... .......... .......... .......... .......... 29% 8.45M 35s
160150K .......... .......... .......... .......... .......... 29% 8.08M 35s
160200K .......... .......... .......... .......... .......... 29% 5.99M 35s
160250K .......... .......... .......... .......... .......... 29% 6.57M 35s
160300K .......... .......... .......... .......... .......... 29% 7.38M 35s
160350K .......... .......... .......... .......... .......... 29% 7.63M 35s
160400K .......... .......... .......... .......... .......... 29% 7.74M 35s
160450K .......... .......... .......... .......... .......... 29% 6.52M 35s
160500K .......... .......... .......... .......... .......... 29% 11.1M 35s
160550K .......... .......... .......... .......... .......... 29% 11.4M 35s
160600K .......... .......... .......... .......... .......... 29% 9.81M 35s
160650K .......... .......... .......... .......... .......... 29% 8.45M 35s
160700K .......... .......... .......... .......... .......... 29% 9.18M 35s
160750K .......... .......... .......... .......... .......... 29% 8.10M 35s
160800K .......... .......... .......... .......... .......... 29% 9.62M 35s
160850K .......... .......... .......... .......... .......... 29% 5.60M 35s
160900K .......... .......... .......... .......... .......... 29% 6.31M 35s
160950K .......... .......... .......... .......... .......... 29% 5.87M 35s
161000K .......... .......... .......... .......... .......... 29% 6.96M 35s
161050K .......... .......... .......... .......... .......... 29% 5.78M 35s
161100K .......... .......... .......... .......... .......... 29% 6.94M 35s
161150K .......... .......... .......... .......... .......... 29% 6.99M 35s
161200K .......... .......... .......... .......... .......... 30% 5.47M 35s
161250K .......... .......... .......... .......... .......... 30% 6.36M 35s
161300K .......... .......... .......... .......... .......... 30% 5.77M 35s
161350K .......... .......... .......... .......... .......... 30% 9.39M 35s
161400K .......... .......... .......... .......... .......... 30% 10.5M 35s
161450K .......... .......... .......... .......... .......... 30% 11.5M 35s
161500K .......... .......... .......... .......... .......... 30% 7.23M 35s
161550K .......... .......... .......... .......... .......... 30% 7.16M 35s
161600K .......... .......... .......... .......... .......... 30% 5.21M 35s
161650K .......... .......... .......... .......... .......... 30% 7.40M 35s
161700K .......... .......... .......... .......... .......... 30% 6.15M 35s
161750K .......... .......... .......... .......... .......... 30% 6.28M 35s
161800K .......... .......... .......... .......... .......... 30% 6.73M 35s
161850K .......... .......... .......... .......... .......... 30% 5.59M 35s
161900K .......... .......... .......... .......... .......... 30% 4.35M 35s
161950K .......... .......... .......... .......... .......... 30% 10.5M 35s
162000K .......... .......... .......... .......... .......... 30% 16.1M 35s
162050K .......... .......... .......... .......... .......... 30% 12.8M 35s
162100K .......... .......... .......... .......... .......... 30% 5.88M 35s
162150K .......... .......... .......... .......... .......... 30% 9.94M 35s
162200K .......... .......... .......... .......... .......... 30% 9.47M 35s
162250K .......... .......... .......... .......... .......... 30% 6.26M 35s
162300K .......... .......... .......... .......... .......... 30% 7.47M 35s
162350K .......... .......... .......... .......... .......... 30% 3.98M 35s
162400K .......... .......... .......... .......... .......... 30% 3.66M 35s
162450K .......... .......... .......... .......... .......... 30% 3.63M 35s
162500K .......... .......... .......... .......... .......... 30% 8.32M 35s
162550K .......... .......... .......... .......... .......... 30% 4.12M 35s
162600K .......... .......... .......... .......... .......... 30% 4.87M 35s
162650K .......... .......... .......... .......... .......... 30%  208K 36s
162700K .......... .......... .......... .......... .......... 30% 2.42M 36s
162750K .......... .......... .......... .......... .......... 30% 7.26M 36s
162800K .......... .......... .......... .......... .......... 30% 6.80M 36s
162850K .......... .......... .......... .......... .......... 30% 12.4M 36s
162900K .......... .......... .......... .......... .......... 30% 9.37M 36s
162950K .......... .......... .......... .......... .......... 30% 8.31M 36s
163000K .......... .......... .......... .......... .......... 30% 7.61M 36s
163050K .......... .......... .......... .......... .......... 30% 8.08M 36s
163100K .......... .......... .......... .......... .......... 30% 5.37M 36s
163150K .......... .......... .......... .......... .......... 30% 1.94M 36s
163200K .......... .......... .......... .......... .......... 30% 8.91M 36s
163250K .......... .......... .......... .......... .......... 30% 11.5M 36s
163300K .......... .......... .......... .......... .......... 30% 16.1M 36s
163350K .......... .......... .......... .......... .......... 30% 10.1M 36s
163400K .......... .......... .......... .......... .......... 30% 9.23M 36s
163450K .......... .......... .......... .......... .......... 30% 6.43M 36s
163500K .......... .......... .......... .......... .......... 30% 7.93M 36s
163550K .......... .......... .......... .......... .......... 30% 8.52M 36s
163600K .......... .......... .......... .......... .......... 30% 8.85M 36s
163650K .......... .......... .......... .......... .......... 30% 7.47M 36s
163700K .......... .......... .......... .......... .......... 30% 5.43M 36s
163750K .......... .......... .......... .......... .......... 30% 10.0M 36s
163800K .......... .......... .......... .......... .......... 30% 11.7M 36s
163850K .......... .......... .......... .......... .......... 30% 10.4M 36s
163900K .......... .......... .......... .......... .......... 30% 13.0M 36s
163950K .......... .......... .......... .......... .......... 30% 10.1M 36s
164000K .......... .......... .......... .......... .......... 30% 10.8M 36s
164050K .......... .......... .......... .......... .......... 30% 12.1M 36s
164100K .......... .......... .......... .......... .......... 30% 8.77M 36s
164150K .......... .......... .......... .......... .......... 30% 10.5M 36s
164200K .......... .......... .......... .......... .......... 30% 6.90M 36s
164250K .......... .......... .......... .......... .......... 30% 9.15M 36s
164300K .......... .......... .......... .......... .......... 30% 9.69M 36s
164350K .......... .......... .......... .......... .......... 30% 4.61M 36s
164400K .......... .......... .......... .......... .......... 30% 6.52M 36s
164450K .......... .......... .......... .......... .......... 30% 5.77M 36s
164500K .......... .......... .......... .......... .......... 30% 6.34M 36s
164550K .......... .......... .......... .......... .......... 30% 6.99M 36s
164600K .......... .......... .......... .......... .......... 30% 20.2M 36s
164650K .......... .......... .......... .......... .......... 30% 13.1M 36s
164700K .......... .......... .......... .......... .......... 30% 16.7M 36s
164750K .......... .......... .......... .......... .......... 30% 16.4M 36s
164800K .......... .......... .......... .......... .......... 30% 28.2M 36s
164850K .......... .......... .......... .......... .......... 30% 8.80M 36s
164900K .......... .......... .......... .......... .......... 30% 39.4M 36s
164950K .......... .......... .......... .......... .......... 30% 11.2M 36s
165000K .......... .......... .......... .......... .......... 30% 12.3M 36s
165050K .......... .......... .......... .......... .......... 30% 12.6M 36s
165100K .......... .......... .......... .......... .......... 30% 6.81M 36s
165150K .......... .......... .......... .......... .......... 30% 6.01M 36s
165200K .......... .......... .......... .......... .......... 30% 3.90M 36s
165250K .......... .......... .......... .......... .......... 30% 5.76M 36s
165300K .......... .......... .......... .......... .......... 30% 6.60M 36s
165350K .......... .......... .......... .......... .......... 30% 20.4M 36s
165400K .......... .......... .......... .......... .......... 30% 13.8M 36s
165450K .......... .......... .......... .......... .......... 30% 14.4M 36s
165500K .......... .......... .......... .......... .......... 30% 18.0M 36s
165550K .......... .......... .......... .......... .......... 30% 14.5M 36s
165600K .......... .......... .......... .......... .......... 30% 15.2M 36s
165650K .......... .......... .......... .......... .......... 30% 15.3M 36s
165700K .......... .......... .......... .......... .......... 30% 15.1M 36s
165750K .......... .......... .......... .......... .......... 30% 14.7M 36s
165800K .......... .......... .......... .......... .......... 30% 14.0M 36s
165850K .......... .......... .......... .......... .......... 30% 15.2M 36s
165900K .......... .......... .......... .......... .......... 30% 15.2M 36s
165950K .......... .......... .......... .......... .......... 30% 9.58M 36s
166000K .......... .......... .......... .......... .......... 30% 15.5M 36s
166050K .......... .......... .......... .......... .......... 30% 10.4M 36s
166100K .......... .......... .......... .......... .......... 30% 5.26M 36s
166150K .......... .......... .......... .......... .......... 30% 7.55M 36s
166200K .......... .......... .......... .......... .......... 30% 4.00M 36s
166250K .......... .......... .......... .......... .......... 30% 7.15M 36s
166300K .......... .......... .......... .......... .......... 30% 8.05M 36s
166350K .......... .......... .......... .......... .......... 30% 8.08M 36s
166400K .......... .......... .......... .......... .......... 30% 9.69M 36s
166450K .......... .......... .......... .......... .......... 30% 7.68M 36s
166500K .......... .......... .......... .......... .......... 30% 9.73M 36s
166550K .......... .......... .......... .......... .......... 31% 9.62M 36s
166600K .......... .......... .......... .......... .......... 31% 15.0M 36s
166650K .......... .......... .......... .......... .......... 31% 30.0M 36s
166700K .......... .......... .......... .......... .......... 31% 40.4M 36s
166750K .......... .......... .......... .......... .......... 31% 49.8M 36s
166800K .......... .......... .......... .......... .......... 31% 39.0M 36s
166850K .......... .......... .......... .......... .......... 31% 42.2M 36s
166900K .......... .......... .......... .......... .......... 31% 50.8M 36s
166950K .......... .......... .......... .......... .......... 31% 34.2M 36s
167000K .......... .......... .......... .......... .......... 31% 32.8M 36s
167050K .......... .......... .......... .......... .......... 31% 34.5M 36s
167100K .......... .......... .......... .......... .......... 31% 17.5M 36s
167150K .......... .......... .......... .......... .......... 31% 42.8M 36s
167200K .......... .......... .......... .......... .......... 31% 36.4M 36s
167250K .......... .......... .......... .......... .......... 31% 20.4M 35s
167300K .......... .......... .......... .......... .......... 31% 23.4M 35s
167350K .......... .......... .......... .......... .......... 31% 13.5M 35s
167400K .......... .......... .......... .......... .......... 31% 16.1M 35s
167450K .......... .......... .......... .......... .......... 31% 7.64M 35s
167500K .......... .......... .......... .......... .......... 31% 6.77M 35s
167550K .......... .......... .......... .......... .......... 31% 6.28M 35s
167600K .......... .......... .......... .......... .......... 31% 4.37M 35s
167650K .......... .......... .......... .......... .......... 31% 6.46M 35s
167700K .......... .......... .......... .......... .......... 31% 5.10M 35s
167750K .......... .......... .......... .......... .......... 31% 8.98M 35s
167800K .......... .......... .......... .......... .......... 31% 10.3M 35s
167850K .......... .......... .......... .......... .......... 31% 5.67M 35s
167900K .......... .......... .......... .......... .......... 31% 10.7M 35s
167950K .......... .......... .......... .......... .......... 31%  200K 36s
168000K .......... .......... .......... .......... .......... 31% 4.92M 36s
168050K .......... .......... .......... .......... .......... 31% 16.1M 36s
168100K .......... .......... .......... .......... .......... 31% 15.7M 36s
168150K .......... .......... .......... .......... .......... 31% 11.7M 36s
168200K .......... .......... .......... .......... .......... 31% 14.6M 36s
168250K .......... .......... .......... .......... .......... 31% 16.3M 36s
168300K .......... .......... .......... .......... .......... 31% 18.3M 36s
168350K .......... .......... .......... .......... .......... 31% 12.7M 36s
168400K .......... .......... .......... .......... .......... 31% 12.6M 36s
168450K .......... .......... .......... .......... .......... 31% 13.9M 36s
168500K .......... .......... .......... .......... .......... 31% 8.03M 36s
168550K .......... .......... .......... .......... .......... 31% 11.8M 36s
168600K .......... .......... .......... .......... .......... 31% 7.79M 36s
168650K .......... .......... .......... .......... .......... 31% 6.98M 36s
168700K .......... .......... .......... .......... .......... 31% 5.61M 36s
168750K .......... .......... .......... .......... .......... 31% 7.56M 36s
168800K .......... .......... .......... .......... .......... 31% 4.67M 36s
168850K .......... .......... .......... .......... .......... 31% 5.57M 36s
168900K .......... .......... .......... .......... .......... 31% 6.13M 36s
168950K .......... .......... .......... .......... .......... 31% 4.96M 36s
169000K .......... .......... .......... .......... .......... 31% 7.03M 36s
169050K .......... .......... .......... .......... .......... 31% 41.2M 36s
169100K .......... .......... .......... .......... .......... 31% 14.2M 36s
169150K .......... .......... .......... .......... .......... 31% 14.4M 36s
169200K .......... .......... .......... .......... .......... 31% 11.7M 36s
169250K .......... .......... .......... .......... .......... 31% 17.7M 36s
169300K .......... .......... .......... .......... .......... 31% 8.32M 36s
169350K .......... .......... .......... .......... .......... 31% 6.86M 36s
169400K .......... .......... .......... .......... .......... 31% 7.34M 36s
169450K .......... .......... .......... .......... .......... 31% 6.44M 36s
169500K .......... .......... .......... .......... .......... 31% 5.72M 36s
169550K .......... .......... .......... .......... .......... 31% 5.34M 36s
169600K .......... .......... .......... .......... .......... 31% 7.47M 36s
169650K .......... .......... .......... .......... .......... 31% 6.97M 36s
169700K .......... .......... .......... .......... .......... 31% 9.57M 36s
169750K .......... .......... .......... .......... .......... 31% 9.92M 36s
169800K .......... .......... .......... .......... .......... 31% 9.52M 36s
169850K .......... .......... .......... .......... .......... 31% 9.12M 36s
169900K .......... .......... .......... .......... .......... 31% 9.61M 36s
169950K .......... .......... .......... .......... .......... 31% 8.64M 36s
170000K .......... .......... .......... .......... .......... 31% 21.0M 36s
170050K .......... .......... .......... .......... .......... 31% 30.0M 36s
170100K .......... .......... .......... .......... .......... 31% 16.3M 36s
170150K .......... .......... .......... .......... .......... 31% 19.5M 36s
170200K .......... .......... .......... .......... .......... 31% 15.7M 36s
170250K .......... .......... .......... .......... .......... 31% 9.06M 36s
170300K .......... .......... .......... .......... .......... 31% 39.0M 36s
170350K .......... .......... .......... .......... .......... 31% 15.0M 36s
170400K .......... .......... .......... .......... .......... 31% 15.8M 36s
170450K .......... .......... .......... .......... .......... 31% 12.9M 36s
170500K .......... .......... .......... .......... .......... 31% 16.8M 36s
170550K .......... .......... .......... .......... .......... 31% 15.6M 36s
170600K .......... .......... .......... .......... .......... 31% 9.77M 36s
170650K .......... .......... .......... .......... .......... 31% 14.1M 36s
170700K .......... .......... .......... .......... .......... 31% 9.63M 36s
170750K .......... .......... .......... .......... .......... 31% 11.9M 36s
170800K .......... .......... .......... .......... .......... 31% 7.11M 36s
170850K .......... .......... .......... .......... .......... 31% 3.72M 36s
170900K .......... .......... .......... .......... .......... 31% 4.51M 36s
170950K .......... .......... .......... .......... .......... 31% 3.28M 36s
171000K .......... .......... .......... .......... .......... 31% 3.32M 36s
171050K .......... .......... .......... .......... .......... 31% 6.95M 36s
171100K .......... .......... .......... .......... .......... 31% 4.14M 36s
171150K .......... .......... .......... .......... .......... 31% 6.69M 36s
171200K .......... .......... .......... .......... .......... 31% 5.01M 36s
171250K .......... .......... .......... .......... .......... 31% 6.86M 36s
171300K .......... .......... .......... .......... .......... 31% 5.14M 36s
171350K .......... .......... .......... .......... .......... 31% 5.27M 36s
171400K .......... .......... .......... .......... .......... 31% 5.65M 36s
171450K .......... .......... .......... .......... .......... 31% 4.41M 36s
171500K .......... .......... .......... .......... .......... 31% 6.58M 36s
171550K .......... .......... .......... .......... .......... 31% 13.8M 36s
171600K .......... .......... .......... .......... .......... 31% 16.1M 36s
171650K .......... .......... .......... .......... .......... 31% 19.1M 36s
171700K .......... .......... .......... .......... .......... 31% 16.3M 36s
171750K .......... .......... .......... .......... .......... 31% 18.8M 36s
171800K .......... .......... .......... .......... .......... 31% 15.8M 36s
171850K .......... .......... .......... .......... .......... 31% 15.7M 36s
171900K .......... .......... .......... .......... .......... 31% 22.6M 36s
171950K .......... .......... .......... .......... .......... 32% 19.8M 36s
172000K .......... .......... .......... .......... .......... 32% 16.9M 36s
172050K .......... .......... .......... .......... .......... 32% 16.8M 36s
172100K .......... .......... .......... .......... .......... 32% 23.2M 36s
172150K .......... .......... .......... .......... .......... 32% 15.9M 36s
172200K .......... .......... .......... .......... .......... 32% 17.8M 36s
172250K .......... .......... .......... .......... .......... 32% 14.3M 36s
172300K .......... .......... .......... .......... .......... 32% 18.7M 36s
172350K .......... .......... .......... .......... .......... 32% 8.71M 36s
172400K .......... .......... .......... .......... .......... 32% 10.1M 36s
172450K .......... .......... .......... .......... .......... 32% 7.37M 36s
172500K .......... .......... .......... .......... .......... 32% 10.6M 36s
172550K .......... .......... .......... .......... .......... 32% 11.7M 36s
172600K .......... .......... .......... .......... .......... 32% 10.7M 36s
172650K .......... .......... .......... .......... .......... 32% 10.5M 36s
172700K .......... .......... .......... .......... .......... 32% 7.76M 36s
172750K .......... .......... .......... .......... .......... 32% 16.6M 36s
172800K .......... .......... .......... .......... .......... 32% 13.1M 36s
172850K .......... .......... .......... .......... .......... 32% 21.1M 36s
172900K .......... .......... .......... .......... .......... 32% 36.3M 36s
172950K .......... .......... .......... .......... .......... 32% 32.7M 36s
173000K .......... .......... .......... .......... .......... 32% 13.7M 36s
173050K .......... .......... .......... .......... .......... 32%  103M 36s
173100K .......... .......... .......... .......... .......... 32% 35.8M 36s
173150K .......... .......... .......... .......... .......... 32% 16.2M 36s
173200K .......... .......... .......... .......... .......... 32% 9.26M 36s
173250K .......... .......... .......... .......... .......... 32% 11.8M 36s
173300K .......... .......... .......... .......... .......... 32% 13.6M 36s
173350K .......... .......... .......... .......... .......... 32% 7.59M 36s
173400K .......... .......... .......... .......... .......... 32% 7.75M 36s
173450K .......... .......... .......... .......... .......... 32% 6.60M 36s
173500K .......... .......... .......... .......... .......... 32% 6.56M 36s
173550K .......... .......... .......... .......... .......... 32% 7.45M 36s
173600K .......... .......... .......... .......... .......... 32% 5.68M 36s
173650K .......... .......... .......... .......... .......... 32% 5.02M 36s
173700K .......... .......... .......... .......... .......... 32% 5.21M 36s
173750K .......... .......... .......... .......... .......... 32% 5.13M 36s
173800K .......... .......... .......... .......... .......... 32% 5.16M 36s
173850K .......... .......... .......... .......... .......... 32% 4.53M 36s
173900K .......... .......... .......... .......... .......... 32% 7.18M 36s
173950K .......... .......... .......... .......... .......... 32% 5.78M 36s
174000K .......... .......... .......... .......... .......... 32% 6.47M 36s
174050K .......... .......... .......... .......... .......... 32% 6.42M 36s
174100K .......... .......... .......... .......... .......... 32% 11.4M 36s
174150K .......... .......... .......... .......... .......... 32% 17.8M 36s
174200K .......... .......... .......... .......... .......... 32% 8.82M 36s
174250K .......... .......... .......... .......... .......... 32% 11.4M 36s
174300K .......... .......... .......... .......... .......... 32% 11.6M 36s
174350K .......... .......... .......... .......... .......... 32% 10.3M 36s
174400K .......... .......... .......... .......... .......... 32% 11.0M 36s
174450K .......... .......... .......... .......... .......... 32% 11.9M 36s
174500K .......... .......... .......... .......... .......... 32% 11.5M 36s
174550K .......... .......... .......... .......... .......... 32% 11.8M 36s
174600K .......... .......... .......... .......... .......... 32% 16.6M 36s
174650K .......... .......... .......... .......... .......... 32% 28.5M 35s
174700K .......... .......... .......... .......... .......... 32% 16.4M 35s
174750K .......... .......... .......... .......... .......... 32% 18.5M 35s
174800K .......... .......... .......... .......... .......... 32% 27.8M 35s
174850K .......... .......... .......... .......... .......... 32% 16.2M 35s
174900K .......... .......... .......... .......... .......... 32% 16.3M 35s
174950K .......... .......... .......... .......... .......... 32% 10.2M 35s
175000K .......... .......... .......... .......... .......... 32% 13.5M 35s
175050K .......... .......... .......... .......... .......... 32% 10.9M 35s
175100K .......... .......... .......... .......... .......... 32% 10.0M 35s
175150K .......... .......... .......... .......... .......... 32% 7.58M 35s
175200K .......... .......... .......... .......... .......... 32% 16.7M 35s
175250K .......... .......... .......... .......... .......... 32% 11.6M 35s
175300K .......... .......... .......... .......... .......... 32% 7.11M 35s
175350K .......... .......... .......... .......... .......... 32% 9.50M 35s
175400K .......... .......... .......... .......... .......... 32% 6.92M 35s
175450K .......... .......... .......... .......... .......... 32% 13.8M 35s
175500K .......... .......... .......... .......... .......... 32% 10.9M 35s
175550K .......... .......... .......... .......... .......... 32% 7.70M 35s
175600K .......... .......... .......... .......... .......... 32% 7.30M 35s
175650K .......... .......... .......... .......... .......... 32% 9.72M 35s
175700K .......... .......... .......... .......... .......... 32% 6.99M 35s
175750K .......... .......... .......... .......... .......... 32% 9.01M 35s
175800K .......... .......... .......... .......... .......... 32% 7.70M 35s
175850K .......... .......... .......... .......... .......... 32% 5.05M 35s
175900K .......... .......... .......... .......... .......... 32% 5.23M 35s
175950K .......... .......... .......... .......... .......... 32% 7.68M 35s
176000K .......... .......... .......... .......... .......... 32% 6.73M 35s
176050K .......... .......... .......... .......... .......... 32% 11.7M 35s
176100K .......... .......... .......... .......... .......... 32% 5.90M 35s
176150K .......... .......... .......... .......... .......... 32% 5.85M 35s
176200K .......... .......... .......... .......... .......... 32% 5.39M 35s
176250K .......... .......... .......... .......... .......... 32% 4.26M 35s
176300K .......... .......... .......... .......... .......... 32% 3.67M 35s
176350K .......... .......... .......... .......... .......... 32% 2.95M 35s
176400K .......... .......... .......... .......... .......... 32% 4.97M 35s
176450K .......... .......... .......... .......... .......... 32% 4.01M 35s
176500K .......... .......... .......... .......... .......... 32% 5.66M 35s
176550K .......... .......... .......... .......... .......... 32% 10.7M 35s
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176650K .......... .......... .......... .......... .......... 32% 23.8M 35s
176700K .......... .......... .......... .......... .......... 32% 12.6M 35s
176750K .......... .......... .......... .......... .......... 32% 13.9M 35s
176800K .......... .......... .......... .......... .......... 32% 19.2M 35s
176850K .......... .......... .......... .......... .......... 32% 11.7M 35s
176900K .......... .......... .......... .......... .......... 32% 12.6M 35s
176950K .......... .......... .......... .......... .......... 32% 10.0M 35s
177000K .......... .......... .......... .......... .......... 32% 11.8M 35s
177050K .......... .......... .......... .......... .......... 32% 14.5M 35s
177100K .......... .......... .......... .......... .......... 32% 9.89M 35s
177150K .......... .......... .......... .......... .......... 32% 14.6M 35s
177200K .......... .......... .......... .......... .......... 32% 13.0M 35s
177250K .......... .......... .......... .......... .......... 32% 8.93M 35s
177300K .......... .......... .......... .......... .......... 33% 17.0M 35s
177350K .......... .......... .......... .......... .......... 33% 15.7M 35s
177400K .......... .......... .......... .......... .......... 33% 11.0M 35s
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177750K .......... .......... .......... .......... .......... 33% 94.3M 35s
177800K .......... .......... .......... .......... .......... 33% 29.9M 35s
177850K .......... .......... .......... .......... .......... 33% 6.92M 35s
177900K .......... .......... .......... .......... .......... 33% 11.3M 35s
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178000K .......... .......... .......... .......... .......... 33% 11.5M 35s
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178100K .......... .......... .......... .......... .......... 33% 9.31M 35s
178150K .......... .......... .......... .......... .......... 33% 10.7M 35s
178200K .......... .......... .......... .......... .......... 33% 8.88M 35s
178250K .......... .......... .......... .......... .......... 33% 18.9M 35s
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178800K .......... .......... .......... .......... .......... 33% 13.9M 35s
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179000K .......... .......... .......... .......... .......... 33% 8.93M 35s
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179100K .......... .......... .......... .......... .......... 33% 10.6M 35s
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179200K .......... .......... .......... .......... .......... 33% 8.11M 35s
179250K .......... .......... .......... .......... .......... 33% 9.30M 35s
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180000K .......... .......... .......... .......... .......... 33% 10.2M 35s
180050K .......... .......... .......... .......... .......... 33% 23.6M 35s
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180200K .......... .......... .......... .......... .......... 33% 17.6M 35s
180250K .......... .......... .......... .......... .......... 33% 29.2M 35s
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181000K .......... .......... .......... .......... .......... 33% 12.4M 35s
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181100K .......... .......... .......... .......... .......... 33% 5.95M 35s
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181400K .......... .......... .......... .......... .......... 33% 12.9M 35s
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182000K .......... .......... .......... .......... .......... 33% 21.8M 35s
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182150K .......... .......... .......... .......... .......... 33% 43.6M 35s
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182250K .......... .......... .......... .......... .......... 33% 21.0M 35s
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182500K .......... .......... .......... .......... .......... 33% 13.9M 35s
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183000K .......... .......... .......... .......... .......... 34% 6.08M 35s
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183150K .......... .......... .......... .......... .......... 34% 17.8M 35s
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183250K .......... .......... .......... .......... .......... 34% 23.8M 35s
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186100K .......... .......... .......... .......... .......... 34% 6.36M 34s
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186250K .......... .......... .......... .......... .......... 34% 7.24M 34s
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187000K .......... .......... .......... .......... .......... 34% 11.5M 34s
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187100K .......... .......... .......... .......... .......... 34% 10.0M 34s
187150K .......... .......... .......... .......... .......... 34% 12.5M 34s
187200K .......... .......... .......... .......... .......... 34% 8.55M 34s
187250K .......... .......... .......... .......... .......... 34% 9.80M 34s
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188000K .......... .......... .......... .......... .......... 34% 49.4M 34s
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188100K .......... .......... .......... .......... .......... 35% 14.4M 34s
188150K .......... .......... .......... .......... .......... 35% 10.9M 34s
188200K .......... .......... .......... .......... .......... 35% 9.85M 34s
188250K .......... .......... .......... .......... .......... 35% 13.6M 34s
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188600K .......... .......... .......... .......... .......... 35%  227K 35s
188650K .......... .......... .......... .......... .......... 35% 4.38M 35s
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189000K .......... .......... .......... .......... .......... 35% 18.3M 35s
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189100K .......... .......... .......... .......... .......... 35% 21.0M 34s
189150K .......... .......... .......... .......... .......... 35% 20.3M 34s
189200K .......... .......... .......... .......... .......... 35% 12.9M 34s
189250K .......... .......... .......... .......... .......... 35% 14.8M 34s
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189500K .......... .......... .......... .......... .......... 35% 11.1M 34s
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189650K .......... .......... .......... .......... .......... 35% 10.6M 34s
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189800K .......... .......... .......... .......... .......... 35% 12.7M 34s
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189900K .......... .......... .......... .......... .......... 35% 14.9M 34s
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190000K .......... .......... .......... .......... .......... 35% 8.02M 34s
190050K .......... .......... .......... .......... .......... 35% 6.00M 34s
190100K .......... .......... .......... .......... .......... 35% 5.96M 34s
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190200K .......... .......... .......... .......... .......... 35% 5.50M 34s
190250K .......... .......... .......... .......... .......... 35% 6.61M 34s
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190350K .......... .......... .......... .......... .......... 35% 22.5M 34s
190400K .......... .......... .......... .......... .......... 35% 27.6M 34s
190450K .......... .......... .......... .......... .......... 35% 23.3M 34s
190500K .......... .......... .......... .......... .......... 35% 24.7M 34s
190550K .......... .......... .......... .......... .......... 35% 25.6M 34s
190600K .......... .......... .......... .......... .......... 35% 17.3M 34s
190650K .......... .......... .......... .......... .......... 35% 23.5M 34s
190700K .......... .......... .......... .......... .......... 35% 17.0M 34s
190750K .......... .......... .......... .......... .......... 35% 14.1M 34s
190800K .......... .......... .......... .......... .......... 35% 18.2M 34s
190850K .......... .......... .......... .......... .......... 35% 12.0M 34s
190900K .......... .......... .......... .......... .......... 35% 14.5M 34s
190950K .......... .......... .......... .......... .......... 35% 15.0M 34s
191000K .......... .......... .......... .......... .......... 35% 20.5M 34s
191050K .......... .......... .......... .......... .......... 35% 17.3M 34s
191100K .......... .......... .......... .......... .......... 35% 14.6M 34s
191150K .......... .......... .......... .......... .......... 35% 15.4M 34s
191200K .......... .......... .......... .......... .......... 35% 12.3M 34s
191250K .......... .......... .......... .......... .......... 35% 10.3M 34s
191300K .......... .......... .......... .......... .......... 35% 15.4M 34s
191350K .......... .......... .......... .......... .......... 35% 10.4M 34s
191400K .......... .......... .......... .......... .......... 35% 13.5M 34s
191450K .......... .......... .......... .......... .......... 35% 18.6M 34s
191500K .......... .......... .......... .......... .......... 35% 24.4M 34s
191550K .......... .......... .......... .......... .......... 35% 21.0M 34s
191600K .......... .......... .......... .......... .......... 35% 16.5M 34s
191650K .......... .......... .......... .......... .......... 35% 10.0M 34s
191700K .......... .......... .......... .......... .......... 35% 12.8M 34s
191750K .......... .......... .......... .......... .......... 35% 9.99M 34s
191800K .......... .......... .......... .......... .......... 35% 11.9M 34s
191850K .......... .......... .......... .......... .......... 35% 9.55M 34s
191900K .......... .......... .......... .......... .......... 35% 9.72M 34s
191950K .......... .......... .......... .......... .......... 35% 11.4M 34s
192000K .......... .......... .......... .......... .......... 35% 10.8M 34s
192050K .......... .......... .......... .......... .......... 35% 13.3M 34s
192100K .......... .......... .......... .......... .......... 35% 13.6M 34s
192150K .......... .......... .......... .......... .......... 35% 14.5M 34s
192200K .......... .......... .......... .......... .......... 35% 10.3M 34s
192250K .......... .......... .......... .......... .......... 35% 10.5M 34s
192300K .......... .......... .......... .......... .......... 35% 8.50M 34s
192350K .......... .......... .......... .......... .......... 35% 7.41M 34s
192400K .......... .......... .......... .......... .......... 35% 9.30M 34s
192450K .......... .......... .......... .......... .......... 35% 8.19M 34s
192500K .......... .......... .......... .......... .......... 35% 8.80M 34s
192550K .......... .......... .......... .......... .......... 35% 12.5M 34s
192600K .......... .......... .......... .......... .......... 35% 22.3M 34s
192650K .......... .......... .......... .......... .......... 35% 16.3M 34s
192700K .......... .......... .......... .......... .......... 35% 15.5M 34s
192750K .......... .......... .......... .......... .......... 35% 12.3M 34s
192800K .......... .......... .......... .......... .......... 35% 18.1M 34s
192850K .......... .......... .......... .......... .......... 35% 11.3M 34s
192900K .......... .......... .......... .......... .......... 35% 11.4M 34s
192950K .......... .......... .......... .......... .......... 35% 9.08M 34s
193000K .......... .......... .......... .......... .......... 35% 11.6M 34s
193050K .......... .......... .......... .......... .......... 35% 10.3M 34s
193100K .......... .......... .......... .......... .......... 35% 10.1M 34s
193150K .......... .......... .......... .......... .......... 35% 9.56M 34s
193200K .......... .......... .......... .......... .......... 35% 10.4M 34s
193250K .......... .......... .......... .......... .......... 35% 15.5M 34s
193300K .......... .......... .......... .......... .......... 35% 16.2M 34s
193350K .......... .......... .......... .......... .......... 35% 19.8M 34s
193400K .......... .......... .......... .......... .......... 35% 17.1M 34s
193450K .......... .......... .......... .......... .......... 36% 7.47M 34s
193500K .......... .......... .......... .......... .......... 36% 18.1M 34s
193550K .......... .......... .......... .......... .......... 36% 14.5M 34s
193600K .......... .......... .......... .......... .......... 36% 6.99M 34s
193650K .......... .......... .......... .......... .......... 36% 7.67M 34s
193700K .......... .......... .......... .......... .......... 36% 6.17M 34s
193750K .......... .......... .......... .......... .......... 36% 10.6M 34s
193800K .......... .......... .......... .......... .......... 36% 9.24M 34s
193850K .......... .......... .......... .......... .......... 36% 8.34M 34s
193900K .......... .......... .......... .......... .......... 36% 9.84M 34s
193950K .......... .......... .......... .......... .......... 36% 6.32M 34s
194000K .......... .......... .......... .......... .......... 36% 6.78M 34s
194050K .......... .......... .......... .......... .......... 36% 13.5M 34s
194100K .......... .......... .......... .......... .......... 36% 11.1M 34s
194150K .......... .......... .......... .......... .......... 36% 7.94M 34s
194200K .......... .......... .......... .......... .......... 36% 8.95M 34s
194250K .......... .......... .......... .......... .......... 36% 10.6M 34s
194300K .......... .......... .......... .......... .......... 36% 9.61M 34s
194350K .......... .......... .......... .......... .......... 36% 10.4M 34s
194400K .......... .......... .......... .......... .......... 36% 11.1M 34s
194450K .......... .......... .......... .......... .......... 36% 5.88M 34s
194500K .......... .......... .......... .......... .......... 36% 5.79M 34s
194550K .......... .......... .......... .......... .......... 36% 8.88M 34s
194600K .......... .......... .......... .......... .......... 36% 7.17M 34s
194650K .......... .......... .......... .......... .......... 36% 6.90M 34s
194700K .......... .......... .......... .......... .......... 36% 6.06M 34s
194750K .......... .......... .......... .......... .......... 36% 6.19M 34s
194800K .......... .......... .......... .......... .......... 36% 7.39M 34s
194850K .......... .......... .......... .......... .......... 36% 6.57M 34s
194900K .......... .......... .......... .......... .......... 36% 5.83M 34s
194950K .......... .......... .......... .......... .......... 36% 5.45M 34s
195000K .......... .......... .......... .......... .......... 36% 3.33M 34s
195050K .......... .......... .......... .......... .......... 36% 4.12M 34s
195100K .......... .......... .......... .......... .......... 36% 4.27M 34s
195150K .......... .......... .......... .......... .......... 36% 10.6M 34s
195200K .......... .......... .......... .......... .......... 36% 13.0M 34s
195250K .......... .......... .......... .......... .......... 36% 17.1M 34s
195300K .......... .......... .......... .......... .......... 36% 25.3M 34s
195350K .......... .......... .......... .......... .......... 36% 16.6M 34s
195400K .......... .......... .......... .......... .......... 36% 18.7M 34s
195450K .......... .......... .......... .......... .......... 36% 11.7M 34s
195500K .......... .......... .......... .......... .......... 36% 12.1M 34s
195550K .......... .......... .......... .......... .......... 36% 14.1M 34s
195600K .......... .......... .......... .......... .......... 36% 13.1M 34s
195650K .......... .......... .......... .......... .......... 36% 13.8M 34s
195700K .......... .......... .......... .......... .......... 36% 11.6M 34s
195750K .......... .......... .......... .......... .......... 36% 13.5M 34s
195800K .......... .......... .......... .......... .......... 36% 13.4M 34s
195850K .......... .......... .......... .......... .......... 36% 9.54M 34s
195900K .......... .......... .......... .......... .......... 36% 12.6M 34s
195950K .......... .......... .......... .......... .......... 36% 7.53M 34s
196000K .......... .......... .......... .......... .......... 36% 8.88M 34s
196050K .......... .......... .......... .......... .......... 36% 10.2M 34s
196100K .......... .......... .......... .......... .......... 36% 7.31M 34s
196150K .......... .......... .......... .......... .......... 36% 11.3M 34s
196200K .......... .......... .......... .......... .......... 36% 9.34M 34s
196250K .......... .......... .......... .......... .......... 36% 9.24M 34s
196300K .......... .......... .......... .......... .......... 36% 10.3M 34s
196350K .......... .......... .......... .......... .......... 36% 7.58M 34s
196400K .......... .......... .......... .......... .......... 36% 35.7M 34s
196450K .......... .......... .......... .......... .......... 36% 26.2M 34s
196500K .......... .......... .......... .......... .......... 36% 44.3M 34s
196550K .......... .......... .......... .......... .......... 36% 33.9M 34s
196600K .......... .......... .......... .......... .......... 36% 32.6M 34s
196650K .......... .......... .......... .......... .......... 36% 22.1M 34s
196700K .......... .......... .......... .......... .......... 36% 34.7M 34s
196750K .......... .......... .......... .......... .......... 36% 30.2M 34s
196800K .......... .......... .......... .......... .......... 36% 25.6M 34s
196850K .......... .......... .......... .......... .......... 36% 24.1M 34s
196900K .......... .......... .......... .......... .......... 36% 26.7M 34s
196950K .......... .......... .......... .......... .......... 36% 37.1M 34s
197000K .......... .......... .......... .......... .......... 36% 30.8M 34s
197050K .......... .......... .......... .......... .......... 36% 22.3M 34s
197100K .......... .......... .......... .......... .......... 36% 23.0M 34s
197150K .......... .......... .......... .......... .......... 36% 22.7M 34s
197200K .......... .......... .......... .......... .......... 36% 22.3M 34s
197250K .......... .......... .......... .......... .......... 36% 26.4M 34s
197300K .......... .......... .......... .......... .......... 36% 18.3M 34s
197350K .......... .......... .......... .......... .......... 36% 13.4M 34s
197400K .......... .......... .......... .......... .......... 36% 11.7M 34s
197450K .......... .......... .......... .......... .......... 36% 8.02M 34s
197500K .......... .......... .......... .......... .......... 36% 10.2M 34s
197550K .......... .......... .......... .......... .......... 36% 11.1M 34s
197600K .......... .......... .......... .......... .......... 36% 8.82M 34s
197650K .......... .......... .......... .......... .......... 36% 9.51M 33s
197700K .......... .......... .......... .......... .......... 36% 9.85M 33s
197750K .......... .......... .......... .......... .......... 36% 16.4M 33s
197800K .......... .......... .......... .......... .......... 36% 28.8M 33s
197850K .......... .......... .......... .......... .......... 36% 15.0M 33s
197900K .......... .......... .......... .......... .......... 36% 24.2M 33s
197950K .......... .......... .......... .......... .......... 36% 12.6M 33s
198000K .......... .......... .......... .......... .......... 36% 33.3M 33s
198050K .......... .......... .......... .......... .......... 36% 13.9M 33s
198100K .......... .......... .......... .......... .......... 36% 15.6M 33s
198150K .......... .......... .......... .......... .......... 36% 16.1M 33s
198200K .......... .......... .......... .......... .......... 36% 15.8M 33s
198250K .......... .......... .......... .......... .......... 36% 16.3M 33s
198300K .......... .......... .......... .......... .......... 36% 12.3M 33s
198350K .......... .......... .......... .......... .......... 36% 9.28M 33s
198400K .......... .......... .......... .......... .......... 36% 8.87M 33s
198450K .......... .......... .......... .......... .......... 36% 6.99M 33s
198500K .......... .......... .......... .......... .......... 36% 8.99M 33s
198550K .......... .......... .......... .......... .......... 36% 5.61M 33s
198600K .......... .......... .......... .......... .......... 36% 5.05M 33s
198650K .......... .......... .......... .......... .......... 36% 4.29M 33s
198700K .......... .......... .......... .......... .......... 36% 7.80M 33s
198750K .......... .......... .......... .......... .......... 36% 12.6M 33s
198800K .......... .......... .......... .......... .......... 37% 14.2M 33s
198850K .......... .......... .......... .......... .......... 37% 11.6M 33s
198900K .......... .......... .......... .......... .......... 37% 14.4M 33s
198950K .......... .......... .......... .......... .......... 37% 8.66M 33s
199000K .......... .......... .......... .......... .......... 37% 8.19M 33s
199050K .......... .......... .......... .......... .......... 37% 6.89M 33s
199100K .......... .......... .......... .......... .......... 37% 5.04M 33s
199150K .......... .......... .......... .......... .......... 37% 7.96M 33s
199200K .......... .......... .......... .......... .......... 37% 5.16M 33s
199250K .......... .......... .......... .......... .......... 37% 7.94M 33s
199300K .......... .......... .......... .......... .......... 37% 9.86M 33s
199350K .......... .......... .......... .......... .......... 37% 20.1M 33s
199400K .......... .......... .......... .......... .......... 37% 10.6M 33s
199450K .......... .......... .......... .......... .......... 37% 9.78M 33s
199500K .......... .......... .......... .......... .......... 37% 14.6M 33s
199550K .......... .......... .......... .......... .......... 37% 15.1M 33s
199600K .......... .......... .......... .......... .......... 37% 10.4M 33s
199650K .......... .......... .......... .......... .......... 37% 13.0M 33s
199700K .......... .......... .......... .......... .......... 37% 12.1M 33s
199750K .......... .......... .......... .......... .......... 37% 13.7M 33s
199800K .......... .......... .......... .......... .......... 37% 12.7M 33s
199850K .......... .......... .......... .......... .......... 37% 14.5M 33s
199900K .......... .......... .......... .......... .......... 37% 14.1M 33s
199950K .......... .......... .......... .......... .......... 37% 10.5M 33s
200000K .......... .......... .......... .......... .......... 37% 12.0M 33s
200050K .......... .......... .......... .......... .......... 37% 10.5M 33s
200100K .......... .......... .......... .......... .......... 37% 7.06M 33s
200150K .......... .......... .......... .......... .......... 37% 37.0M 33s
200200K .......... .......... .......... .......... .......... 37% 14.6M 33s
200250K .......... .......... .......... .......... .......... 37% 12.7M 33s
200300K .......... .......... .......... .......... .......... 37% 11.9M 33s
200350K .......... .......... .......... .......... .......... 37% 8.29M 33s
200400K .......... .......... .......... .......... .......... 37% 8.81M 33s
200450K .......... .......... .......... .......... .......... 37% 7.72M 33s
200500K .......... .......... .......... .......... .......... 37% 7.63M 33s
200550K .......... .......... .......... .......... .......... 37% 5.48M 33s
200600K .......... .......... .......... .......... .......... 37% 4.65M 33s
200650K .......... .......... .......... .......... .......... 37% 5.22M 33s
200700K .......... .......... .......... .......... .......... 37% 4.49M 33s
200750K .......... .......... .......... .......... .......... 37% 8.79M 33s
200800K .......... .......... .......... .......... .......... 37% 23.2M 33s
200850K .......... .......... .......... .......... .......... 37% 16.4M 33s
200900K .......... .......... .......... .......... .......... 37% 22.8M 33s
200950K .......... .......... .......... .......... .......... 37%  140M 33s
201000K .......... .......... .......... .......... .......... 37% 44.6M 33s
201050K .......... .......... .......... .......... .......... 37% 32.9M 33s
201100K .......... .......... .......... .......... .......... 37% 26.1M 33s
201150K .......... .......... .......... .......... .......... 37% 34.3M 33s
201200K .......... .......... .......... .......... .......... 37% 27.1M 33s
201250K .......... .......... .......... .......... .......... 37% 26.9M 33s
201300K .......... .......... .......... .......... .......... 37% 32.3M 33s
201350K .......... .......... .......... .......... .......... 37% 14.5M 33s
201400K .......... .......... .......... .......... .......... 37% 38.5M 33s
201450K .......... .......... .......... .......... .......... 37% 13.8M 33s
201500K .......... .......... .......... .......... .......... 37% 22.2M 33s
201550K .......... .......... .......... .......... .......... 37% 13.1M 33s
201600K .......... .......... .......... .......... .......... 37% 14.0M 33s
201650K .......... .......... .......... .......... .......... 37% 11.4M 33s
201700K .......... .......... .......... .......... .......... 37% 9.97M 33s
201750K .......... .......... .......... .......... .......... 37% 10.6M 33s
201800K .......... .......... .......... .......... .......... 37% 13.5M 33s
201850K .......... .......... .......... .......... .......... 37% 8.99M 33s
201900K .......... .......... .......... .......... .......... 37% 9.06M 33s
201950K .......... .......... .......... .......... .......... 37% 8.40M 33s
202000K .......... .......... .......... .......... .......... 37% 8.47M 33s
202050K .......... .......... .......... .......... .......... 37% 8.08M 33s
202100K .......... .......... .......... .......... .......... 37% 8.42M 33s
202150K .......... .......... .......... .......... .......... 37% 8.91M 33s
202200K .......... .......... .......... .......... .......... 37% 11.0M 33s
202250K .......... .......... .......... .......... .......... 37% 72.6M 33s
202300K .......... .......... .......... .......... .......... 37% 20.0M 33s
202350K .......... .......... .......... .......... .......... 37% 19.7M 33s
202400K .......... .......... .......... .......... .......... 37% 16.3M 33s
202450K .......... .......... .......... .......... .......... 37% 13.7M 33s
202500K .......... .......... .......... .......... .......... 37% 19.7M 33s
202550K .......... .......... .......... .......... .......... 37% 14.1M 33s
202600K .......... .......... .......... .......... .......... 37% 9.41M 33s
202650K .......... .......... .......... .......... .......... 37% 9.80M 33s
202700K .......... .......... .......... .......... .......... 37% 8.53M 33s
202750K .......... .......... .......... .......... .......... 37% 11.6M 33s
202800K .......... .......... .......... .......... .......... 37% 14.2M 33s
202850K .......... .......... .......... .......... .......... 37% 9.25M 33s
202900K .......... .......... .......... .......... .......... 37% 8.16M 33s
202950K .......... .......... .......... .......... .......... 37% 8.38M 33s
203000K .......... .......... .......... .......... .......... 37% 7.30M 33s
203050K .......... .......... .......... .......... .......... 37% 7.19M 33s
203100K .......... .......... .......... .......... .......... 37% 6.40M 33s
203150K .......... .......... .......... .......... .......... 37% 6.96M 33s
203200K .......... .......... .......... .......... .......... 37% 5.93M 33s
203250K .......... .......... .......... .......... .......... 37% 8.52M 33s
203300K .......... .......... .......... .......... .......... 37% 17.5M 33s
203350K .......... .......... .......... .......... .......... 37% 19.9M 33s
203400K .......... .......... .......... .......... .......... 37% 16.4M 33s
203450K .......... .......... .......... .......... .......... 37% 7.62M 33s
203500K .......... .......... .......... .......... .......... 37% 13.1M 33s
203550K .......... .......... .......... .......... .......... 37% 7.59M 33s
203600K .......... .......... .......... .......... .......... 37% 7.24M 33s
203650K .......... .......... .......... .......... .......... 37% 7.35M 33s
203700K .......... .......... .......... .......... .......... 37% 5.80M 33s
203750K .......... .......... .......... .......... .......... 37% 6.77M 33s
203800K .......... .......... .......... .......... .......... 37% 4.32M 33s
203850K .......... .......... .......... .......... .......... 37% 4.50M 33s
203900K .......... .......... .......... .......... .......... 37% 4.58M 33s
203950K .......... .......... .......... .......... .......... 37% 5.57M 33s
204000K .......... .......... .......... .......... .......... 37% 14.0M 33s
204050K .......... .......... .......... .......... .......... 37% 14.3M 33s
204100K .......... .......... .......... .......... .......... 37% 10.9M 33s
204150K .......... .......... .......... .......... .......... 37% 6.14M 33s
204200K .......... .......... .......... .......... .......... 38% 6.99M 33s
204250K .......... .......... .......... .......... .......... 38% 8.87M 33s
204300K .......... .......... .......... .......... .......... 38% 6.70M 33s
204350K .......... .......... .......... .......... .......... 38% 5.68M 33s
204400K .......... .......... .......... .......... .......... 38% 5.34M 33s
204450K .......... .......... .......... .......... .......... 38% 3.95M 33s
204500K .......... .......... .......... .......... .......... 38% 4.29M 33s
204550K .......... .......... .......... .......... .......... 38% 7.19M 33s
204600K .......... .......... .......... .......... .......... 38% 4.75M 33s
204650K .......... .......... .......... .......... .......... 38% 7.40M 33s
204700K .......... .......... .......... .......... .......... 38% 13.8M 33s
204750K .......... .......... .......... .......... .......... 38% 22.5M 33s
204800K .......... .......... .......... .......... .......... 38% 23.7M 33s
204850K .......... .......... .......... .......... .......... 38% 17.4M 33s
204900K .......... .......... .......... .......... .......... 38% 28.5M 33s
204950K .......... .......... .......... .......... .......... 38% 15.8M 33s
205000K .......... .......... .......... .......... .......... 38% 19.8M 33s
205050K .......... .......... .......... .......... .......... 38% 24.6M 33s
205100K .......... .......... .......... .......... .......... 38% 15.3M 33s
205150K .......... .......... .......... .......... .......... 38% 21.6M 33s
205200K .......... .......... .......... .......... .......... 38% 6.76M 33s
205250K .......... .......... .......... .......... .......... 38% 5.80M 33s
205300K .......... .......... .......... .......... .......... 38% 7.60M 33s
205350K .......... .......... .......... .......... .......... 38% 6.05M 33s
205400K .......... .......... .......... .......... .......... 38% 7.39M 33s
205450K .......... .......... .......... .......... .......... 38% 3.06M 33s
205500K .......... .......... .......... .......... .......... 38% 3.21M 33s
205550K .......... .......... .......... .......... .......... 38% 4.19M 33s
205600K .......... .......... .......... .......... .......... 38% 3.06M 33s
205650K .......... .......... .......... .......... .......... 38% 4.10M 33s
205700K .......... .......... .......... .......... .......... 38% 3.39M 33s
205750K .......... .......... .......... .......... .......... 38% 14.8M 33s
205800K .......... .......... .......... .......... .......... 38% 22.5M 33s
205850K .......... .......... .......... .......... .......... 38% 14.7M 33s
205900K .......... .......... .......... .......... .......... 38% 16.4M 33s
205950K .......... .......... .......... .......... .......... 38% 13.9M 33s
206000K .......... .......... .......... .......... .......... 38% 14.4M 33s
206050K .......... .......... .......... .......... .......... 38% 17.3M 33s
206100K .......... .......... .......... .......... .......... 38% 10.0M 33s
206150K .......... .......... .......... .......... .......... 38% 9.12M 33s
206200K .......... .......... .......... .......... .......... 38% 7.69M 33s
206250K .......... .......... .......... .......... .......... 38% 10.1M 33s
206300K .......... .......... .......... .......... .......... 38% 9.85M 33s
206350K .......... .......... .......... .......... .......... 38% 8.87M 33s
206400K .......... .......... .......... .......... .......... 38% 8.15M 33s
206450K .......... .......... .......... .......... .......... 38% 8.70M 33s
206500K .......... .......... .......... .......... .......... 38% 14.0M 33s
206550K .......... .......... .......... .......... .......... 38% 9.05M 33s
206600K .......... .......... .......... .......... .......... 38% 5.71M 33s
206650K .......... .......... .......... .......... .......... 38% 8.23M 33s
206700K .......... .......... .......... .......... .......... 38% 5.77M 33s
206750K .......... .......... .......... .......... .......... 38% 8.32M 33s
206800K .......... .......... .......... .......... .......... 38% 7.24M 33s
206850K .......... .......... .......... .......... .......... 38% 9.83M 33s
206900K .......... .......... .......... .......... .......... 38% 14.7M 33s
206950K .......... .......... .......... .......... .......... 38% 70.5M 33s
207000K .......... .......... .......... .......... .......... 38% 19.0M 33s
207050K .......... .......... .......... .......... .......... 38% 16.0M 33s
207100K .......... .......... .......... .......... .......... 38% 29.9M 33s
207150K .......... .......... .......... .......... .......... 38% 14.8M 33s
207200K .......... .......... .......... .......... .......... 38% 9.95M 33s
207250K .......... .......... .......... .......... .......... 38% 11.6M 33s
207300K .......... .......... .......... .......... .......... 38% 5.68M 33s
207350K .......... .......... .......... .......... .......... 38% 5.53M 33s
207400K .......... .......... .......... .......... .......... 38% 7.83M 33s
207450K .......... .......... .......... .......... .......... 38% 6.56M 33s
207500K .......... .......... .......... .......... .......... 38% 4.67M 33s
207550K .......... .......... .......... .......... .......... 38% 4.06M 33s
207600K .......... .......... .......... .......... .......... 38% 2.70M 33s
207650K .......... .......... .......... .......... .......... 38% 10.1M 33s
207700K .......... .......... .......... .......... .......... 38% 5.96M 33s
207750K .......... .......... .......... .......... .......... 38% 5.82M 33s
207800K .......... .......... .......... .......... .......... 38% 7.41M 33s
207850K .......... .......... .......... .......... .......... 38% 5.46M 33s
207900K .......... .......... .......... .......... .......... 38% 35.1M 33s
207950K .......... .......... .......... .......... .......... 38% 23.3M 33s
208000K .......... .......... .......... .......... .......... 38% 18.4M 33s
208050K .......... .......... .......... .......... .......... 38% 15.0M 33s
208100K .......... .......... .......... .......... .......... 38% 10.3M 33s
208150K .......... .......... .......... .......... .......... 38% 17.9M 33s
208200K .......... .......... .......... .......... .......... 38% 4.89M 33s
208250K .......... .......... .......... .......... .......... 38% 5.54M 33s
208300K .......... .......... .......... .......... .......... 38% 4.56M 33s
208350K .......... .......... .......... .......... .......... 38%  224K 33s
208400K .......... .......... .......... .......... .......... 38% 5.27M 33s
208450K .......... .......... .......... .......... .......... 38% 9.73M 33s
208500K .......... .......... .......... .......... .......... 38% 10.7M 33s
208550K .......... .......... .......... .......... .......... 38% 13.8M 33s
208600K .......... .......... .......... .......... .......... 38% 9.85M 33s
208650K .......... .......... .......... .......... .......... 38% 10.4M 33s
208700K .......... .......... .......... .......... .......... 38% 10.7M 33s
208750K .......... .......... .......... .......... .......... 38% 13.1M 33s
208800K .......... .......... .......... .......... .......... 38% 11.9M 33s
208850K .......... .......... .......... .......... .......... 38% 7.90M 33s
208900K .......... .......... .......... .......... .......... 38% 11.0M 33s
208950K .......... .......... .......... .......... .......... 38% 9.88M 33s
209000K .......... .......... .......... .......... .......... 38% 11.3M 33s
209050K .......... .......... .......... .......... .......... 38% 9.64M 33s
209100K .......... .......... .......... .......... .......... 38% 9.74M 33s
209150K .......... .......... .......... .......... .......... 38% 11.9M 33s
209200K .......... .......... .......... .......... .......... 38% 9.52M 33s
209250K .......... .......... .......... .......... .......... 38% 9.55M 33s
209300K .......... .......... .......... .......... .......... 38% 9.77M 33s
209350K .......... .......... .......... .......... .......... 38% 9.22M 33s
209400K .......... .......... .......... .......... .......... 38% 11.1M 33s
209450K .......... .......... .......... .......... .......... 38% 7.55M 33s
209500K .......... .......... .......... .......... .......... 38% 7.41M 33s
209550K .......... .......... .......... .......... .......... 39% 8.13M 33s
209600K .......... .......... .......... .......... .......... 39% 5.54M 33s
209650K .......... .......... .......... .......... .......... 39% 5.31M 33s
209700K .......... .......... .......... .......... .......... 39% 4.47M 33s
209750K .......... .......... .......... .......... .......... 39% 5.95M 33s
209800K .......... .......... .......... .......... .......... 39% 4.81M 33s
209850K .......... .......... .......... .......... .......... 39% 3.27M 33s
209900K .......... .......... .......... .......... .......... 39% 6.63M 33s
209950K .......... .......... .......... .......... .......... 39% 7.20M 33s
210000K .......... .......... .......... .......... .......... 39% 11.2M 33s
210050K .......... .......... .......... .......... .......... 39% 8.67M 33s
210100K .......... .......... .......... .......... .......... 39% 5.66M 33s
210150K .......... .......... .......... .......... .......... 39% 8.40M 33s
210200K .......... .......... .......... .......... .......... 39% 6.04M 33s
210250K .......... .......... .......... .......... .......... 39% 7.15M 33s
210300K .......... .......... .......... .......... .......... 39% 8.46M 33s
210350K .......... .......... .......... .......... .......... 39% 5.77M 33s
210400K .......... .......... .......... .......... .......... 39% 6.67M 33s
210450K .......... .......... .......... .......... .......... 39% 5.49M 33s
210500K .......... .......... .......... .......... .......... 39% 7.08M 33s
210550K .......... .......... .......... .......... .......... 39% 10.0M 33s
210600K .......... .......... .......... .......... .......... 39% 8.87M 33s
210650K .......... .......... .......... .......... .......... 39% 9.24M 33s
210700K .......... .......... .......... .......... .......... 39% 8.36M 33s
210750K .......... .......... .......... .......... .......... 39% 9.08M 33s
210800K .......... .......... .......... .......... .......... 39% 10.3M 33s
210850K .......... .......... .......... .......... .......... 39% 19.8M 33s
210900K .......... .......... .......... .......... .......... 39% 16.4M 33s
210950K .......... .......... .......... .......... .......... 39% 13.3M 33s
211000K .......... .......... .......... .......... .......... 39% 40.5M 33s
211050K .......... .......... .......... .......... .......... 39% 11.1M 33s
211100K .......... .......... .......... .......... .......... 39% 9.95M 33s
211150K .......... .......... .......... .......... .......... 39% 13.0M 33s
211200K .......... .......... .......... .......... .......... 39% 8.52M 33s
211250K .......... .......... .......... .......... .......... 39% 6.99M 33s
211300K .......... .......... .......... .......... .......... 39% 13.3M 33s
211350K .......... .......... .......... .......... .......... 39% 8.19M 33s
211400K .......... .......... .......... .......... .......... 39% 9.90M 33s
211450K .......... .......... .......... .......... .......... 39% 5.41M 33s
211500K .......... .......... .......... .......... .......... 39% 5.98M 33s
211550K .......... .......... .......... .......... .......... 39% 6.17M 33s
211600K .......... .......... .......... .......... .......... 39% 4.40M 33s
211650K .......... .......... .......... .......... .......... 39% 6.67M 33s
211700K .......... .......... .......... .......... .......... 39% 6.81M 33s
211750K .......... .......... .......... .......... .......... 39% 7.53M 33s
211800K .......... .......... .......... .......... .......... 39% 7.57M 33s
211850K .......... .......... .......... .......... .......... 39% 7.41M 33s
211900K .......... .......... .......... .......... .......... 39% 7.84M 33s
211950K .......... .......... .......... .......... .......... 39% 7.71M 33s
212000K .......... .......... .......... .......... .......... 39% 8.27M 33s
212050K .......... .......... .......... .......... .......... 39% 14.6M 33s
212100K .......... .......... .......... .......... .......... 39% 22.9M 33s
212150K .......... .......... .......... .......... .......... 39% 19.0M 33s
212200K .......... .......... .......... .......... .......... 39% 13.7M 33s
212250K .......... .......... .......... .......... .......... 39% 17.4M 33s
212300K .......... .......... .......... .......... .......... 39% 10.1M 33s
212350K .......... .......... .......... .......... .......... 39% 9.01M 33s
212400K .......... .......... .......... .......... .......... 39% 11.5M 33s
212450K .......... .......... .......... .......... .......... 39% 8.00M 33s
212500K .......... .......... .......... .......... .......... 39% 10.4M 33s
212550K .......... .......... .......... .......... .......... 39% 8.96M 33s
212600K .......... .......... .......... .......... .......... 39% 8.86M 33s
212650K .......... .......... .......... .......... .......... 39% 11.8M 33s
212700K .......... .......... .......... .......... .......... 39% 15.2M 33s
212750K .......... .......... .......... .......... .......... 39% 19.2M 33s
212800K .......... .......... .......... .......... .......... 39% 18.2M 33s
212850K .......... .......... .......... .......... .......... 39% 13.1M 33s
212900K .......... .......... .......... .......... .......... 39% 18.0M 33s
212950K .......... .......... .......... .......... .......... 39% 10.1M 33s
213000K .......... .......... .......... .......... .......... 39% 12.1M 33s
213050K .......... .......... .......... .......... .......... 39% 12.5M 33s
213100K .......... .......... .......... .......... .......... 39% 9.50M 33s
213150K .......... .......... .......... .......... .......... 39% 9.71M 33s
213200K .......... .......... .......... .......... .......... 39% 10.2M 33s
213250K .......... .......... .......... .......... .......... 39% 10.4M 33s
213300K .......... .......... .......... .......... .......... 39% 12.0M 33s
213350K .......... .......... .......... .......... .......... 39% 10.6M 33s
213400K .......... .......... .......... .......... .......... 39% 23.9M 33s
213450K .......... .......... .......... .......... .......... 39% 19.9M 33s
213500K .......... .......... .......... .......... .......... 39% 16.5M 33s
213550K .......... .......... .......... .......... .......... 39% 22.2M 33s
213600K .......... .......... .......... .......... .......... 39% 15.0M 32s
213650K .......... .......... .......... .......... .......... 39% 14.5M 32s
213700K .......... .......... .......... .......... .......... 39% 13.4M 32s
213750K .......... .......... .......... .......... .......... 39% 8.90M 32s
213800K .......... .......... .......... .......... .......... 39% 12.5M 32s
213850K .......... .......... .......... .......... .......... 39% 8.89M 32s
213900K .......... .......... .......... .......... .......... 39% 9.50M 32s
213950K .......... .......... .......... .......... .......... 39% 11.5M 32s
214000K .......... .......... .......... .......... .......... 39% 14.3M 32s
214050K .......... .......... .......... .......... .......... 39% 13.8M 32s
214100K .......... .......... .......... .......... .......... 39% 11.8M 32s
214150K .......... .......... .......... .......... .......... 39% 12.1M 32s
214200K .......... .......... .......... .......... .......... 39% 10.2M 32s
214250K .......... .......... .......... .......... .......... 39% 9.66M 32s
214300K .......... .......... .......... .......... .......... 39% 15.2M 32s
214350K .......... .......... .......... .......... .......... 39% 8.61M 32s
214400K .......... .......... .......... .......... .......... 39% 11.3M 32s
214450K .......... .......... .......... .......... .......... 39% 11.5M 32s
214500K .......... .......... .......... .......... .......... 39% 11.4M 32s
214550K .......... .......... .......... .......... .......... 39% 12.1M 32s
214600K .......... .......... .......... .......... .......... 39% 8.85M 32s
214650K .......... .......... .......... .......... .......... 39% 9.56M 32s
214700K .......... .......... .......... .......... .......... 39% 6.45M 32s
214750K .......... .......... .......... .......... .......... 39% 9.95M 32s
214800K .......... .......... .......... .......... .......... 39% 7.14M 32s
214850K .......... .......... .......... .......... .......... 39% 5.46M 32s
214900K .......... .......... .......... .......... .......... 39% 5.21M 32s
214950K .......... .......... .......... .......... .......... 40% 6.40M 32s
215000K .......... .......... .......... .......... .......... 40% 8.29M 32s
215050K .......... .......... .......... .......... .......... 40% 6.63M 32s
215100K .......... .......... .......... .......... .......... 40% 4.82M 32s
215150K .......... .......... .......... .......... .......... 40% 6.06M 32s
215200K .......... .......... .......... .......... .......... 40% 5.38M 32s
215250K .......... .......... .......... .......... .......... 40% 5.86M 32s
215300K .......... .......... .......... .......... .......... 40% 6.79M 32s
215350K .......... .......... .......... .......... .......... 40% 6.62M 32s
215400K .......... .......... .......... .......... .......... 40% 8.90M 32s
215450K .......... .......... .......... .......... .......... 40% 6.89M 32s
215500K .......... .......... .......... .......... .......... 40% 8.81M 32s
215550K .......... .......... .......... .......... .......... 40% 8.09M 32s
215600K .......... .......... .......... .......... .......... 40% 7.05M 32s
215650K .......... .......... .......... .......... .......... 40% 7.71M 32s
215700K .......... .......... .......... .......... .......... 40% 10.6M 32s
215750K .......... .......... .......... .......... .......... 40% 11.2M 32s
215800K .......... .......... .......... .......... .......... 40% 11.3M 32s
215850K .......... .......... .......... .......... .......... 40% 9.87M 32s
215900K .......... .......... .......... .......... .......... 40% 10.7M 32s
215950K .......... .......... .......... .......... .......... 40% 10.6M 32s
216000K .......... .......... .......... .......... .......... 40% 9.09M 32s
216050K .......... .......... .......... .......... .......... 40% 10.2M 32s
216100K .......... .......... .......... .......... .......... 40% 9.91M 32s
216150K .......... .......... .......... .......... .......... 40% 9.78M 32s
216200K .......... .......... .......... .......... .......... 40% 12.1M 32s
216250K .......... .......... .......... .......... .......... 40% 14.6M 32s
216300K .......... .......... .......... .......... .......... 40% 12.6M 32s
216350K .......... .......... .......... .......... .......... 40% 12.1M 32s
216400K .......... .......... .......... .......... .......... 40% 15.3M 32s
216450K .......... .......... .......... .......... .......... 40% 20.8M 32s
216500K .......... .......... .......... .......... .......... 40% 32.4M 32s
216550K .......... .......... .......... .......... .......... 40% 49.7M 32s
216600K .......... .......... .......... .......... .......... 40% 21.4M 32s
216650K .......... .......... .......... .......... .......... 40%  120M 32s
216700K .......... .......... .......... .......... .......... 40% 22.8M 32s
216750K .......... .......... .......... .......... .......... 40% 28.6M 32s
216800K .......... .......... .......... .......... .......... 40% 23.2M 32s
216850K .......... .......... .......... .......... .......... 40% 21.4M 32s
216900K .......... .......... .......... .......... .......... 40% 27.8M 32s
216950K .......... .......... .......... .......... .......... 40% 12.1M 32s
217000K .......... .......... .......... .......... .......... 40% 24.4M 32s
217050K .......... .......... .......... .......... .......... 40% 21.2M 32s
217100K .......... .......... .......... .......... .......... 40% 14.3M 32s
217150K .......... .......... .......... .......... .......... 40% 11.5M 32s
217200K .......... .......... .......... .......... .......... 40% 10.6M 32s
217250K .......... .......... .......... .......... .......... 40% 9.41M 32s
217300K .......... .......... .......... .......... .......... 40% 8.27M 32s
217350K .......... .......... .......... .......... .......... 40% 7.23M 32s
217400K .......... .......... .......... .......... .......... 40% 5.03M 32s
217450K .......... .......... .......... .......... .......... 40% 3.52M 32s
217500K .......... .......... .......... .......... .......... 40% 3.99M 32s
217550K .......... .......... .......... .......... .......... 40% 4.16M 32s
217600K .......... .......... .......... .......... .......... 40% 9.24M 32s
217650K .......... .......... .......... .......... .......... 40% 12.5M 32s
217700K .......... .......... .......... .......... .......... 40% 11.9M 32s
217750K .......... .......... .......... .......... .......... 40% 13.8M 32s
217800K .......... .......... .......... .......... .......... 40% 9.48M 32s
217850K .......... .......... .......... .......... .......... 40% 5.81M 32s
217900K .......... .......... .......... .......... .......... 40% 6.18M 32s
217950K .......... .......... .......... .......... .......... 40% 5.98M 32s
218000K .......... .......... .......... .......... .......... 40% 8.47M 32s
218050K .......... .......... .......... .......... .......... 40% 7.29M 32s
218100K .......... .......... .......... .......... .......... 40% 5.86M 32s
218150K .......... .......... .......... .......... .......... 40% 5.64M 32s
218200K .......... .......... .......... .......... .......... 40% 7.55M 32s
218250K .......... .......... .......... .......... .......... 40% 7.84M 32s
218300K .......... .......... .......... .......... .......... 40% 8.93M 32s
218350K .......... .......... .......... .......... .......... 40% 7.60M 32s
218400K .......... .......... .......... .......... .......... 40% 8.75M 32s
218450K .......... .......... .......... .......... .......... 40% 11.8M 32s
218500K .......... .......... .......... .......... .......... 40% 22.0M 32s
218550K .......... .......... .......... .......... .......... 40% 11.9M 32s
218600K .......... .......... .......... .......... .......... 40%  102M 32s
218650K .......... .......... .......... .......... .......... 40% 8.43M 32s
218700K .......... .......... .......... .......... .......... 40% 86.3M 32s
218750K .......... .......... .......... .......... .......... 40% 18.2M 32s
218800K .......... .......... .......... .......... .......... 40% 14.2M 32s
218850K .......... .......... .......... .......... .......... 40% 11.0M 32s
218900K .......... .......... .......... .......... .......... 40% 15.5M 32s
218950K .......... .......... .......... .......... .......... 40% 11.1M 32s
219000K .......... .......... .......... .......... .......... 40% 12.0M 32s
219050K .......... .......... .......... .......... .......... 40% 14.1M 32s
219100K .......... .......... .......... .......... .......... 40% 11.7M 32s
219150K .......... .......... .......... .......... .......... 40% 19.8M 32s
219200K .......... .......... .......... .......... .......... 40% 8.47M 32s
219250K .......... .......... .......... .......... .......... 40%  115M 32s
219300K .......... .......... .......... .......... .......... 40% 15.1M 32s
219350K .......... .......... .......... .......... .......... 40% 13.5M 32s
219400K .......... .......... .......... .......... .......... 40% 8.65M 32s
219450K .......... .......... .......... .......... .......... 40% 12.7M 32s
219500K .......... .......... .......... .......... .......... 40% 9.58M 32s
219550K .......... .......... .......... .......... .......... 40% 9.30M 32s
219600K .......... .......... .......... .......... .......... 40% 6.55M 32s
219650K .......... .......... .......... .......... .......... 40% 9.20M 32s
219700K .......... .......... .......... .......... .......... 40% 8.25M 32s
219750K .......... .......... .......... .......... .......... 40% 6.79M 32s
219800K .......... .......... .......... .......... .......... 40% 7.17M 32s
219850K .......... .......... .......... .......... .......... 40% 6.39M 32s
219900K .......... .......... .......... .......... .......... 40% 6.49M 32s
219950K .......... .......... .......... .......... .......... 40% 5.58M 32s
220000K .......... .......... .......... .......... .......... 40% 10.6M 32s
220050K .......... .......... .......... .......... .......... 40% 21.3M 32s
220100K .......... .......... .......... .......... .......... 40% 31.8M 32s
220150K .......... .......... .......... .......... .......... 40% 21.0M 32s
220200K .......... .......... .......... .......... .......... 40% 18.3M 32s
220250K .......... .......... .......... .......... .......... 40% 21.3M 32s
220300K .......... .......... .......... .......... .......... 41% 24.8M 32s
220350K .......... .......... .......... .......... .......... 41% 15.1M 32s
220400K .......... .......... .......... .......... .......... 41% 19.9M 32s
220450K .......... .......... .......... .......... .......... 41% 16.2M 32s
220500K .......... .......... .......... .......... .......... 41% 17.3M 32s
220550K .......... .......... .......... .......... .......... 41% 14.3M 32s
220600K .......... .......... .......... .......... .......... 41% 10.0M 32s
220650K .......... .......... .......... .......... .......... 41% 7.65M 32s
220700K .......... .......... .......... .......... .......... 41% 6.53M 32s
220750K .......... .......... .......... .......... .......... 41% 11.0M 32s
220800K .......... .......... .......... .......... .......... 41% 11.4M 32s
220850K .......... .......... .......... .......... .......... 41% 8.91M 32s
220900K .......... .......... .......... .......... .......... 41% 9.83M 32s
220950K .......... .......... .......... .......... .......... 41% 7.36M 32s
221000K .......... .......... .......... .......... .......... 41% 7.16M 32s
221050K .......... .......... .......... .......... .......... 41% 7.60M 32s
221100K .......... .......... .......... .......... .......... 41% 6.60M 32s
221150K .......... .......... .......... .......... .......... 41% 7.58M 32s
221200K .......... .......... .......... .......... .......... 41% 6.40M 32s
221250K .......... .......... .......... .......... .......... 41% 9.71M 32s
221300K .......... .......... .......... .......... .......... 41% 13.2M 32s
221350K .......... .......... .......... .......... .......... 41% 7.34M 32s
221400K .......... .......... .......... .......... .......... 41% 9.29M 32s
221450K .......... .......... .......... .......... .......... 41% 14.7M 32s
221500K .......... .......... .......... .......... .......... 41% 12.7M 32s
221550K .......... .......... .......... .......... .......... 41% 30.6M 32s
221600K .......... .......... .......... .......... .......... 41% 15.2M 32s
221650K .......... .......... .......... .......... .......... 41% 15.6M 32s
221700K .......... .......... .......... .......... .......... 41% 14.2M 32s
221750K .......... .......... .......... .......... .......... 41% 17.8M 32s
221800K .......... .......... .......... .......... .......... 41% 18.2M 32s
221850K .......... .......... .......... .......... .......... 41% 15.3M 32s
221900K .......... .......... .......... .......... .......... 41% 20.5M 32s
221950K .......... .......... .......... .......... .......... 41% 12.2M 32s
222000K .......... .......... .......... .......... .......... 41% 18.2M 32s
222050K .......... .......... .......... .......... .......... 41% 11.7M 32s
222100K .......... .......... .......... .......... .......... 41% 9.45M 32s
222150K .......... .......... .......... .......... .......... 41% 13.8M 32s
222200K .......... .......... .......... .......... .......... 41% 17.2M 32s
222250K .......... .......... .......... .......... .......... 41% 20.2M 32s
222300K .......... .......... .......... .......... .......... 41% 18.4M 32s
222350K .......... .......... .......... .......... .......... 41% 16.6M 32s
222400K .......... .......... .......... .......... .......... 41% 25.7M 32s
222450K .......... .......... .......... .......... .......... 41% 22.3M 32s
222500K .......... .......... .......... .......... .......... 41% 21.1M 32s
222550K .......... .......... .......... .......... .......... 41% 20.4M 32s
222600K .......... .......... .......... .......... .......... 41% 20.0M 32s
222650K .......... .......... .......... .......... .......... 41% 16.2M 32s
222700K .......... .......... .......... .......... .......... 41% 21.7M 32s
222750K .......... .......... .......... .......... .......... 41% 23.7M 31s
222800K .......... .......... .......... .......... .......... 41% 18.4M 31s
222850K .......... .......... .......... .......... .......... 41% 16.0M 31s
222900K .......... .......... .......... .......... .......... 41% 20.5M 31s
222950K .......... .......... .......... .......... .......... 41% 17.8M 31s
223000K .......... .......... .......... .......... .......... 41% 20.1M 31s
223050K .......... .......... .......... .......... .......... 41% 15.4M 31s
223100K .......... .......... .......... .......... .......... 41% 12.6M 31s
223150K .......... .......... .......... .......... .......... 41% 7.88M 31s
223200K .......... .......... .......... .......... .......... 41% 10.0M 31s
223250K .......... .......... .......... .......... .......... 41% 12.8M 31s
223300K .......... .......... .......... .......... .......... 41% 9.65M 31s
223350K .......... .......... .......... .......... .......... 41% 10.9M 31s
223400K .......... .......... .......... .......... .......... 41% 11.9M 31s
223450K .......... .......... .......... .......... .......... 41% 10.1M 31s
223500K .......... .......... .......... .......... .......... 41% 9.31M 31s
223550K .......... .......... .......... .......... .......... 41% 10.7M 31s
223600K .......... .......... .......... .......... .......... 41% 11.6M 31s
223650K .......... .......... .......... .......... .......... 41% 10.0M 31s
223700K .......... .......... .......... .......... .......... 41% 10.6M 31s
223750K .......... .......... .......... .......... .......... 41% 12.3M 31s
223800K .......... .......... .......... .......... .......... 41% 11.4M 31s
223850K .......... .......... .......... .......... .......... 41% 11.6M 31s
223900K .......... .......... .......... .......... .......... 41% 10.1M 31s
223950K .......... .......... .......... .......... .......... 41% 11.5M 31s
224000K .......... .......... .......... .......... .......... 41% 24.6M 31s
224050K .......... .......... .......... .......... .......... 41% 26.7M 31s
224100K .......... .......... .......... .......... .......... 41% 9.38M 31s
224150K .......... .......... .......... .......... .......... 41% 24.2M 31s
224200K .......... .......... .......... .......... .......... 41% 23.4M 31s
224250K .......... .......... .......... .......... .......... 41% 14.9M 31s
224300K .......... .......... .......... .......... .......... 41% 12.6M 31s
224350K .......... .......... .......... .......... .......... 41% 12.7M 31s
224400K .......... .......... .......... .......... .......... 41% 10.2M 31s
224450K .......... .......... .......... .......... .......... 41% 10.8M 31s
224500K .......... .......... .......... .......... .......... 41% 15.3M 31s
224550K .......... .......... .......... .......... .......... 41% 16.0M 31s
224600K .......... .......... .......... .......... .......... 41% 11.7M 31s
224650K .......... .......... .......... .......... .......... 41% 10.8M 31s
224700K .......... .......... .......... .......... .......... 41% 12.7M 31s
224750K .......... .......... .......... .......... .......... 41% 10.7M 31s
224800K .......... .......... .......... .......... .......... 41% 7.77M 31s
224850K .......... .......... .......... .......... .......... 41% 6.84M 31s
224900K .......... .......... .......... .......... .......... 41% 6.79M 31s
224950K .......... .......... .......... .......... .......... 41% 6.43M 31s
225000K .......... .......... .......... .......... .......... 41% 6.68M 31s
225050K .......... .......... .......... .......... .......... 41% 12.5M 31s
225100K .......... .......... .......... .......... .......... 41% 16.6M 31s
225150K .......... .......... .......... .......... .......... 41% 57.9M 31s
225200K .......... .......... .......... .......... .......... 41% 21.7M 31s
225250K .......... .......... .......... .......... .......... 41% 18.8M 31s
225300K .......... .......... .......... .......... .......... 41% 22.7M 31s
225350K .......... .......... .......... .......... .......... 41% 11.7M 31s
225400K .......... .......... .......... .......... .......... 41% 14.5M 31s
225450K .......... .......... .......... .......... .......... 41% 11.7M 31s
225500K .......... .......... .......... .......... .......... 41% 12.1M 31s
225550K .......... .......... .......... .......... .......... 41% 13.8M 31s
225600K .......... .......... .......... .......... .......... 41% 13.5M 31s
225650K .......... .......... .......... .......... .......... 41% 15.7M 31s
225700K .......... .......... .......... .......... .......... 42% 13.0M 31s
225750K .......... .......... .......... .......... .......... 42% 12.9M 31s
225800K .......... .......... .......... .......... .......... 42% 15.9M 31s
225850K .......... .......... .......... .......... .......... 42% 15.0M 31s
225900K .......... .......... .......... .......... .......... 42% 17.2M 31s
225950K .......... .......... .......... .......... .......... 42% 18.9M 31s
226000K .......... .......... .......... .......... .......... 42% 90.9M 31s
226050K .......... .......... .......... .......... .......... 42% 27.7M 31s
226100K .......... .......... .......... .......... .......... 42% 42.3M 31s
226150K .......... .......... .......... .......... .......... 42% 22.6M 31s
226200K .......... .......... .......... .......... .......... 42% 15.4M 31s
226250K .......... .......... .......... .......... .......... 42% 20.6M 31s
226300K .......... .......... .......... .......... .......... 42% 22.4M 31s
226350K .......... .......... .......... .......... .......... 42% 18.7M 31s
226400K .......... .......... .......... .......... .......... 42% 20.2M 31s
226450K .......... .......... .......... .......... .......... 42% 21.1M 31s
226500K .......... .......... .......... .......... .......... 42% 18.0M 31s
226550K .......... .......... .......... .......... .......... 42% 20.8M 31s
226600K .......... .......... .......... .......... .......... 42% 20.2M 31s
226650K .......... .......... .......... .......... .......... 42% 20.3M 31s
226700K .......... .......... .......... .......... .......... 42% 17.8M 31s
226750K .......... .......... .......... .......... .......... 42% 21.9M 31s
226800K .......... .......... .......... .......... .......... 42% 21.5M 31s
226850K .......... .......... .......... .......... .......... 42% 12.1M 31s
226900K .......... .......... .......... .......... .......... 42% 12.0M 31s
226950K .......... .......... .......... .......... .......... 42% 13.7M 31s
227000K .......... .......... .......... .......... .......... 42% 11.0M 31s
227050K .......... .......... .......... .......... .......... 42% 21.2M 31s
227100K .......... .......... .......... .......... .......... 42% 11.4M 31s
227150K .......... .......... .......... .......... .......... 42% 15.7M 31s
227200K .......... .......... .......... .......... .......... 42% 9.88M 31s
227250K .......... .......... .......... .......... .......... 42% 12.3M 31s
227300K .......... .......... .......... .......... .......... 42% 10.3M 31s
227350K .......... .......... .......... .......... .......... 42% 9.62M 31s
227400K .......... .......... .......... .......... .......... 42% 10.9M 31s
227450K .......... .......... .......... .......... .......... 42% 10.4M 31s
227500K .......... .......... .......... .......... .......... 42% 14.2M 31s
227550K .......... .......... .......... .......... .......... 42% 9.86M 31s
227600K .......... .......... .......... .......... .......... 42% 9.44M 31s
227650K .......... .......... .......... .......... .......... 42% 7.49M 31s
227700K .......... .......... .......... .......... .......... 42% 6.51M 31s
227750K .......... .......... .......... .......... .......... 42% 8.21M 31s
227800K .......... .......... .......... .......... .......... 42% 6.36M 31s
227850K .......... .......... .......... .......... .......... 42% 7.46M 31s
227900K .......... .......... .......... .......... .......... 42% 7.00M 31s
227950K .......... .......... .......... .......... .......... 42% 6.49M 31s
228000K .......... .......... .......... .......... .......... 42% 6.08M 31s
228050K .......... .......... .......... .......... .......... 42% 5.66M 31s
228100K .......... .......... .......... .......... .......... 42% 8.41M 31s
228150K .......... .......... .......... .......... .......... 42% 17.3M 31s
228200K .......... .......... .......... .......... .......... 42% 15.4M 31s
228250K .......... .......... .......... .......... .......... 42% 15.5M 31s
228300K .......... .......... .......... .......... .......... 42% 10.2M 31s
228350K .......... .......... .......... .......... .......... 42% 10.7M 31s
228400K .......... .......... .......... .......... .......... 42% 9.61M 31s
228450K .......... .......... .......... .......... .......... 42% 9.13M 31s
228500K .......... .......... .......... .......... .......... 42% 9.75M 31s
228550K .......... .......... .......... .......... .......... 42% 9.68M 31s
228600K .......... .......... .......... .......... .......... 42% 8.98M 31s
228650K .......... .......... .......... .......... .......... 42% 11.7M 31s
228700K .......... .......... .......... .......... .......... 42% 9.22M 31s
228750K .......... .......... .......... .......... .......... 42% 6.26M 31s
228800K .......... .......... .......... .......... .......... 42% 10.2M 31s
228850K .......... .......... .......... .......... .......... 42% 9.57M 31s
228900K .......... .......... .......... .......... .......... 42% 12.7M 31s
228950K .......... .......... .......... .......... .......... 42% 9.82M 31s
229000K .......... .......... .......... .......... .......... 42% 14.7M 31s
229050K .......... .......... .......... .......... .......... 42% 9.20M 31s
229100K .......... .......... .......... .......... .......... 42% 8.88M 31s
229150K .......... .......... .......... .......... .......... 42% 14.9M 31s
229200K .......... .......... .......... .......... .......... 42% 9.13M 31s
229250K .......... .......... .......... .......... .......... 42% 11.3M 31s
229300K .......... .......... .......... .......... .......... 42% 13.7M 31s
229350K .......... .......... .......... .......... .......... 42% 5.54M 31s
229400K .......... .......... .......... .......... .......... 42% 9.02M 31s
229450K .......... .......... .......... .......... .......... 42% 8.19M 31s
229500K .......... .......... .......... .......... .......... 42% 9.51M 31s
229550K .......... .......... .......... .......... .......... 42% 9.80M 31s
229600K .......... .......... .......... .......... .......... 42% 9.27M 31s
229650K .......... .......... .......... .......... .......... 42% 9.69M 31s
229700K .......... .......... .......... .......... .......... 42% 6.12M 31s
229750K .......... .......... .......... .......... .......... 42% 4.51M 31s
229800K .......... .......... .......... .......... .......... 42% 16.8M 31s
229850K .......... .......... .......... .......... .......... 42% 14.8M 31s
229900K .......... .......... .......... .......... .......... 42% 13.9M 31s
229950K .......... .......... .......... .......... .......... 42% 32.0M 31s
230000K .......... .......... .......... .......... .......... 42% 16.2M 31s
230050K .......... .......... .......... .......... .......... 42% 17.0M 31s
230100K .......... .......... .......... .......... .......... 42% 9.75M 31s
230150K .......... .......... .......... .......... .......... 42% 12.4M 31s
230200K .......... .......... .......... .......... .......... 42% 10.9M 31s
230250K .......... .......... .......... .......... .......... 42% 14.0M 31s
230300K .......... .......... .......... .......... .......... 42% 13.4M 31s
230350K .......... .......... .......... .......... .......... 42% 11.7M 31s
230400K .......... .......... .......... .......... .......... 42% 12.6M 31s
230450K .......... .......... .......... .......... .......... 42% 10.8M 31s
230500K .......... .......... .......... .......... .......... 42% 12.4M 31s
230550K .......... .......... .......... .......... .......... 42% 13.5M 31s
230600K .......... .......... .......... .......... .......... 42% 15.2M 31s
230650K .......... .......... .......... .......... .......... 42% 16.9M 31s
230700K .......... .......... .......... .......... .......... 42% 12.0M 31s
230750K .......... .......... .......... .......... .......... 42% 17.5M 31s
230800K .......... .......... .......... .......... .......... 42% 15.5M 31s
230850K .......... .......... .......... .......... .......... 42% 7.47M 31s
230900K .......... .......... .......... .......... .......... 42% 10.0M 31s
230950K .......... .......... .......... .......... .......... 42% 10.9M 31s
231000K .......... .......... .......... .......... .......... 42% 10.9M 30s
231050K .......... .......... .......... .......... .......... 43% 18.4M 30s
231100K .......... .......... .......... .......... .......... 43% 14.6M 30s
231150K .......... .......... .......... .......... .......... 43% 24.6M 30s
231200K .......... .......... .......... .......... .......... 43% 10.3M 30s
231250K .......... .......... .......... .......... .......... 43% 12.4M 30s
231300K .......... .......... .......... .......... .......... 43% 13.3M 30s
231350K .......... .......... .......... .......... .......... 43% 10.7M 30s
231400K .......... .......... .......... .......... .......... 43% 8.73M 30s
231450K .......... .......... .......... .......... .......... 43% 8.82M 30s
231500K .......... .......... .......... .......... .......... 43% 11.2M 30s
231550K .......... .......... .......... .......... .......... 43% 11.5M 30s
231600K .......... .......... .......... .......... .......... 43% 7.95M 30s
231650K .......... .......... .......... .......... .......... 43% 6.74M 30s
231700K .......... .......... .......... .......... .......... 43% 6.28M 30s
231750K .......... .......... .......... .......... .......... 43% 8.24M 30s
231800K .......... .......... .......... .......... .......... 43% 9.04M 30s
231850K .......... .......... .......... .......... .......... 43% 6.82M 30s
231900K .......... .......... .......... .......... .......... 43% 9.88M 30s
231950K .......... .......... .......... .......... .......... 43% 15.8M 30s
232000K .......... .......... .......... .......... .......... 43% 42.5M 30s
232050K .......... .......... .......... .......... .......... 43% 46.4M 30s
232100K .......... .......... .......... .......... .......... 43% 13.2M 30s
232150K .......... .......... .......... .......... .......... 43%  138M 30s
232200K .......... .......... .......... .......... .......... 43% 20.5M 30s
232250K .......... .......... .......... .......... .......... 43% 20.9M 30s
232300K .......... .......... .......... .......... .......... 43% 24.5M 30s
232350K .......... .......... .......... .......... .......... 43% 17.7M 30s
232400K .......... .......... .......... .......... .......... 43% 20.8M 30s
232450K .......... .......... .......... .......... .......... 43% 24.2M 30s
232500K .......... .......... .......... .......... .......... 43% 24.8M 30s
232550K .......... .......... .......... .......... .......... 43% 20.8M 30s
232600K .......... .......... .......... .......... .......... 43% 16.4M 30s
232650K .......... .......... .......... .......... .......... 43% 23.7M 30s
232700K .......... .......... .......... .......... .......... 43% 20.7M 30s
232750K .......... .......... .......... .......... .......... 43% 25.4M 30s
232800K .......... .......... .......... .......... .......... 43% 23.9M 30s
232850K .......... .......... .......... .......... .......... 43% 20.7M 30s
232900K .......... .......... .......... .......... .......... 43% 25.4M 30s
232950K .......... .......... .......... .......... .......... 43% 13.1M 30s
233000K .......... .......... .......... .......... .......... 43% 7.48M 30s
233050K .......... .......... .......... .......... .......... 43% 25.6M 30s
233100K .......... .......... .......... .......... .......... 43% 8.63M 30s
233150K .......... .......... .......... .......... .......... 43% 11.2M 30s
233200K .......... .......... .......... .......... .......... 43% 10.8M 30s
233250K .......... .......... .......... .......... .......... 43% 15.4M 30s
233300K .......... .......... .......... .......... .......... 43% 15.8M 30s
233350K .......... .......... .......... .......... .......... 43% 11.7M 30s
233400K .......... .......... .......... .......... .......... 43% 15.6M 30s
233450K .......... .......... .......... .......... .......... 43% 12.3M 30s
233500K .......... .......... .......... .......... .......... 43% 12.3M 30s
233550K .......... .......... .......... .......... .......... 43% 12.6M 30s
233600K .......... .......... .......... .......... .......... 43% 9.90M 30s
233650K .......... .......... .......... .......... .......... 43% 25.9M 30s
233700K .......... .......... .......... .......... .......... 43% 13.5M 30s
233750K .......... .......... .......... .......... .......... 43% 96.9M 30s
233800K .......... .......... .......... .......... .......... 43% 16.6M 30s
233850K .......... .......... .......... .......... .......... 43% 17.6M 30s
233900K .......... .......... .......... .......... .......... 43% 14.9M 30s
233950K .......... .......... .......... .......... .......... 43% 16.3M 30s
234000K .......... .......... .......... .......... .......... 43% 23.6M 30s
234050K .......... .......... .......... .......... .......... 43% 13.4M 30s
234100K .......... .......... .......... .......... .......... 43% 19.9M 30s
234150K .......... .......... .......... .......... .......... 43% 19.9M 30s
234200K .......... .......... .......... .......... .......... 43% 18.3M 30s
234250K .......... .......... .......... .......... .......... 43% 18.7M 30s
234300K .......... .......... .......... .......... .......... 43% 17.7M 30s
234350K .......... .......... .......... .......... .......... 43% 17.6M 30s
234400K .......... .......... .......... .......... .......... 43% 18.3M 30s
234450K .......... .......... .......... .......... .......... 43% 18.9M 30s
234500K .......... .......... .......... .......... .......... 43% 24.4M 30s
234550K .......... .......... .......... .......... .......... 43% 26.2M 30s
234600K .......... .......... .......... .......... .......... 43% 24.1M 30s
234650K .......... .......... .......... .......... .......... 43% 21.5M 30s
234700K .......... .......... .......... .......... .......... 43% 95.9M 30s
234750K .......... .......... .......... .......... .......... 43% 26.4M 30s
234800K .......... .......... .......... .......... .......... 43%  131M 30s
234850K .......... .......... .......... .......... .......... 43% 23.0M 30s
234900K .......... .......... .......... .......... .......... 43% 27.3M 30s
234950K .......... .......... .......... .......... .......... 43% 16.3M 30s
235000K .......... .......... .......... .......... .......... 43% 17.8M 30s
235050K .......... .......... .......... .......... .......... 43% 17.6M 30s
235100K .......... .......... .......... .......... .......... 43% 18.2M 30s
235150K .......... .......... .......... .......... .......... 43% 19.7M 30s
235200K .......... .......... .......... .......... .......... 43% 16.0M 30s
235250K .......... .......... .......... .......... .......... 43% 16.1M 30s
235300K .......... .......... .......... .......... .......... 43% 14.3M 30s
235350K .......... .......... .......... .......... .......... 43% 15.6M 30s
235400K .......... .......... .......... .......... .......... 43% 16.5M 30s
235450K .......... .......... .......... .......... .......... 43% 16.0M 30s
235500K .......... .......... .......... .......... .......... 43% 19.9M 30s
235550K .......... .......... .......... .......... .......... 43% 18.7M 30s
235600K .......... .......... .......... .......... .......... 43% 14.8M 30s
235650K .......... .......... .......... .......... .......... 43% 18.6M 30s
235700K .......... .......... .......... .......... .......... 43% 10.9M 30s
235750K .......... .......... .......... .......... .......... 43% 10.4M 30s
235800K .......... .......... .......... .......... .......... 43% 12.4M 30s
235850K .......... .......... .......... .......... .......... 43% 13.8M 30s
235900K .......... .......... .......... .......... .......... 43% 16.9M 30s
235950K .......... .......... .......... .......... .......... 43% 15.7M 30s
236000K .......... .......... .......... .......... .......... 43% 19.2M 30s
236050K .......... .......... .......... .......... .......... 43% 16.6M 30s
236100K .......... .......... .......... .......... .......... 43% 10.5M 30s
236150K .......... .......... .......... .......... .......... 43% 17.0M 30s
236200K .......... .......... .......... .......... .......... 43% 12.2M 30s
236250K .......... .......... .......... .......... .......... 43% 16.8M 30s
236300K .......... .......... .......... .......... .......... 43% 14.0M 30s
236350K .......... .......... .......... .......... .......... 43% 13.3M 30s
236400K .......... .......... .......... .......... .......... 43% 17.0M 30s
236450K .......... .......... .......... .......... .......... 44% 11.9M 30s
236500K .......... .......... .......... .......... .......... 44% 8.69M 30s
236550K .......... .......... .......... .......... .......... 44% 12.1M 30s
236600K .......... .......... .......... .......... .......... 44% 11.8M 30s
236650K .......... .......... .......... .......... .......... 44% 20.7M 30s
236700K .......... .......... .......... .......... .......... 44% 11.7M 30s
236750K .......... .......... .......... .......... .......... 44% 10.8M 30s
236800K .......... .......... .......... .......... .......... 44% 9.43M 30s
236850K .......... .......... .......... .......... .......... 44% 10.3M 30s
236900K .......... .......... .......... .......... .......... 44% 10.0M 30s
236950K .......... .......... .......... .......... .......... 44% 9.12M 30s
237000K .......... .......... .......... .......... .......... 44% 9.71M 30s
237050K .......... .......... .......... .......... .......... 44% 10.0M 30s
237100K .......... .......... .......... .......... .......... 44% 9.55M 30s
237150K .......... .......... .......... .......... .......... 44% 22.9M 30s
237200K .......... .......... .......... .......... .......... 44% 12.6M 30s
237250K .......... .......... .......... .......... .......... 44% 21.2M 30s
237300K .......... .......... .......... .......... .......... 44% 21.6M 30s
237350K .......... .......... .......... .......... .......... 44% 17.1M 30s
237400K .......... .......... .......... .......... .......... 44% 23.5M 30s
237450K .......... .......... .......... .......... .......... 44% 14.9M 30s
237500K .......... .......... .......... .......... .......... 44% 17.3M 30s
237550K .......... .......... .......... .......... .......... 44% 25.5M 30s
237600K .......... .......... .......... .......... .......... 44% 15.4M 30s
237650K .......... .......... .......... .......... .......... 44% 17.6M 30s
237700K .......... .......... .......... .......... .......... 44% 20.7M 30s
237750K .......... .......... .......... .......... .......... 44% 16.9M 30s
237800K .......... .......... .......... .......... .......... 44% 20.8M 30s
237850K .......... .......... .......... .......... .......... 44% 18.6M 30s
237900K .......... .......... .......... .......... .......... 44% 16.8M 30s
237950K .......... .......... .......... .......... .......... 44% 16.7M 30s
238000K .......... .......... .......... .......... .......... 44% 10.3M 29s
238050K .......... .......... .......... .......... .......... 44% 58.9M 29s
238100K .......... .......... .......... .......... .......... 44% 15.4M 29s
238150K .......... .......... .......... .......... .......... 44%  112M 29s
238200K .......... .......... .......... .......... .......... 44% 16.0M 29s
238250K .......... .......... .......... .......... .......... 44% 24.0M 29s
238300K .......... .......... .......... .......... .......... 44% 15.8M 29s
238350K .......... .......... .......... .......... .......... 44% 21.3M 29s
238400K .......... .......... .......... .......... .......... 44% 11.3M 29s
238450K .......... .......... .......... .......... .......... 44% 16.1M 29s
238500K .......... .......... .......... .......... .......... 44% 22.9M 29s
238550K .......... .......... .......... .......... .......... 44% 14.7M 29s
238600K .......... .......... .......... .......... .......... 44% 13.8M 29s
238650K .......... .......... .......... .......... .......... 44% 20.7M 29s
238700K .......... .......... .......... .......... .......... 44% 11.5M 29s
238750K .......... .......... .......... .......... .......... 44% 16.1M 29s
238800K .......... .......... .......... .......... .......... 44% 15.4M 29s
238850K .......... .......... .......... .......... .......... 44% 11.2M 29s
238900K .......... .......... .......... .......... .......... 44% 13.5M 29s
238950K .......... .......... .......... .......... .......... 44% 10.9M 29s
239000K .......... .......... .......... .......... .......... 44% 10.4M 29s
239050K .......... .......... .......... .......... .......... 44% 16.8M 29s
239100K .......... .......... .......... .......... .......... 44% 11.3M 29s
239150K .......... .......... .......... .......... .......... 44% 12.1M 29s
239200K .......... .......... .......... .......... .......... 44% 11.5M 29s
239250K .......... .......... .......... .......... .......... 44% 13.4M 29s
239300K .......... .......... .......... .......... .......... 44% 11.6M 29s
239350K .......... .......... .......... .......... .......... 44% 9.95M 29s
239400K .......... .......... .......... .......... .......... 44% 9.35M 29s
239450K .......... .......... .......... .......... .......... 44% 18.7M 29s
239500K .......... .......... .......... .......... .......... 44% 14.8M 29s
239550K .......... .......... .......... .......... .......... 44% 13.2M 29s
239600K .......... .......... .......... .......... .......... 44% 13.9M 29s
239650K .......... .......... .......... .......... .......... 44% 15.8M 29s
239700K .......... .......... .......... .......... .......... 44% 10.4M 29s
239750K .......... .......... .......... .......... .......... 44% 15.8M 29s
239800K .......... .......... .......... .......... .......... 44% 15.2M 29s
239850K .......... .......... .......... .......... .......... 44% 14.1M 29s
239900K .......... .......... .......... .......... .......... 44% 17.4M 29s
239950K .......... .......... .......... .......... .......... 44% 9.68M 29s
240000K .......... .......... .......... .......... .......... 44% 11.6M 29s
240050K .......... .......... .......... .......... .......... 44% 17.0M 29s
240100K .......... .......... .......... .......... .......... 44% 19.8M 29s
240150K .......... .......... .......... .......... .......... 44% 61.0M 29s
240200K .......... .......... .......... .......... .......... 44% 23.0M 29s
240250K .......... .......... .......... .......... .......... 44% 36.3M 29s
240300K .......... .......... .......... .......... .......... 44% 26.5M 29s
240350K .......... .......... .......... .......... .......... 44% 35.0M 29s
240400K .......... .......... .......... .......... .......... 44% 26.9M 29s
240450K .......... .......... .......... .......... .......... 44% 26.3M 29s
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240550K .......... .......... .......... .......... .......... 44% 25.0M 29s
240600K .......... .......... .......... .......... .......... 44% 32.1M 29s
240650K .......... .......... .......... .......... .......... 44% 8.40M 29s
240700K .......... .......... .......... .......... .......... 44% 44.9M 29s
240750K .......... .......... .......... .......... .......... 44% 26.1M 29s
240800K .......... .......... .......... .......... .......... 44% 27.7M 29s
240850K .......... .......... .......... .......... .......... 44% 24.6M 29s
240900K .......... .......... .......... .......... .......... 44% 31.1M 29s
240950K .......... .......... .......... .......... .......... 44% 25.4M 29s
241000K .......... .......... .......... .......... .......... 44% 31.9M 29s
241050K .......... .......... .......... .......... .......... 44% 23.4M 29s
241100K .......... .......... .......... .......... .......... 44% 75.4M 29s
241150K .......... .......... .......... .......... .......... 44% 32.3M 29s
241200K .......... .......... .......... .......... .......... 44% 19.5M 29s
241250K .......... .......... .......... .......... .......... 44% 59.8M 29s
241300K .......... .......... .......... .......... .......... 44%  112M 29s
241350K .......... .......... .......... .......... .......... 44% 42.3M 29s
241400K .......... .......... .......... .......... .......... 44% 60.7M 29s
241450K .......... .......... .......... .......... .......... 44% 59.9M 29s
241500K .......... .......... .......... .......... .......... 44% 34.5M 29s
241550K .......... .......... .......... .......... .......... 44% 29.5M 29s
241600K .......... .......... .......... .......... .......... 44% 37.6M 29s
241650K .......... .......... .......... .......... .......... 44% 28.3M 29s
241700K .......... .......... .......... .......... .......... 44% 26.9M 29s
241750K .......... .......... .......... .......... .......... 44% 35.8M 29s
241800K .......... .......... .......... .......... .......... 45% 25.5M 29s
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241900K .......... .......... .......... .......... .......... 45% 25.3M 29s
241950K .......... .......... .......... .......... .......... 45% 22.3M 29s
242000K .......... .......... .......... .......... .......... 45% 23.4M 29s
242050K .......... .......... .......... .......... .......... 45% 22.4M 29s
242100K .......... .......... .......... .......... .......... 45% 5.98M 29s
242150K .......... .......... .......... .......... .......... 45%  113M 29s
242200K .......... .......... .......... .......... .......... 45%  114M 29s
242250K .......... .......... .......... .......... .......... 45%  104M 29s
242300K .......... .......... .......... .......... .......... 45% 34.7M 29s
242350K .......... .......... .......... .......... .......... 45% 13.4M 29s
242400K .......... .......... .......... .......... .......... 45% 13.4M 29s
242450K .......... .......... .......... .......... .......... 45% 10.7M 29s
242500K .......... .......... .......... .......... .......... 45% 8.72M 29s
242550K .......... .......... .......... .......... .......... 45% 9.09M 29s
242600K .......... .......... .......... .......... .......... 45% 6.46M 29s
242650K .......... .......... .......... .......... .......... 45% 8.67M 29s
242700K .......... .......... .......... .......... .......... 45% 7.66M 29s
242750K .......... .......... .......... .......... .......... 45% 7.96M 29s
242800K .......... .......... .......... .......... .......... 45% 10.6M 29s
242850K .......... .......... .......... .......... .......... 45% 14.3M 29s
242900K .......... .......... .......... .......... .......... 45% 8.74M 29s
242950K .......... .......... .......... .......... .......... 45% 14.9M 29s
243000K .......... .......... .......... .......... .......... 45% 14.6M 29s
243050K .......... .......... .......... .......... .......... 45% 18.9M 29s
243100K .......... .......... .......... .......... .......... 45% 14.7M 29s
243150K .......... .......... .......... .......... .......... 45% 16.3M 29s
243200K .......... .......... .......... .......... .......... 45% 14.4M 29s
243250K .......... .......... .......... .......... .......... 45% 16.6M 29s
243300K .......... .......... .......... .......... .......... 45% 14.9M 29s
243350K .......... .......... .......... .......... .......... 45% 15.4M 29s
243400K .......... .......... .......... .......... .......... 45% 16.4M 29s
243450K .......... .......... .......... .......... .......... 45% 13.4M 29s
243500K .......... .......... .......... .......... .......... 45% 16.5M 29s
243550K .......... .......... .......... .......... .......... 45% 15.9M 29s
243600K .......... .......... .......... .......... .......... 45% 12.7M 29s
243650K .......... .......... .......... .......... .......... 45% 18.4M 29s
243700K .......... .......... .......... .......... .......... 45% 17.3M 29s
243750K .......... .......... .......... .......... .......... 45% 9.93M 29s
243800K .......... .......... .......... .......... .......... 45% 34.4M 29s
243850K .......... .......... .......... .......... .......... 45% 15.0M 29s
243900K .......... .......... .......... .......... .......... 45% 13.9M 29s
243950K .......... .......... .......... .......... .......... 45% 10.9M 29s
244000K .......... .......... .......... .......... .......... 45% 14.4M 29s
244050K .......... .......... .......... .......... .......... 45% 14.9M 29s
244100K .......... .......... .......... .......... .......... 45% 14.5M 29s
244150K .......... .......... .......... .......... .......... 45% 15.1M 29s
244200K .......... .......... .......... .......... .......... 45% 12.7M 29s
244250K .......... .......... .......... .......... .......... 45% 13.8M 29s
244300K .......... .......... .......... .......... .......... 45% 15.8M 29s
244350K .......... .......... .......... .......... .......... 45% 10.7M 29s
244400K .......... .......... .......... .......... .......... 45% 9.36M 29s
244450K .......... .......... .......... .......... .......... 45% 8.49M 29s
244500K .......... .......... .......... .......... .......... 45% 20.7M 29s
244550K .......... .......... .......... .......... .......... 45% 31.8M 29s
244600K .......... .......... .......... .......... .......... 45% 17.1M 29s
244650K .......... .......... .......... .......... .......... 45% 17.2M 29s
244700K .......... .......... .......... .......... .......... 45% 15.5M 29s
244750K .......... .......... .......... .......... .......... 45% 19.7M 29s
244800K .......... .......... .......... .......... .......... 45% 18.9M 29s
244850K .......... .......... .......... .......... .......... 45% 16.0M 29s
244900K .......... .......... .......... .......... .......... 45% 16.9M 29s
244950K .......... .......... .......... .......... .......... 45% 14.6M 28s
245000K .......... .......... .......... .......... .......... 45% 19.7M 28s
245050K .......... .......... .......... .......... .......... 45% 16.9M 28s
245100K .......... .......... .......... .......... .......... 45% 17.4M 28s
245150K .......... .......... .......... .......... .......... 45% 20.1M 28s
245200K .......... .......... .......... .......... .......... 45% 14.3M 28s
245250K .......... .......... .......... .......... .......... 45% 33.8M 28s
245300K .......... .......... .......... .......... .......... 45% 12.3M 28s
245350K .......... .......... .......... .......... .......... 45% 28.5M 28s
245400K .......... .......... .......... .......... .......... 45% 22.3M 28s
245450K .......... .......... .......... .......... .......... 45% 24.9M 28s
245500K .......... .......... .......... .......... .......... 45% 18.7M 28s
245550K .......... .......... .......... .......... .......... 45% 20.2M 28s
245600K .......... .......... .......... .......... .......... 45% 17.6M 28s
245650K .......... .......... .......... .......... .......... 45% 27.4M 28s
245700K .......... .......... .......... .......... .......... 45% 17.7M 28s
245750K .......... .......... .......... .......... .......... 45% 24.8M 28s
245800K .......... .......... .......... .......... .......... 45% 19.1M 28s
245850K .......... .......... .......... .......... .......... 45% 19.8M 28s
245900K .......... .......... .......... .......... .......... 45% 17.6M 28s
245950K .......... .......... .......... .......... .......... 45% 15.1M 28s
246000K .......... .......... .......... .......... .......... 45% 16.1M 28s
246050K .......... .......... .......... .......... .......... 45% 15.7M 28s
246100K .......... .......... .......... .......... .......... 45% 16.0M 28s
246150K .......... .......... .......... .......... .......... 45% 16.3M 28s
246200K .......... .......... .......... .......... .......... 45% 16.8M 28s
246250K .......... .......... .......... .......... .......... 45% 13.9M 28s
246300K .......... .......... .......... .......... .......... 45% 8.26M 28s
246350K .......... .......... .......... .......... .......... 45% 10.9M 28s
246400K .......... .......... .......... .......... .......... 45% 12.0M 28s
246450K .......... .......... .......... .......... .......... 45% 10.0M 28s
246500K .......... .......... .......... .......... .......... 45% 12.6M 28s
246550K .......... .......... .......... .......... .......... 45% 12.6M 28s
246600K .......... .......... .......... .......... .......... 45% 8.91M 28s
246650K .......... .......... .......... .......... .......... 45% 10.3M 28s
246700K .......... .......... .......... .......... .......... 45% 12.2M 28s
246750K .......... .......... .......... .......... .......... 45% 12.0M 28s
246800K .......... .......... .......... .......... .......... 45% 13.8M 28s
246850K .......... .......... .......... .......... .......... 45% 12.8M 28s
246900K .......... .......... .......... .......... .......... 45% 15.1M 28s
246950K .......... .......... .......... .......... .......... 45% 10.7M 28s
247000K .......... .......... .......... .......... .......... 45% 13.8M 28s
247050K .......... .......... .......... .......... .......... 45% 16.8M 28s
247100K .......... .......... .......... .......... .......... 45% 15.8M 28s
247150K .......... .......... .......... .......... .......... 45% 15.5M 28s
247200K .......... .......... .......... .......... .......... 46% 13.8M 28s
247250K .......... .......... .......... .......... .......... 46% 21.2M 28s
247300K .......... .......... .......... .......... .......... 46% 15.0M 28s
247350K .......... .......... .......... .......... .......... 46% 15.9M 28s
247400K .......... .......... .......... .......... .......... 46% 16.6M 28s
247450K .......... .......... .......... .......... .......... 46% 12.9M 28s
247500K .......... .......... .......... .......... .......... 46% 14.3M 28s
247550K .......... .......... .......... .......... .......... 46% 12.2M 28s
247600K .......... .......... .......... .......... .......... 46% 11.5M 28s
247650K .......... .......... .......... .......... .......... 46% 17.2M 28s
247700K .......... .......... .......... .......... .......... 46% 18.8M 28s
247750K .......... .......... .......... .......... .......... 46% 15.3M 28s
247800K .......... .......... .......... .......... .......... 46% 14.1M 28s
247850K .......... .......... .......... .......... .......... 46% 13.8M 28s
247900K .......... .......... .......... .......... .......... 46% 14.3M 28s
247950K .......... .......... .......... .......... .......... 46% 12.6M 28s
248000K .......... .......... .......... .......... .......... 46% 14.9M 28s
248050K .......... .......... .......... .......... .......... 46% 16.2M 28s
248100K .......... .......... .......... .......... .......... 46% 14.7M 28s
248150K .......... .......... .......... .......... .......... 46% 13.8M 28s
248200K .......... .......... .......... .......... .......... 46% 12.5M 28s
248250K .......... .......... .......... .......... .......... 46% 14.6M 28s
248300K .......... .......... .......... .......... .......... 46% 11.0M 28s
248350K .......... .......... .......... .......... .......... 46% 9.16M 28s
248400K .......... .......... .......... .......... .......... 46% 30.3M 28s
248450K .......... .......... .......... .......... .......... 46% 16.6M 28s
248500K .......... .......... .......... .......... .......... 46% 16.4M 28s
248550K .......... .......... .......... .......... .......... 46% 11.6M 28s
248600K .......... .......... .......... .......... .......... 46% 10.2M 28s
248650K .......... .......... .......... .......... .......... 46% 12.0M 28s
248700K .......... .......... .......... .......... .......... 46% 11.4M 28s
248750K .......... .......... .......... .......... .......... 46% 14.6M 28s
248800K .......... .......... .......... .......... .......... 46% 12.4M 28s
248850K .......... .......... .......... .......... .......... 46% 12.8M 28s
248900K .......... .......... .......... .......... .......... 46% 13.4M 28s
248950K .......... .......... .......... .......... .......... 46% 9.74M 28s
249000K .......... .......... .......... .......... .......... 46% 19.1M 28s
249050K .......... .......... .......... .......... .......... 46% 21.2M 28s
249100K .......... .......... .......... .......... .......... 46% 10.6M 28s
249150K .......... .......... .......... .......... .......... 46% 18.2M 28s
249200K .......... .......... .......... .......... .......... 46% 12.3M 28s
249250K .......... .......... .......... .......... .......... 46% 12.1M 28s
249300K .......... .......... .......... .......... .......... 46% 34.2M 28s
249350K .......... .......... .......... .......... .......... 46% 11.7M 28s
249400K .......... .......... .......... .......... .......... 46% 13.9M 28s
249450K .......... .......... .......... .......... .......... 46% 9.93M 28s
249500K .......... .......... .......... .......... .......... 46% 12.0M 28s
249550K .......... .......... .......... .......... .......... 46% 13.7M 28s
249600K .......... .......... .......... .......... .......... 46% 9.91M 28s
249650K .......... .......... .......... .......... .......... 46% 13.6M 28s
249700K .......... .......... .......... .......... .......... 46% 7.61M 28s
249750K .......... .......... .......... .......... .......... 46% 6.05M 28s
249800K .......... .......... .......... .......... .......... 46% 6.44M 28s
249850K .......... .......... .......... .......... .......... 46% 5.88M 28s
249900K .......... .......... .......... .......... .......... 46% 6.52M 28s
249950K .......... .......... .......... .......... .......... 46% 6.20M 28s
250000K .......... .......... .......... .......... .......... 46% 12.6M 28s
250050K .......... .......... .......... .......... .......... 46% 38.1M 28s
250100K .......... .......... .......... .......... .......... 46% 24.4M 28s
250150K .......... .......... .......... .......... .......... 46% 31.1M 28s
250200K .......... .......... .......... .......... .......... 46% 20.5M 28s
250250K .......... .......... .......... .......... .......... 46% 47.0M 28s
250300K .......... .......... .......... .......... .......... 46% 16.4M 28s
250350K .......... .......... .......... .......... .......... 46% 16.3M 28s
250400K .......... .......... .......... .......... .......... 46% 24.8M 28s
250450K .......... .......... .......... .......... .......... 46% 15.4M 28s
250500K .......... .......... .......... .......... .......... 46% 19.1M 28s
250550K .......... .......... .......... .......... .......... 46% 21.1M 28s
250600K .......... .......... .......... .......... .......... 46% 16.8M 28s
250650K .......... .......... .......... .......... .......... 46% 19.8M 28s
250700K .......... .......... .......... .......... .......... 46% 16.8M 28s
250750K .......... .......... .......... .......... .......... 46% 18.7M 28s
250800K .......... .......... .......... .......... .......... 46% 21.2M 28s
250850K .......... .......... .......... .......... .......... 46% 13.9M 28s
250900K .......... .......... .......... .......... .......... 46% 16.3M 28s
250950K .......... .......... .......... .......... .......... 46% 14.9M 28s
251000K .......... .......... .......... .......... .......... 46% 13.8M 28s
251050K .......... .......... .......... .......... .......... 46% 8.96M 28s
251100K .......... .......... .......... .......... .......... 46% 8.11M 28s
251150K .......... .......... .......... .......... .......... 46% 10.9M 28s
251200K .......... .......... .......... .......... .......... 46% 8.47M 28s
251250K .......... .......... .......... .......... .......... 46% 11.0M 28s
251300K .......... .......... .......... .......... .......... 46% 13.2M 28s
251350K .......... .......... .......... .......... .......... 46% 8.77M 28s
251400K .......... .......... .......... .......... .......... 46% 12.3M 28s
251450K .......... .......... .......... .......... .......... 46% 10.0M 28s
251500K .......... .......... .......... .......... .......... 46% 12.4M 28s
251550K .......... .......... .......... .......... .......... 46% 27.2M 28s
251600K .......... .......... .......... .......... .......... 46% 10.1M 28s
251650K .......... .......... .......... .......... .......... 46% 26.4M 28s
251700K .......... .......... .......... .......... .......... 46% 19.6M 28s
251750K .......... .......... .......... .......... .......... 46% 22.2M 28s
251800K .......... .......... .......... .......... .......... 46% 23.3M 28s
251850K .......... .......... .......... .......... .......... 46% 19.3M 28s
251900K .......... .......... .......... .......... .......... 46% 23.0M 28s
251950K .......... .......... .......... .......... .......... 46% 23.6M 28s
252000K .......... .......... .......... .......... .......... 46% 22.1M 28s
252050K .......... .......... .......... .......... .......... 46% 22.8M 28s
252100K .......... .......... .......... .......... .......... 46% 16.5M 28s
252150K .......... .......... .......... .......... .......... 46% 27.4M 28s
252200K .......... .......... .......... .......... .......... 46% 20.3M 28s
252250K .......... .......... .......... .......... .......... 46% 25.2M 28s
252300K .......... .......... .......... .......... .......... 46% 21.7M 28s
252350K .......... .......... .......... .......... .......... 46% 16.9M 28s
252400K .......... .......... .......... .......... .......... 46% 18.7M 28s
252450K .......... .......... .......... .......... .......... 46% 15.4M 28s
252500K .......... .......... .......... .......... .......... 46% 13.3M 28s
252550K .......... .......... .......... .......... .......... 47% 24.6M 28s
252600K .......... .......... .......... .......... .......... 47% 14.4M 28s
252650K .......... .......... .......... .......... .......... 47% 17.8M 27s
252700K .......... .......... .......... .......... .......... 47% 18.8M 27s
252750K .......... .......... .......... .......... .......... 47% 16.7M 27s
252800K .......... .......... .......... .......... .......... 47% 21.5M 27s
252850K .......... .......... .......... .......... .......... 47% 19.1M 27s
252900K .......... .......... .......... .......... .......... 47% 18.8M 27s
252950K .......... .......... .......... .......... .......... 47% 20.7M 27s
253000K .......... .......... .......... .......... .......... 47% 21.5M 27s
253050K .......... .......... .......... .......... .......... 47% 17.7M 27s
253100K .......... .......... .......... .......... .......... 47% 19.9M 27s
253150K .......... .......... .......... .......... .......... 47% 18.0M 27s
253200K .......... .......... .......... .......... .......... 47% 18.2M 27s
253250K .......... .......... .......... .......... .......... 47% 17.9M 27s
253300K .......... .......... .......... .......... .......... 47% 26.6M 27s
253350K .......... .......... .......... .......... .......... 47% 15.8M 27s
253400K .......... .......... .......... .......... .......... 47% 23.5M 27s
253450K .......... .......... .......... .......... .......... 47% 24.0M 27s
253500K .......... .......... .......... .......... .......... 47% 20.3M 27s
253550K .......... .......... .......... .......... .......... 47% 20.7M 27s
253600K .......... .......... .......... .......... .......... 47% 17.6M 27s
253650K .......... .......... .......... .......... .......... 47% 19.7M 27s
253700K .......... .......... .......... .......... .......... 47% 23.9M 27s
253750K .......... .......... .......... .......... .......... 47% 68.0M 27s
253800K .......... .......... .......... .......... .......... 47% 17.8M 27s
253850K .......... .......... .......... .......... .......... 47% 6.49M 27s
253900K .......... .......... .......... .......... .......... 47%  109M 27s
253950K .......... .......... .......... .......... .......... 47% 96.3M 27s
254000K .......... .......... .......... .......... .......... 47%  121M 27s
254050K .......... .......... .......... .......... .......... 47% 48.2M 27s
254100K .......... .......... .......... .......... .......... 47% 25.6M 27s
254150K .......... .......... .......... .......... .......... 47% 24.1M 27s
254200K .......... .......... .......... .......... .......... 47% 26.3M 27s
254250K .......... .......... .......... .......... .......... 47% 23.9M 27s
254300K .......... .......... .......... .......... .......... 47% 14.2M 27s
254350K .......... .......... .......... .......... .......... 47% 26.8M 27s
254400K .......... .......... .......... .......... .......... 47% 17.7M 27s
254450K .......... .......... .......... .......... .......... 47% 15.0M 27s
254500K .......... .......... .......... .......... .......... 47% 17.4M 27s
254550K .......... .......... .......... .......... .......... 47% 17.8M 27s
254600K .......... .......... .......... .......... .......... 47% 10.4M 27s
254650K .......... .......... .......... .......... .......... 47% 11.0M 27s
254700K .......... .......... .......... .......... .......... 47% 8.60M 27s
254750K .......... .......... .......... .......... .......... 47% 14.0M 27s
254800K .......... .......... .......... .......... .......... 47% 12.1M 27s
254850K .......... .......... .......... .......... .......... 47% 9.54M 27s
254900K .......... .......... .......... .......... .......... 47% 11.0M 27s
254950K .......... .......... .......... .......... .......... 47% 9.90M 27s
255000K .......... .......... .......... .......... .......... 47% 13.5M 27s
255050K .......... .......... .......... .......... .......... 47% 28.3M 27s
255100K .......... .......... .......... .......... .......... 47% 12.8M 27s
255150K .......... .......... .......... .......... .......... 47% 21.2M 27s
255200K .......... .......... .......... .......... .......... 47% 25.9M 27s
255250K .......... .......... .......... .......... .......... 47% 22.6M 27s
255300K .......... .......... .......... .......... .......... 47% 21.3M 27s
255350K .......... .......... .......... .......... .......... 47% 20.6M 27s
255400K .......... .......... .......... .......... .......... 47% 20.1M 27s
255450K .......... .......... .......... .......... .......... 47% 17.2M 27s
255500K .......... .......... .......... .......... .......... 47% 24.5M 27s
255550K .......... .......... .......... .......... .......... 47% 25.4M 27s
255600K .......... .......... .......... .......... .......... 47% 19.6M 27s
255650K .......... .......... .......... .......... .......... 47% 26.5M 27s
255700K .......... .......... .......... .......... .......... 47% 18.6M 27s
255750K .......... .......... .......... .......... .......... 47% 22.7M 27s
255800K .......... .......... .......... .......... .......... 47% 24.7M 27s
255850K .......... .......... .......... .......... .......... 47% 21.1M 27s
255900K .......... .......... .......... .......... .......... 47% 21.0M 27s
255950K .......... .......... .......... .......... .......... 47% 19.7M 27s
256000K .......... .......... .......... .......... .......... 47% 15.2M 27s
256050K .......... .......... .......... .......... .......... 47% 19.4M 27s
256100K .......... .......... .......... .......... .......... 47% 15.9M 27s
256150K .......... .......... .......... .......... .......... 47% 14.1M 27s
256200K .......... .......... .......... .......... .......... 47% 12.9M 27s
256250K .......... .......... .......... .......... .......... 47% 10.9M 27s
256300K .......... .......... .......... .......... .......... 47% 14.9M 27s
256350K .......... .......... .......... .......... .......... 47% 10.9M 27s
256400K .......... .......... .......... .......... .......... 47% 13.3M 27s
256450K .......... .......... .......... .......... .......... 47% 8.91M 27s
256500K .......... .......... .......... .......... .......... 47% 11.6M 27s
256550K .......... .......... .......... .......... .......... 47% 12.1M 27s
256600K .......... .......... .......... .......... .......... 47% 7.47M 27s
256650K .......... .......... .......... .......... .......... 47% 11.6M 27s
256700K .......... .......... .......... .......... .......... 47% 21.2M 27s
256750K .......... .......... .......... .......... .......... 47% 35.1M 27s
256800K .......... .......... .......... .......... .......... 47% 23.0M 27s
256850K .......... .......... .......... .......... .......... 47% 24.8M 27s
256900K .......... .......... .......... .......... .......... 47% 23.3M 27s
256950K .......... .......... .......... .......... .......... 47% 19.2M 27s
257000K .......... .......... .......... .......... .......... 47% 30.2M 27s
257050K .......... .......... .......... .......... .......... 47% 17.6M 27s
257100K .......... .......... .......... .......... .......... 47% 20.1M 27s
257150K .......... .......... .......... .......... .......... 47% 27.8M 27s
257200K .......... .......... .......... .......... .......... 47% 22.6M 27s
257250K .......... .......... .......... .......... .......... 47% 21.6M 27s
257300K .......... .......... .......... .......... .......... 47% 18.9M 27s
257350K .......... .......... .......... .......... .......... 47% 27.6M 27s
257400K .......... .......... .......... .......... .......... 47% 25.8M 27s
257450K .......... .......... .......... .......... .......... 47% 21.3M 27s
257500K .......... .......... .......... .......... .......... 47% 23.0M 27s
257550K .......... .......... .......... .......... .......... 47% 21.2M 27s
257600K .......... .......... .......... .......... .......... 47% 21.6M 27s
257650K .......... .......... .......... .......... .......... 47% 23.3M 27s
257700K .......... .......... .......... .......... .......... 47% 18.5M 27s
257750K .......... .......... .......... .......... .......... 47% 23.6M 27s
257800K .......... .......... .......... .......... .......... 47% 25.7M 27s
257850K .......... .......... .......... .......... .......... 47% 10.2M 27s
257900K .......... .......... .......... .......... .......... 48% 37.8M 27s
257950K .......... .......... .......... .......... .......... 48% 14.7M 27s
258000K .......... .......... .......... .......... .......... 48% 15.1M 27s
258050K .......... .......... .......... .......... .......... 48% 18.7M 27s
258100K .......... .......... .......... .......... .......... 48% 13.9M 27s
258150K .......... .......... .......... .......... .......... 48% 19.7M 27s
258200K .......... .......... .......... .......... .......... 48% 16.9M 27s
258250K .......... .......... .......... .......... .......... 48% 17.6M 27s
258300K .......... .......... .......... .......... .......... 48% 15.5M 27s
258350K .......... .......... .......... .......... .......... 48% 15.4M 27s
258400K .......... .......... .......... .......... .......... 48% 19.8M 27s
258450K .......... .......... .......... .......... .......... 48% 14.7M 27s
258500K .......... .......... .......... .......... .......... 48% 20.0M 27s
258550K .......... .......... .......... .......... .......... 48% 15.7M 27s
258600K .......... .......... .......... .......... .......... 48% 11.3M 27s
258650K .......... .......... .......... .......... .......... 48% 42.6M 27s
258700K .......... .......... .......... .......... .......... 48% 15.4M 27s
258750K .......... .......... .......... .......... .......... 48% 15.5M 27s
258800K .......... .......... .......... .......... .......... 48% 20.2M 27s
258850K .......... .......... .......... .......... .......... 48% 14.9M 27s
258900K .......... .......... .......... .......... .......... 48% 14.3M 27s
258950K .......... .......... .......... .......... .......... 48% 10.7M 27s
259000K .......... .......... .......... .......... .......... 48% 13.6M 27s
259050K .......... .......... .......... .......... .......... 48% 8.98M 27s
259100K .......... .......... .......... .......... .......... 48% 13.9M 27s
259150K .......... .......... .......... .......... .......... 48% 14.6M 27s
259200K .......... .......... .......... .......... .......... 48% 9.35M 27s
259250K .......... .......... .......... .......... .......... 48% 9.68M 27s
259300K .......... .......... .......... .......... .......... 48% 8.99M 27s
259350K .......... .......... .......... .......... .......... 48% 8.76M 27s
259400K .......... .......... .......... .......... .......... 48% 9.68M 27s
259450K .......... .......... .......... .......... .......... 48% 9.14M 27s
259500K .......... .......... .......... .......... .......... 48% 8.83M 27s
259550K .......... .......... .......... .......... .......... 48% 6.42M 27s
259600K .......... .......... .......... .......... .......... 48% 5.99M 27s
259650K .......... .......... .......... .......... .......... 48% 12.1M 27s
259700K .......... .......... .......... .......... .......... 48% 11.4M 27s
259750K .......... .......... .......... .......... .......... 48% 15.4M 27s
259800K .......... .......... .......... .......... .......... 48% 14.9M 27s
259850K .......... .......... .......... .......... .......... 48% 7.92M 27s
259900K .......... .......... .......... .......... .......... 48% 12.2M 27s
259950K .......... .......... .......... .......... .......... 48% 11.7M 27s
260000K .......... .......... .......... .......... .......... 48% 14.3M 27s
260050K .......... .......... .......... .......... .......... 48% 17.2M 27s
260100K .......... .......... .......... .......... .......... 48% 30.1M 26s
260150K .......... .......... .......... .......... .......... 48% 18.3M 26s
260200K .......... .......... .......... .......... .......... 48%  122M 26s
260250K .......... .......... .......... .......... .......... 48% 24.1M 26s
260300K .......... .......... .......... .......... .......... 48% 15.2M 26s
260350K .......... .......... .......... .......... .......... 48% 20.5M 26s
260400K .......... .......... .......... .......... .......... 48% 14.4M 26s
260450K .......... .......... .......... .......... .......... 48% 12.5M 26s
260500K .......... .......... .......... .......... .......... 48% 11.5M 26s
260550K .......... .......... .......... .......... .......... 48% 17.0M 26s
260600K .......... .......... .......... .......... .......... 48% 11.7M 26s
260650K .......... .......... .......... .......... .......... 48% 17.0M 26s
260700K .......... .......... .......... .......... .......... 48% 16.8M 26s
260750K .......... .......... .......... .......... .......... 48% 13.6M 26s
260800K .......... .......... .......... .......... .......... 48% 16.5M 26s
260850K .......... .......... .......... .......... .......... 48% 15.9M 26s
260900K .......... .......... .......... .......... .......... 48% 11.9M 26s
260950K .......... .......... .......... .......... .......... 48% 7.82M 26s
261000K .......... .......... .......... .......... .......... 48% 11.6M 26s
261050K .......... .......... .......... .......... .......... 48% 18.3M 26s
261100K .......... .......... .......... .......... .......... 48% 13.3M 26s
261150K .......... .......... .......... .......... .......... 48% 14.0M 26s
261200K .......... .......... .......... .......... .......... 48% 12.2M 26s
261250K .......... .......... .......... .......... .......... 48% 17.4M 26s
261300K .......... .......... .......... .......... .......... 48% 13.2M 26s
261350K .......... .......... .......... .......... .......... 48% 13.1M 26s
261400K .......... .......... .......... .......... .......... 48% 16.3M 26s
261450K .......... .......... .......... .......... .......... 48% 15.2M 26s
261500K .......... .......... .......... .......... .......... 48% 11.4M 26s
261550K .......... .......... .......... .......... .......... 48% 11.8M 26s
261600K .......... .......... .......... .......... .......... 48% 10.7M 26s
261650K .......... .......... .......... .......... .......... 48% 13.9M 26s
261700K .......... .......... .......... .......... .......... 48% 9.43M 26s
261750K .......... .......... .......... .......... .......... 48% 8.92M 26s
261800K .......... .......... .......... .......... .......... 48% 12.7M 26s
261850K .......... .......... .......... .......... .......... 48% 6.72M 26s
261900K .......... .......... .......... .......... .......... 48% 9.86M 26s
261950K .......... .......... .......... .......... .......... 48% 10.6M 26s
262000K .......... .......... .......... .......... .......... 48% 22.9M 26s
262050K .......... .......... .......... .......... .......... 48% 17.5M 26s
262100K .......... .......... .......... .......... .......... 48% 14.4M 26s
262150K .......... .......... .......... .......... .......... 48% 14.0M 26s
262200K .......... .......... .......... .......... .......... 48% 14.3M 26s
262250K .......... .......... .......... .......... .......... 48% 15.6M 26s
262300K .......... .......... .......... .......... .......... 48% 17.7M 26s
262350K .......... .......... .......... .......... .......... 48% 15.3M 26s
262400K .......... .......... .......... .......... .......... 48% 17.8M 26s
262450K .......... .......... .......... .......... .......... 48% 12.6M 26s
262500K .......... .......... .......... .......... .......... 48% 17.7M 26s
262550K .......... .......... .......... .......... .......... 48% 14.4M 26s
262600K .......... .......... .......... .......... .......... 48% 19.3M 26s
262650K .......... .......... .......... .......... .......... 48% 19.1M 26s
262700K .......... .......... .......... .......... .......... 48% 13.7M 26s
262750K .......... .......... .......... .......... .......... 48% 11.7M 26s
262800K .......... .......... .......... .......... .......... 48% 19.3M 26s
262850K .......... .......... .......... .......... .......... 48% 12.5M 26s
262900K .......... .......... .......... .......... .......... 48% 11.5M 26s
262950K .......... .......... .......... .......... .......... 48% 12.4M 26s
263000K .......... .......... .......... .......... .......... 48% 14.1M 26s
263050K .......... .......... .......... .......... .......... 48% 15.0M 26s
263100K .......... .......... .......... .......... .......... 48% 10.2M 26s
263150K .......... .......... .......... .......... .......... 48% 14.0M 26s
263200K .......... .......... .......... .......... .......... 48% 10.5M 26s
263250K .......... .......... .......... .......... .......... 48% 12.0M 26s
263300K .......... .......... .......... .......... .......... 49% 9.63M 26s
263350K .......... .......... .......... .......... .......... 49% 15.9M 26s
263400K .......... .......... .......... .......... .......... 49% 14.5M 26s
263450K .......... .......... .......... .......... .......... 49% 16.8M 26s
263500K .......... .......... .......... .......... .......... 49% 16.7M 26s
263550K .......... .......... .......... .......... .......... 49% 54.3M 26s
263600K .......... .......... .......... .......... .......... 49% 15.7M 26s
263650K .......... .......... .......... .......... .......... 49% 25.3M 26s
263700K .......... .......... .......... .......... .......... 49% 18.0M 26s
263750K .......... .......... .......... .......... .......... 49% 21.2M 26s
263800K .......... .......... .......... .......... .......... 49% 24.3M 26s
263850K .......... .......... .......... .......... .......... 49% 19.8M 26s
263900K .......... .......... .......... .......... .......... 49% 30.6M 26s
263950K .......... .......... .......... .......... .......... 49% 18.6M 26s
264000K .......... .......... .......... .......... .......... 49% 30.0M 26s
264050K .......... .......... .......... .......... .......... 49% 26.8M 26s
264100K .......... .......... .......... .......... .......... 49% 22.4M 26s
264150K .......... .......... .......... .......... .......... 49% 25.0M 26s
264200K .......... .......... .......... .......... .......... 49% 22.6M 26s
264250K .......... .......... .......... .......... .......... 49% 26.2M 26s
264300K .......... .......... .......... .......... .......... 49% 27.0M 26s
264350K .......... .......... .......... .......... .......... 49% 29.0M 26s
264400K .......... .......... .......... .......... .......... 49% 51.2M 26s
264450K .......... .......... .......... .......... .......... 49% 37.8M 26s
264500K .......... .......... .......... .......... .......... 49%  137M 26s
264550K .......... .......... .......... .......... .......... 49% 22.6M 26s
264600K .......... .......... .......... .......... .......... 49% 58.7M 26s
264650K .......... .......... .......... .......... .......... 49%  123M 26s
264700K .......... .......... .......... .......... .......... 49% 32.6M 26s
264750K .......... .......... .......... .......... .......... 49% 72.3M 26s
264800K .......... .......... .......... .......... .......... 49% 41.6M 26s
264850K .......... .......... .......... .......... .......... 49% 37.3M 26s
264900K .......... .......... .......... .......... .......... 49% 54.9M 26s
264950K .......... .......... .......... .......... .......... 49% 24.8M 26s
265000K .......... .......... .......... .......... .......... 49% 26.1M 26s
265050K .......... .......... .......... .......... .......... 49% 39.9M 26s
265100K .......... .......... .......... .......... .......... 49% 23.9M 26s
265150K .......... .......... .......... .......... .......... 49% 29.9M 26s
265200K .......... .......... .......... .......... .......... 49% 25.7M 26s
265250K .......... .......... .......... .......... .......... 49% 23.9M 26s
265300K .......... .......... .......... .......... .......... 49% 33.1M 26s
265350K .......... .......... .......... .......... .......... 49% 25.9M 26s
265400K .......... .......... .......... .......... .......... 49% 29.7M 26s
265450K .......... .......... .......... .......... .......... 49% 21.3M 26s
265500K .......... .......... .......... .......... .......... 49% 35.5M 26s
265550K .......... .......... .......... .......... .......... 49% 29.1M 26s
265600K .......... .......... .......... .......... .......... 49% 26.7M 26s
265650K .......... .......... .......... .......... .......... 49% 31.4M 26s
265700K .......... .......... .......... .......... .......... 49% 25.3M 26s
265750K .......... .......... .......... .......... .......... 49% 23.1M 26s
265800K .......... .......... .......... .......... .......... 49% 22.1M 26s
265850K .......... .......... .......... .......... .......... 49% 21.1M 26s
265900K .......... .......... .......... .......... .......... 49% 19.9M 26s
265950K .......... .......... .......... .......... .......... 49% 18.5M 26s
266000K .......... .......... .......... .......... .......... 49% 31.1M 26s
266050K .......... .......... .......... .......... .......... 49% 23.8M 26s
266100K .......... .......... .......... .......... .......... 49% 24.6M 26s
266150K .......... .......... .......... .......... .......... 49% 26.4M 26s
266200K .......... .......... .......... .......... .......... 49% 21.9M 26s
266250K .......... .......... .......... .......... .......... 49% 22.7M 26s
266300K .......... .......... .......... .......... .......... 49% 27.0M 26s
266350K .......... .......... .......... .......... .......... 49% 19.9M 26s
266400K .......... .......... .......... .......... .......... 49% 29.2M 26s
266450K .......... .......... .......... .......... .......... 49% 22.2M 26s
266500K .......... .......... .......... .......... .......... 49% 28.4M 26s
266550K .......... .......... .......... .......... .......... 49% 25.6M 26s
266600K .......... .......... .......... .......... .......... 49% 21.7M 26s
266650K .......... .......... .......... .......... .......... 49% 4.74M 26s
266700K .......... .......... .......... .......... .......... 49%  127M 26s
266750K .......... .......... .......... .......... .......... 49%  106M 26s
266800K .......... .......... .......... .......... .......... 49%  122M 26s
266850K .......... .......... .......... .......... .......... 49% 24.5M 26s
266900K .......... .......... .......... .......... .......... 49% 22.7M 26s
266950K .......... .......... .......... .......... .......... 49% 13.8M 26s
267000K .......... .......... .......... .......... .......... 49% 17.3M 26s
267050K .......... .......... .......... .......... .......... 49% 23.0M 26s
267100K .......... .......... .......... .......... .......... 49% 14.0M 26s
267150K .......... .......... .......... .......... .......... 49% 22.0M 26s
267200K .......... .......... .......... .......... .......... 49% 16.6M 26s
267250K .......... .......... .......... .......... .......... 49% 17.4M 26s
267300K .......... .......... .......... .......... .......... 49% 22.2M 26s
267350K .......... .......... .......... .......... .......... 49% 20.5M 25s
267400K .......... .......... .......... .......... .......... 49% 21.7M 25s
267450K .......... .......... .......... .......... .......... 49% 15.0M 25s
267500K .......... .......... .......... .......... .......... 49% 77.6M 25s
267550K .......... .......... .......... .......... .......... 49% 18.9M 25s
267600K .......... .......... .......... .......... .......... 49% 13.8M 25s
267650K .......... .......... .......... .......... .......... 49% 23.6M 25s
267700K .......... .......... .......... .......... .......... 49% 15.2M 25s
267750K .......... .......... .......... .......... .......... 49% 22.1M 25s
267800K .......... .......... .......... .......... .......... 49% 20.6M 25s
267850K .......... .......... .......... .......... .......... 49% 15.1M 25s
267900K .......... .......... .......... .......... .......... 49% 20.2M 25s
267950K .......... .......... .......... .......... .......... 49% 15.5M 25s
268000K .......... .......... .......... .......... .......... 49% 18.7M 25s
268050K .......... .......... .......... .......... .......... 49% 25.4M 25s
268100K .......... .......... .......... .......... .......... 49% 15.7M 25s
268150K .......... .......... .......... .......... .......... 49% 26.0M 25s
268200K .......... .......... .......... .......... .......... 49% 16.7M 25s
268250K .......... .......... .......... .......... .......... 49% 22.2M 25s
268300K .......... .......... .......... .......... .......... 49% 19.6M 25s
268350K .......... .......... .......... .......... .......... 49% 16.4M 25s
268400K .......... .......... .......... .......... .......... 49% 31.0M 25s
268450K .......... .......... .......... .......... .......... 49% 27.7M 25s
268500K .......... .......... .......... .......... .......... 49% 69.5M 25s
268550K .......... .......... .......... .......... .......... 49% 32.5M 25s
268600K .......... .......... .......... .......... .......... 49% 20.7M 25s
268650K .......... .......... .......... .......... .......... 50% 30.6M 25s
268700K .......... .......... .......... .......... .......... 50% 33.5M 25s
268750K .......... .......... .......... .......... .......... 50% 34.6M 25s
268800K .......... .......... .......... .......... .......... 50% 22.2M 25s
268850K .......... .......... .......... .......... .......... 50% 15.6M 25s
268900K .......... .......... .......... .......... .......... 50% 21.0M 25s
268950K .......... .......... .......... .......... .......... 50% 19.6M 25s
269000K .......... .......... .......... .......... .......... 50% 27.9M 25s
269050K .......... .......... .......... .......... .......... 50% 24.0M 25s
269100K .......... .......... .......... .......... .......... 50% 20.1M 25s
269150K .......... .......... .......... .......... .......... 50% 29.5M 25s
269200K .......... .......... .......... .......... .......... 50% 18.0M 25s
269250K .......... .......... .......... .......... .......... 50% 21.3M 25s
269300K .......... .......... .......... .......... .......... 50% 18.0M 25s
269350K .......... .......... .......... .......... .......... 50% 20.9M 25s
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269450K .......... .......... .......... .......... .......... 50% 19.7M 25s
269500K .......... .......... .......... .......... .......... 50% 29.7M 25s
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269650K .......... .......... .......... .......... .......... 50% 33.7M 25s
269700K .......... .......... .......... .......... .......... 50% 30.7M 25s
269750K .......... .......... .......... .......... .......... 50% 22.4M 25s
269800K .......... .......... .......... .......... .......... 50% 21.2M 25s
269850K .......... .......... .......... .......... .......... 50% 28.6M 25s
269900K .......... .......... .......... .......... .......... 50% 22.5M 25s
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270000K .......... .......... .......... .......... .......... 50% 21.4M 25s
270050K .......... .......... .......... .......... .......... 50% 24.7M 25s
270100K .......... .......... .......... .......... .......... 50% 18.0M 25s
270150K .......... .......... .......... .......... .......... 50% 25.6M 25s
270200K .......... .......... .......... .......... .......... 50% 14.6M 25s
270250K .......... .......... .......... .......... .......... 50% 30.5M 25s
270300K .......... .......... .......... .......... .......... 50% 21.4M 25s
270350K .......... .......... .......... .......... .......... 50% 16.4M 25s
270400K .......... .......... .......... .......... .......... 50% 21.5M 25s
270450K .......... .......... .......... .......... .......... 50% 18.1M 25s
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270550K .......... .......... .......... .......... .......... 50% 12.5M 25s
270600K .......... .......... .......... .......... .......... 50% 12.5M 25s
270650K .......... .......... .......... .......... .......... 50% 6.72M 25s
270700K .......... .......... .......... .......... .......... 50% 5.08M 25s
270750K .......... .......... .......... .......... .......... 50% 6.28M 25s
270800K .......... .......... .......... .......... .......... 50% 9.94M 25s
270850K .......... .......... .......... .......... .......... 50% 7.88M 25s
270900K .......... .......... .......... .......... .......... 50% 9.79M 25s
270950K .......... .......... .......... .......... .......... 50% 7.59M 25s
271000K .......... .......... .......... .......... .......... 50% 6.27M 25s
271050K .......... .......... .......... .......... .......... 50% 5.08M 25s
271100K .......... .......... .......... .......... .......... 50% 8.07M 25s
271150K .......... .......... .......... .......... .......... 50% 10.8M 25s
271200K .......... .......... .......... .......... .......... 50% 8.04M 25s
271250K .......... .......... .......... .......... .......... 50% 10.2M 25s
271300K .......... .......... .......... .......... .......... 50% 10.3M 25s
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271400K .......... .......... .......... .......... .......... 50% 8.94M 25s
271450K .......... .......... .......... .......... .......... 50% 12.1M 25s
271500K .......... .......... .......... .......... .......... 50% 9.80M 25s
271550K .......... .......... .......... .......... .......... 50% 22.9M 25s
271600K .......... .......... .......... .......... .......... 50% 10.9M 25s
271650K .......... .......... .......... .......... .......... 50% 15.0M 25s
271700K .......... .......... .......... .......... .......... 50% 13.1M 25s
271750K .......... .......... .......... .......... .......... 50% 12.0M 25s
271800K .......... .......... .......... .......... .......... 50% 15.8M 25s
271850K .......... .......... .......... .......... .......... 50% 13.5M 25s
271900K .......... .......... .......... .......... .......... 50% 17.4M 25s
271950K .......... .......... .......... .......... .......... 50% 12.9M 25s
272000K .......... .......... .......... .......... .......... 50% 14.2M 25s
272050K .......... .......... .......... .......... .......... 50% 14.6M 25s
272100K .......... .......... .......... .......... .......... 50% 15.2M 25s
272150K .......... .......... .......... .......... .......... 50% 18.2M 25s
272200K .......... .......... .......... .......... .......... 50% 14.8M 25s
272250K .......... .......... .......... .......... .......... 50% 13.2M 25s
272300K .......... .......... .......... .......... .......... 50% 24.8M 25s
272350K .......... .......... .......... .......... .......... 50% 18.9M 25s
272400K .......... .......... .......... .......... .......... 50% 14.4M 25s
272450K .......... .......... .......... .......... .......... 50% 11.4M 25s
272500K .......... .......... .......... .......... .......... 50% 11.0M 25s
272550K .......... .......... .......... .......... .......... 50% 11.3M 25s
272600K .......... .......... .......... .......... .......... 50% 9.87M 25s
272650K .......... .......... .......... .......... .......... 50% 12.1M 25s
272700K .......... .......... .......... .......... .......... 50% 8.12M 25s
272750K .......... .......... .......... .......... .......... 50% 11.4M 25s
272800K .......... .......... .......... .......... .......... 50% 12.8M 25s
272850K .......... .......... .......... .......... .......... 50% 8.85M 25s
272900K .......... .......... .......... .......... .......... 50% 9.72M 25s
272950K .......... .......... .......... .......... .......... 50% 13.5M 25s
273000K .......... .......... .......... .......... .......... 50% 61.3M 25s
273050K .......... .......... .......... .......... .......... 50% 21.8M 25s
273100K .......... .......... .......... .......... .......... 50% 15.1M 25s
273150K .......... .......... .......... .......... .......... 50% 18.7M 25s
273200K .......... .......... .......... .......... .......... 50% 14.3M 25s
273250K .......... .......... .......... .......... .......... 50% 15.1M 25s
273300K .......... .......... .......... .......... .......... 50% 21.0M 25s
273350K .......... .......... .......... .......... .......... 50% 17.0M 25s
273400K .......... .......... .......... .......... .......... 50% 18.5M 25s
273450K .......... .......... .......... .......... .......... 50% 13.8M 25s
273500K .......... .......... .......... .......... .......... 50% 20.2M 25s
273550K .......... .......... .......... .......... .......... 50% 18.1M 25s
273600K .......... .......... .......... .......... .......... 50% 16.5M 25s
273650K .......... .......... .......... .......... .......... 50% 22.1M 25s
273700K .......... .......... .......... .......... .......... 50% 9.24M 25s
273750K .......... .......... .......... .......... .......... 50% 9.35M 25s
273800K .......... .......... .......... .......... .......... 50% 12.6M 25s
273850K .......... .......... .......... .......... .......... 50% 15.7M 25s
273900K .......... .......... .......... .......... .......... 50% 14.3M 25s
273950K .......... .......... .......... .......... .......... 50% 14.0M 25s
274000K .......... .......... .......... .......... .......... 50% 14.2M 25s
274050K .......... .......... .......... .......... .......... 51% 12.6M 25s
274100K .......... .......... .......... .......... .......... 51% 14.5M 25s
274150K .......... .......... .......... .......... .......... 51% 14.1M 25s
274200K .......... .......... .......... .......... .......... 51% 13.2M 25s
274250K .......... .......... .......... .......... .......... 51% 15.8M 25s
274300K .......... .......... .......... .......... .......... 51% 14.9M 25s
274350K .......... .......... .......... .......... .......... 51% 8.06M 25s
274400K .......... .......... .......... .......... .......... 51% 29.3M 25s
274450K .......... .......... .......... .......... .......... 51% 14.8M 25s
274500K .......... .......... .......... .......... .......... 51% 12.5M 25s
274550K .......... .......... .......... .......... .......... 51% 21.4M 25s
274600K .......... .......... .......... .......... .......... 51% 11.5M 25s
274650K .......... .......... .......... .......... .......... 51% 14.8M 25s
274700K .......... .......... .......... .......... .......... 51% 12.0M 25s
274750K .......... .......... .......... .......... .......... 51% 12.7M 25s
274800K .......... .......... .......... .......... .......... 51% 12.0M 25s
274850K .......... .......... .......... .......... .......... 51% 15.2M 25s
274900K .......... .......... .......... .......... .......... 51% 13.7M 25s
274950K .......... .......... .......... .......... .......... 51% 12.5M 25s
275000K .......... .......... .......... .......... .......... 51% 8.22M 25s
275050K .......... .......... .......... .......... .......... 51% 10.7M 25s
275100K .......... .......... .......... .......... .......... 51% 14.2M 25s
275150K .......... .......... .......... .......... .......... 51% 18.6M 25s
275200K .......... .......... .......... .......... .......... 51% 11.9M 25s
275250K .......... .......... .......... .......... .......... 51% 13.3M 25s
275300K .......... .......... .......... .......... .......... 51% 15.1M 25s
275350K .......... .......... .......... .......... .......... 51% 10.6M 25s
275400K .......... .......... .......... .......... .......... 51% 16.9M 25s
275450K .......... .......... .......... .......... .......... 51% 13.1M 25s
275500K .......... .......... .......... .......... .......... 51% 15.0M 25s
275550K .......... .......... .......... .......... .......... 51% 14.8M 25s
275600K .......... .......... .......... .......... .......... 51% 14.0M 25s
275650K .......... .......... .......... .......... .......... 51% 14.2M 24s
275700K .......... .......... .......... .......... .......... 51% 8.01M 24s
275750K .......... .......... .......... .......... .......... 51% 9.07M 24s
275800K .......... .......... .......... .......... .......... 51% 14.2M 24s
275850K .......... .......... .......... .......... .......... 51% 9.87M 24s
275900K .......... .......... .......... .......... .......... 51% 13.0M 24s
275950K .......... .......... .......... .......... .......... 51% 10.5M 24s
276000K .......... .......... .......... .......... .......... 51% 11.9M 24s
276050K .......... .......... .......... .......... .......... 51% 13.2M 24s
276100K .......... .......... .......... .......... .......... 51% 10.4M 24s
276150K .......... .......... .......... .......... .......... 51% 14.6M 24s
276200K .......... .......... .......... .......... .......... 51% 17.9M 24s
276250K .......... .......... .......... .......... .......... 51% 25.4M 24s
276300K .......... .......... .......... .......... .......... 51% 23.0M 24s
276350K .......... .......... .......... .......... .......... 51% 11.8M 24s
276400K .......... .......... .......... .......... .......... 51% 19.8M 24s
276450K .......... .......... .......... .......... .......... 51% 19.9M 24s
276500K .......... .......... .......... .......... .......... 51% 42.2M 24s
276550K .......... .......... .......... .......... .......... 51% 20.6M 24s
276600K .......... .......... .......... .......... .......... 51% 17.8M 24s
276650K .......... .......... .......... .......... .......... 51% 24.4M 24s
276700K .......... .......... .......... .......... .......... 51% 16.5M 24s
276750K .......... .......... .......... .......... .......... 51% 15.2M 24s
276800K .......... .......... .......... .......... .......... 51% 24.4M 24s
276850K .......... .......... .......... .......... .......... 51% 14.9M 24s
276900K .......... .......... .......... .......... .......... 51% 16.9M 24s
276950K .......... .......... .......... .......... .......... 51% 14.3M 24s
277000K .......... .......... .......... .......... .......... 51% 17.2M 24s
277050K .......... .......... .......... .......... .......... 51% 18.8M 24s
277100K .......... .......... .......... .......... .......... 51% 15.1M 24s
277150K .......... .......... .......... .......... .......... 51% 11.6M 24s
277200K .......... .......... .......... .......... .......... 51% 7.83M 24s
277250K .......... .......... .......... .......... .......... 51% 9.89M 24s
277300K .......... .......... .......... .......... .......... 51% 10.8M 24s
277350K .......... .......... .......... .......... .......... 51% 8.14M 24s
277400K .......... .......... .......... .......... .......... 51% 9.30M 24s
277450K .......... .......... .......... .......... .......... 51% 8.31M 24s
277500K .......... .......... .......... .......... .......... 51% 9.13M 24s
277550K .......... .......... .......... .......... .......... 51% 8.98M 24s
277600K .......... .......... .......... .......... .......... 51% 7.24M 24s
277650K .......... .......... .......... .......... .......... 51% 10.9M 24s
277700K .......... .......... .......... .......... .......... 51% 11.9M 24s
277750K .......... .......... .......... .......... .......... 51% 29.1M 24s
277800K .......... .......... .......... .......... .......... 51% 27.7M 24s
277850K .......... .......... .......... .......... .......... 51% 11.2M 24s
277900K .......... .......... .......... .......... .......... 51% 15.5M 24s
277950K .......... .......... .......... .......... .......... 51% 12.4M 24s
278000K .......... .......... .......... .......... .......... 51% 14.6M 24s
278050K .......... .......... .......... .......... .......... 51% 13.9M 24s
278100K .......... .......... .......... .......... .......... 51% 12.4M 24s
278150K .......... .......... .......... .......... .......... 51% 14.6M 24s
278200K .......... .......... .......... .......... .......... 51% 13.2M 24s
278250K .......... .......... .......... .......... .......... 51% 12.8M 24s
278300K .......... .......... .......... .......... .......... 51% 10.8M 24s
278350K .......... .......... .......... .......... .......... 51% 7.26M 24s
278400K .......... .......... .......... .......... .......... 51% 16.0M 24s
278450K .......... .......... .......... .......... .......... 51% 8.17M 24s
278500K .......... .......... .......... .......... .......... 51% 9.43M 24s
278550K .......... .......... .......... .......... .......... 51% 9.37M 24s
278600K .......... .......... .......... .......... .......... 51% 9.71M 24s
278650K .......... .......... .......... .......... .......... 51% 8.57M 24s
278700K .......... .......... .......... .......... .......... 51% 9.12M 24s
278750K .......... .......... .......... .......... .......... 51% 9.36M 24s
278800K .......... .......... .......... .......... .......... 51% 12.9M 24s
278850K .......... .......... .......... .......... .......... 51% 11.5M 24s
278900K .......... .......... .......... .......... .......... 51% 24.1M 24s
278950K .......... .......... .......... .......... .......... 51% 14.9M 24s
279000K .......... .......... .......... .......... .......... 51% 16.9M 24s
279050K .......... .......... .......... .......... .......... 51% 18.3M 24s
279100K .......... .......... .......... .......... .......... 51% 23.6M 24s
279150K .......... .......... .......... .......... .......... 51% 16.9M 24s
279200K .......... .......... .......... .......... .......... 51% 14.7M 24s
279250K .......... .......... .......... .......... .......... 51% 20.9M 24s
279300K .......... .......... .......... .......... .......... 51% 16.4M 24s
279350K .......... .......... .......... .......... .......... 51% 16.9M 24s
279400K .......... .......... .......... .......... .......... 52% 16.4M 24s
279450K .......... .......... .......... .......... .......... 52% 15.7M 24s
279500K .......... .......... .......... .......... .......... 52% 19.7M 24s
279550K .......... .......... .......... .......... .......... 52% 17.2M 24s
279600K .......... .......... .......... .......... .......... 52% 14.9M 24s
279650K .......... .......... .......... .......... .......... 52% 15.7M 24s
279700K .......... .......... .......... .......... .......... 52% 12.5M 24s
279750K .......... .......... .......... .......... .......... 52% 11.7M 24s
279800K .......... .......... .......... .......... .......... 52% 17.3M 24s
279850K .......... .......... .......... .......... .......... 52% 11.0M 24s
279900K .......... .......... .......... .......... .......... 52% 19.9M 24s
279950K .......... .......... .......... .......... .......... 52% 14.7M 24s
280000K .......... .......... .......... .......... .......... 52% 16.7M 24s
280050K .......... .......... .......... .......... .......... 52% 15.5M 24s
280100K .......... .......... .......... .......... .......... 52% 14.4M 24s
280150K .......... .......... .......... .......... .......... 52% 15.2M 24s
280200K .......... .......... .......... .......... .......... 52% 15.0M 24s
280250K .......... .......... .......... .......... .......... 52% 16.2M 24s
280300K .......... .......... .......... .......... .......... 52% 15.1M 24s
280350K .......... .......... .......... .......... .......... 52% 11.8M 24s
280400K .......... .......... .......... .......... .......... 52% 17.1M 24s
280450K .......... .......... .......... .......... .......... 52% 14.4M 24s
280500K .......... .......... .......... .......... .......... 52% 17.4M 24s
280550K .......... .......... .......... .......... .......... 52% 14.2M 24s
280600K .......... .......... .......... .......... .......... 52% 8.11M 24s
280650K .......... .......... .......... .......... .......... 52% 7.71M 24s
280700K .......... .......... .......... .......... .......... 52% 14.8M 24s
280750K .......... .......... .......... .......... .......... 52% 14.0M 24s
280800K .......... .......... .......... .......... .......... 52% 14.4M 24s
280850K .......... .......... .......... .......... .......... 52% 36.5M 24s
280900K .......... .......... .......... .......... .......... 52% 13.0M 24s
280950K .......... .......... .......... .......... .......... 52% 16.5M 24s
281000K .......... .......... .......... .......... .......... 52% 16.7M 24s
281050K .......... .......... .......... .......... .......... 52% 16.7M 24s
281100K .......... .......... .......... .......... .......... 52% 12.1M 24s
281150K .......... .......... .......... .......... .......... 52% 19.0M 24s
281200K .......... .......... .......... .......... .......... 52% 12.4M 24s
281250K .......... .......... .......... .......... .......... 52% 21.5M 24s
281300K .......... .......... .......... .......... .......... 52% 14.7M 24s
281350K .......... .......... .......... .......... .......... 52% 13.3M 24s
281400K .......... .......... .......... .......... .......... 52% 19.2M 24s
281450K .......... .......... .......... .......... .......... 52% 12.4M 24s
281500K .......... .......... .......... .......... .......... 52% 18.4M 24s
281550K .......... .......... .......... .......... .......... 52% 20.8M 24s
281600K .......... .......... .......... .......... .......... 52% 16.3M 24s
281650K .......... .......... .......... .......... .......... 52% 19.9M 24s
281700K .......... .......... .......... .......... .......... 52% 12.6M 24s
281750K .......... .......... .......... .......... .......... 52% 9.80M 24s
281800K .......... .......... .......... .......... .......... 52%  123M 24s
281850K .......... .......... .......... .......... .......... 52% 13.7M 24s
281900K .......... .......... .......... .......... .......... 52% 17.5M 24s
281950K .......... .......... .......... .......... .......... 52% 11.1M 24s
282000K .......... .......... .......... .......... .......... 52% 21.3M 24s
282050K .......... .......... .......... .......... .......... 52% 13.3M 24s
282100K .......... .......... .......... .......... .......... 52% 15.0M 24s
282150K .......... .......... .......... .......... .......... 52% 15.6M 24s
282200K .......... .......... .......... .......... .......... 52% 12.9M 24s
282250K .......... .......... .......... .......... .......... 52% 15.6M 24s
282300K .......... .......... .......... .......... .......... 52% 16.2M 24s
282350K .......... .......... .......... .......... .......... 52% 15.0M 24s
282400K .......... .......... .......... .......... .......... 52% 16.7M 24s
282450K .......... .......... .......... .......... .......... 52% 12.5M 24s
282500K .......... .......... .......... .......... .......... 52% 12.9M 24s
282550K .......... .......... .......... .......... .......... 52% 16.6M 24s
282600K .......... .......... .......... .......... .......... 52% 25.4M 24s
282650K .......... .......... .......... .......... .......... 52% 26.6M 24s
282700K .......... .......... .......... .......... .......... 52% 14.1M 24s
282750K .......... .......... .......... .......... .......... 52% 43.7M 24s
282800K .......... .......... .......... .......... .......... 52% 29.2M 24s
282850K .......... .......... .......... .......... .......... 52% 20.0M 24s
282900K .......... .......... .......... .......... .......... 52% 25.0M 24s
282950K .......... .......... .......... .......... .......... 52% 20.1M 24s
283000K .......... .......... .......... .......... .......... 52% 22.2M 24s
283050K .......... .......... .......... .......... .......... 52% 20.7M 24s
283100K .......... .......... .......... .......... .......... 52% 23.4M 24s
283150K .......... .......... .......... .......... .......... 52% 22.8M 24s
283200K .......... .......... .......... .......... .......... 52% 18.3M 24s
283250K .......... .......... .......... .......... .......... 52% 19.4M 24s
283300K .......... .......... .......... .......... .......... 52% 30.0M 24s
283350K .......... .......... .......... .......... .......... 52% 20.5M 24s
283400K .......... .......... .......... .......... .......... 52% 28.3M 24s
283450K .......... .......... .......... .......... .......... 52% 17.2M 24s
283500K .......... .......... .......... .......... .......... 52% 29.3M 24s
283550K .......... .......... .......... .......... .......... 52% 27.0M 24s
283600K .......... .......... .......... .......... .......... 52% 19.5M 24s
283650K .......... .......... .......... .......... .......... 52% 26.1M 24s
283700K .......... .......... .......... .......... .......... 52% 21.9M 24s
283750K .......... .......... .......... .......... .......... 52% 55.2M 24s
283800K .......... .......... .......... .......... .......... 52% 19.7M 24s
283850K .......... .......... .......... .......... .......... 52% 25.6M 24s
283900K .......... .......... .......... .......... .......... 52% 17.8M 24s
283950K .......... .......... .......... .......... .......... 52%  131M 24s
284000K .......... .......... .......... .......... .......... 52% 14.9M 24s
284050K .......... .......... .......... .......... .......... 52%  124M 24s
284100K .......... .......... .......... .......... .......... 52% 22.2M 23s
284150K .......... .......... .......... .......... .......... 52% 28.1M 23s
284200K .......... .......... .......... .......... .......... 52% 32.1M 23s
284250K .......... .......... .......... .......... .......... 52% 26.1M 23s
284300K .......... .......... .......... .......... .......... 52% 21.9M 23s
284350K .......... .......... .......... .......... .......... 52% 18.8M 23s
284400K .......... .......... .......... .......... .......... 52% 26.8M 23s
284450K .......... .......... .......... .......... .......... 52% 20.6M 23s
284500K .......... .......... .......... .......... .......... 52% 25.3M 23s
284550K .......... .......... .......... .......... .......... 52% 25.7M 23s
284600K .......... .......... .......... .......... .......... 52% 20.8M 23s
284650K .......... .......... .......... .......... .......... 52% 19.3M 23s
284700K .......... .......... .......... .......... .......... 52% 23.4M 23s
284750K .......... .......... .......... .......... .......... 52% 26.0M 23s
284800K .......... .......... .......... .......... .......... 53% 24.5M 23s
284850K .......... .......... .......... .......... .......... 53% 25.2M 23s
284900K .......... .......... .......... .......... .......... 53% 21.1M 23s
284950K .......... .......... .......... .......... .......... 53% 17.2M 23s
285000K .......... .......... .......... .......... .......... 53% 17.5M 23s
285050K .......... .......... .......... .......... .......... 53% 20.7M 23s
285100K .......... .......... .......... .......... .......... 53% 33.0M 23s
285150K .......... .......... .......... .......... .......... 53% 20.8M 23s
285200K .......... .......... .......... .......... .......... 53% 19.8M 23s
285250K .......... .......... .......... .......... .......... 53% 18.4M 23s
285300K .......... .......... .......... .......... .......... 53% 21.4M 23s
285350K .......... .......... .......... .......... .......... 53% 14.9M 23s
285400K .......... .......... .......... .......... .......... 53% 14.2M 23s
285450K .......... .......... .......... .......... .......... 53% 14.8M 23s
285500K .......... .......... .......... .......... .......... 53% 18.0M 23s
285550K .......... .......... .......... .......... .......... 53% 19.9M 23s
285600K .......... .......... .......... .......... .......... 53% 16.2M 23s
285650K .......... .......... .......... .......... .......... 53% 19.5M 23s
285700K .......... .......... .......... .......... .......... 53% 14.0M 23s
285750K .......... .......... .......... .......... .......... 53% 18.6M 23s
285800K .......... .......... .......... .......... .......... 53% 22.2M 23s
285850K .......... .......... .......... .......... .......... 53% 14.3M 23s
285900K .......... .......... .......... .......... .......... 53% 24.3M 23s
285950K .......... .......... .......... .......... .......... 53% 17.0M 23s
286000K .......... .......... .......... .......... .......... 53% 46.4M 23s
286050K .......... .......... .......... .......... .......... 53% 95.2M 23s
286100K .......... .......... .......... .......... .......... 53% 35.3M 23s
286150K .......... .......... .......... .......... .......... 53% 47.6M 23s
286200K .......... .......... .......... .......... .......... 53% 24.1M 23s
286250K .......... .......... .......... .......... .......... 53%  132M 23s
286300K .......... .......... .......... .......... .......... 53% 20.3M 23s
286350K .......... .......... .......... .......... .......... 53% 55.5M 23s
286400K .......... .......... .......... .......... .......... 53% 26.0M 23s
286450K .......... .......... .......... .......... .......... 53% 26.3M 23s
286500K .......... .......... .......... .......... .......... 53% 20.2M 23s
286550K .......... .......... .......... .......... .......... 53% 44.3M 23s
286600K .......... .......... .......... .......... .......... 53% 18.1M 23s
286650K .......... .......... .......... .......... .......... 53% 30.2M 23s
286700K .......... .......... .......... .......... .......... 53% 20.4M 23s
286750K .......... .......... .......... .......... .......... 53% 34.5M 23s
286800K .......... .......... .......... .......... .......... 53% 27.4M 23s
286850K .......... .......... .......... .......... .......... 53% 23.9M 23s
286900K .......... .......... .......... .......... .......... 53% 26.0M 23s
286950K .......... .......... .......... .......... .......... 53% 23.9M 23s
287000K .......... .......... .......... .......... .......... 53% 23.7M 23s
287050K .......... .......... .......... .......... .......... 53% 21.7M 23s
287100K .......... .......... .......... .......... .......... 53% 21.6M 23s
287150K .......... .......... .......... .......... .......... 53% 25.7M 23s
287200K .......... .......... .......... .......... .......... 53% 23.3M 23s
287250K .......... .......... .......... .......... .......... 53% 22.5M 23s
287300K .......... .......... .......... .......... .......... 53% 31.0M 23s
287350K .......... .......... .......... .......... .......... 53% 38.1M 23s
287400K .......... .......... .......... .......... .......... 53% 11.5M 23s
287450K .......... .......... .......... .......... .......... 53%  116M 23s
287500K .......... .......... .......... .......... .......... 53% 29.1M 23s
287550K .......... .......... .......... .......... .......... 53%  141M 23s
287600K .......... .......... .......... .......... .......... 53% 18.1M 23s
287650K .......... .......... .......... .......... .......... 53%  120M 23s
287700K .......... .......... .......... .......... .......... 53% 22.9M 23s
287750K .......... .......... .......... .......... .......... 53% 29.0M 23s
287800K .......... .......... .......... .......... .......... 53% 28.9M 23s
287850K .......... .......... .......... .......... .......... 53% 20.1M 23s
287900K .......... .......... .......... .......... .......... 53% 23.1M 23s
287950K .......... .......... .......... .......... .......... 53% 20.3M 23s
288000K .......... .......... .......... .......... .......... 53% 23.8M 23s
288050K .......... .......... .......... .......... .......... 53% 21.3M 23s
288100K .......... .......... .......... .......... .......... 53% 24.9M 23s
288150K .......... .......... .......... .......... .......... 53% 23.9M 23s
288200K .......... .......... .......... .......... .......... 53% 18.1M 23s
288250K .......... .......... .......... .......... .......... 53% 23.1M 23s
288300K .......... .......... .......... .......... .......... 53% 24.1M 23s
288350K .......... .......... .......... .......... .......... 53% 20.0M 23s
288400K .......... .......... .......... .......... .......... 53% 23.6M 23s
288450K .......... .......... .......... .......... .......... 53% 20.1M 23s
288500K .......... .......... .......... .......... .......... 53% 23.0M 23s
288550K .......... .......... .......... .......... .......... 53% 47.8M 23s
288600K .......... .......... .......... .......... .......... 53% 11.5M 23s
288650K .......... .......... .......... .......... .......... 53%  121M 23s
288700K .......... .......... .......... .......... .......... 53% 16.9M 23s
288750K .......... .......... .......... .......... .......... 53% 58.5M 23s
288800K .......... .......... .......... .......... .......... 53% 20.3M 23s
288850K .......... .......... .......... .......... .......... 53% 14.1M 23s
288900K .......... .......... .......... .......... .......... 53% 19.9M 23s
288950K .......... .......... .......... .......... .......... 53% 15.2M 23s
289000K .......... .......... .......... .......... .......... 53% 16.1M 23s
289050K .......... .......... .......... .......... .......... 53% 18.1M 23s
289100K .......... .......... .......... .......... .......... 53% 14.3M 23s
289150K .......... .......... .......... .......... .......... 53% 17.0M 23s
289200K .......... .......... .......... .......... .......... 53% 13.9M 23s
289250K .......... .......... .......... .......... .......... 53% 17.6M 23s
289300K .......... .......... .......... .......... .......... 53% 18.1M 23s
289350K .......... .......... .......... .......... .......... 53% 14.7M 23s
289400K .......... .......... .......... .......... .......... 53% 17.7M 23s
289450K .......... .......... .......... .......... .......... 53% 13.5M 23s
289500K .......... .......... .......... .......... .......... 53% 27.5M 23s
289550K .......... .......... .......... .......... .......... 53% 17.0M 23s
289600K .......... .......... .......... .......... .......... 53% 37.0M 23s
289650K .......... .......... .......... .......... .......... 53% 18.1M 23s
289700K .......... .......... .......... .......... .......... 53% 15.3M 23s
289750K .......... .......... .......... .......... .......... 53% 12.8M 23s
289800K .......... .......... .......... .......... .......... 53% 14.2M 23s
289850K .......... .......... .......... .......... .......... 53% 12.3M 23s
289900K .......... .......... .......... .......... .......... 53% 16.5M 23s
289950K .......... .......... .......... .......... .......... 53% 7.66M 23s
290000K .......... .......... .......... .......... .......... 53% 34.9M 23s
290050K .......... .......... .......... .......... .......... 53% 15.1M 23s
290100K .......... .......... .......... .......... .......... 53% 11.1M 23s
290150K .......... .......... .......... .......... .......... 54% 12.7M 23s
290200K .......... .......... .......... .......... .......... 54% 15.7M 23s
290250K .......... .......... .......... .......... .......... 54% 24.4M 23s
290300K .......... .......... .......... .......... .......... 54% 22.1M 23s
290350K .......... .......... .......... .......... .......... 54% 14.0M 23s
290400K .......... .......... .......... .......... .......... 54% 48.9M 23s
290450K .......... .......... .......... .......... .......... 54% 18.9M 23s
290500K .......... .......... .......... .......... .......... 54% 19.8M 23s
290550K .......... .......... .......... .......... .......... 54% 25.6M 23s
290600K .......... .......... .......... .......... .......... 54% 28.2M 23s
290650K .......... .......... .......... .......... .......... 54% 20.9M 23s
290700K .......... .......... .......... .......... .......... 54% 19.7M 23s
290750K .......... .......... .......... .......... .......... 54% 23.8M 23s
290800K .......... .......... .......... .......... .......... 54% 25.4M 23s
290850K .......... .......... .......... .......... .......... 54% 25.8M 23s
290900K .......... .......... .......... .......... .......... 54% 22.3M 23s
290950K .......... .......... .......... .......... .......... 54% 20.2M 23s
291000K .......... .......... .......... .......... .......... 54% 23.9M 23s
291050K .......... .......... .......... .......... .......... 54% 26.2M 23s
291100K .......... .......... .......... .......... .......... 54% 24.2M 23s
291150K .......... .......... .......... .......... .......... 54% 18.6M 23s
291200K .......... .......... .......... .......... .......... 54% 24.3M 23s
291250K .......... .......... .......... .......... .......... 54% 21.4M 23s
291300K .......... .......... .......... .......... .......... 54% 8.35M 23s
291350K .......... .......... .......... .......... .......... 54% 23.1M 23s
291400K .......... .......... .......... .......... .......... 54% 17.6M 23s
291450K .......... .......... .......... .......... .......... 54% 15.2M 23s
291500K .......... .......... .......... .......... .......... 54% 26.1M 23s
291550K .......... .......... .......... .......... .......... 54% 18.9M 23s
291600K .......... .......... .......... .......... .......... 54% 14.4M 23s
291650K .......... .......... .......... .......... .......... 54% 20.0M 23s
291700K .......... .......... .......... .......... .......... 54% 16.8M 22s
291750K .......... .......... .......... .......... .......... 54% 23.6M 22s
291800K .......... .......... .......... .......... .......... 54% 16.6M 22s
291850K .......... .......... .......... .......... .......... 54% 17.8M 22s
291900K .......... .......... .......... .......... .......... 54% 23.5M 22s
291950K .......... .......... .......... .......... .......... 54% 19.1M 22s
292000K .......... .......... .......... .......... .......... 54% 19.4M 22s
292050K .......... .......... .......... .......... .......... 54% 11.3M 22s
292100K .......... .......... .......... .......... .......... 54% 47.9M 22s
292150K .......... .......... .......... .......... .......... 54% 24.3M 22s
292200K .......... .......... .......... .......... .......... 54% 16.8M 22s
292250K .......... .......... .......... .......... .......... 54% 6.51M 22s
292300K .......... .......... .......... .......... .......... 54% 79.7M 22s
292350K .......... .......... .......... .......... .......... 54%  101M 22s
292400K .......... .......... .......... .......... .......... 54% 13.0M 22s
292450K .......... .......... .......... .......... .......... 54% 12.0M 22s
292500K .......... .......... .......... .......... .......... 54% 15.4M 22s
292550K .......... .......... .......... .......... .......... 54% 12.2M 22s
292600K .......... .......... .......... .......... .......... 54% 15.7M 22s
292650K .......... .......... .......... .......... .......... 54% 15.5M 22s
292700K .......... .......... .......... .......... .......... 54% 12.3M 22s
292750K .......... .......... .......... .......... .......... 54% 17.3M 22s
292800K .......... .......... .......... .......... .......... 54% 15.0M 22s
292850K .......... .......... .......... .......... .......... 54% 15.0M 22s
292900K .......... .......... .......... .......... .......... 54% 13.8M 22s
292950K .......... .......... .......... .......... .......... 54% 13.1M 22s
293000K .......... .......... .......... .......... .......... 54% 19.2M 22s
293050K .......... .......... .......... .......... .......... 54% 12.5M 22s
293100K .......... .......... .......... .......... .......... 54% 34.1M 22s
293150K .......... .......... .......... .......... .......... 54% 25.9M 22s
293200K .......... .......... .......... .......... .......... 54% 13.9M 22s
293250K .......... .......... .......... .......... .......... 54% 23.2M 22s
293300K .......... .......... .......... .......... .......... 54% 18.1M 22s
293350K .......... .......... .......... .......... .......... 54% 18.4M 22s
293400K .......... .......... .......... .......... .......... 54% 16.8M 22s
293450K .......... .......... .......... .......... .......... 54% 18.5M 22s
293500K .......... .......... .......... .......... .......... 54% 17.8M 22s
293550K .......... .......... .......... .......... .......... 54% 20.3M 22s
293600K .......... .......... .......... .......... .......... 54% 14.0M 22s
293650K .......... .......... .......... .......... .......... 54% 24.0M 22s
293700K .......... .......... .......... .......... .......... 54% 14.4M 22s
293750K .......... .......... .......... .......... .......... 54% 20.1M 22s
293800K .......... .......... .......... .......... .......... 54% 15.1M 22s
293850K .......... .......... .......... .......... .......... 54% 10.2M 22s
293900K .......... .......... .......... .......... .......... 54% 18.0M 22s
293950K .......... .......... .......... .......... .......... 54% 12.8M 22s
294000K .......... .......... .......... .......... .......... 54% 12.3M 22s
294050K .......... .......... .......... .......... .......... 54% 16.8M 22s
294100K .......... .......... .......... .......... .......... 54% 10.5M 22s
294150K .......... .......... .......... .......... .......... 54% 12.6M 22s
294200K .......... .......... .......... .......... .......... 54% 11.2M 22s
294250K .......... .......... .......... .......... .......... 54% 14.3M 22s
294300K .......... .......... .......... .......... .......... 54% 9.01M 22s
294350K .......... .......... .......... .......... .......... 54% 11.6M 22s
294400K .......... .......... .......... .......... .......... 54% 6.61M 22s
294450K .......... .......... .......... .......... .......... 54% 14.3M 22s
294500K .......... .......... .......... .......... .......... 54% 12.2M 22s
294550K .......... .......... .......... .......... .......... 54% 12.3M 22s
294600K .......... .......... .......... .......... .......... 54% 14.1M 22s
294650K .......... .......... .......... .......... .......... 54% 15.8M 22s
294700K .......... .......... .......... .......... .......... 54% 13.9M 22s
294750K .......... .......... .......... .......... .......... 54% 15.0M 22s
294800K .......... .......... .......... .......... .......... 54% 14.4M 22s
294850K .......... .......... .......... .......... .......... 54% 12.4M 22s
294900K .......... .......... .......... .......... .......... 54% 16.1M 22s
294950K .......... .......... .......... .......... .......... 54% 14.3M 22s
295000K .......... .......... .......... .......... .......... 54% 17.3M 22s
295050K .......... .......... .......... .......... .......... 54% 9.40M 22s
295100K .......... .......... .......... .......... .......... 54% 21.8M 22s
295150K .......... .......... .......... .......... .......... 54% 10.1M 22s
295200K .......... .......... .......... .......... .......... 54% 11.4M 22s
295250K .......... .......... .......... .......... .......... 54% 13.9M 22s
295300K .......... .......... .......... .......... .......... 54% 13.0M 22s
295350K .......... .......... .......... .......... .......... 54% 11.3M 22s
295400K .......... .......... .......... .......... .......... 54% 15.1M 22s
295450K .......... .......... .......... .......... .......... 54% 14.0M 22s
295500K .......... .......... .......... .......... .......... 54% 13.4M 22s
295550K .......... .......... .......... .......... .......... 55% 14.5M 22s
295600K .......... .......... .......... .......... .......... 55% 13.3M 22s
295650K .......... .......... .......... .......... .......... 55% 17.8M 22s
295700K .......... .......... .......... .......... .......... 55% 9.48M 22s
295750K .......... .......... .......... .......... .......... 55% 15.4M 22s
295800K .......... .......... .......... .......... .......... 55% 32.0M 22s
295850K .......... .......... .......... .......... .......... 55% 16.4M 22s
295900K .......... .......... .......... .......... .......... 55% 22.7M 22s
295950K .......... .......... .......... .......... .......... 55% 17.0M 22s
296000K .......... .......... .......... .......... .......... 55% 23.5M 22s
296050K .......... .......... .......... .......... .......... 55% 20.8M 22s
296100K .......... .......... .......... .......... .......... 55% 18.6M 22s
296150K .......... .......... .......... .......... .......... 55% 22.7M 22s
296200K .......... .......... .......... .......... .......... 55% 24.4M 22s
296250K .......... .......... .......... .......... .......... 55% 26.7M 22s
296300K .......... .......... .......... .......... .......... 55% 22.7M 22s
296350K .......... .......... .......... .......... .......... 55% 17.3M 22s
296400K .......... .......... .......... .......... .......... 55% 18.9M 22s
296450K .......... .......... .......... .......... .......... 55% 19.5M 22s
296500K .......... .......... .......... .......... .......... 55% 20.3M 22s
296550K .......... .......... .......... .......... .......... 55% 22.1M 22s
296600K .......... .......... .......... .......... .......... 55% 37.9M 22s
296650K .......... .......... .......... .......... .......... 55%  119M 22s
296700K .......... .......... .......... .......... .......... 55% 45.8M 22s
296750K .......... .......... .......... .......... .......... 55% 50.9M 22s
296800K .......... .......... .......... .......... .......... 55% 17.1M 22s
296850K .......... .......... .......... .......... .......... 55% 77.4M 22s
296900K .......... .......... .......... .......... .......... 55% 34.2M 22s
296950K .......... .......... .......... .......... .......... 55% 20.9M 22s
297000K .......... .......... .......... .......... .......... 55% 32.7M 22s
297050K .......... .......... .......... .......... .......... 55% 42.7M 22s
297100K .......... .......... .......... .......... .......... 55% 21.6M 22s
297150K .......... .......... .......... .......... .......... 55% 18.3M 22s
297200K .......... .......... .......... .......... .......... 55% 19.6M 22s
297250K .......... .......... .......... .......... .......... 55% 19.5M 22s
297300K .......... .......... .......... .......... .......... 55% 16.7M 22s
297350K .......... .......... .......... .......... .......... 55% 20.0M 22s
297400K .......... .......... .......... .......... .......... 55% 17.0M 22s
297450K .......... .......... .......... .......... .......... 55% 18.5M 22s
297500K .......... .......... .......... .......... .......... 55% 17.5M 22s
297550K .......... .......... .......... .......... .......... 55% 24.2M 22s
297600K .......... .......... .......... .......... .......... 55% 15.3M 22s
297650K .......... .......... .......... .......... .......... 55% 23.0M 22s
297700K .......... .......... .......... .......... .......... 55% 16.0M 22s
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297850K .......... .......... .......... .......... .......... 55% 19.9M 22s
297900K .......... .......... .......... .......... .......... 55% 18.8M 22s
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298000K .......... .......... .......... .......... .......... 55% 27.7M 22s
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298100K .......... .......... .......... .......... .......... 55% 18.0M 22s
298150K .......... .......... .......... .......... .......... 55% 18.7M 22s
298200K .......... .......... .......... .......... .......... 55% 15.2M 22s
298250K .......... .......... .......... .......... .......... 55% 17.3M 22s
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298350K .......... .......... .......... .......... .......... 55% 17.2M 22s
298400K .......... .......... .......... .......... .......... 55% 16.0M 22s
298450K .......... .......... .......... .......... .......... 55% 16.7M 22s
298500K .......... .......... .......... .......... .......... 55% 19.7M 22s
298550K .......... .......... .......... .......... .......... 55% 18.5M 22s
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298650K .......... .......... .......... .......... .......... 55% 13.5M 22s
298700K .......... .......... .......... .......... .......... 55% 7.28M 22s
298750K .......... .......... .......... .......... .......... 55% 15.6M 22s
298800K .......... .......... .......... .......... .......... 55% 22.2M 22s
298850K .......... .......... .......... .......... .......... 55% 20.7M 22s
298900K .......... .......... .......... .......... .......... 55% 13.9M 22s
298950K .......... .......... .......... .......... .......... 55% 16.9M 22s
299000K .......... .......... .......... .......... .......... 55% 21.2M 22s
299050K .......... .......... .......... .......... .......... 55% 16.1M 22s
299100K .......... .......... .......... .......... .......... 55% 15.9M 22s
299150K .......... .......... .......... .......... .......... 55% 12.5M 22s
299200K .......... .......... .......... .......... .......... 55% 10.6M 22s
299250K .......... .......... .......... .......... .......... 55% 15.2M 22s
299300K .......... .......... .......... .......... .......... 55% 12.5M 22s
299350K .......... .......... .......... .......... .......... 55% 10.4M 22s
299400K .......... .......... .......... .......... .......... 55% 10.0M 22s
299450K .......... .......... .......... .......... .......... 55% 6.35M 22s
299500K .......... .......... .......... .......... .......... 55% 14.9M 22s
299550K .......... .......... .......... .......... .......... 55% 17.3M 22s
299600K .......... .......... .......... .......... .......... 55% 12.6M 22s
299650K .......... .......... .......... .......... .......... 55% 14.8M 22s
299700K .......... .......... .......... .......... .......... 55% 14.1M 22s
299750K .......... .......... .......... .......... .......... 55% 16.7M 22s
299800K .......... .......... .......... .......... .......... 55% 14.2M 22s
299850K .......... .......... .......... .......... .......... 55% 13.3M 22s
299900K .......... .......... .......... .......... .......... 55% 16.8M 22s
299950K .......... .......... .......... .......... .......... 55% 9.87M 22s
300000K .......... .......... .......... .......... .......... 55% 12.7M 22s
300050K .......... .......... .......... .......... .......... 55% 14.4M 22s
300100K .......... .......... .......... .......... .......... 55% 20.2M 22s
300150K .......... .......... .......... .......... .......... 55% 16.3M 22s
300200K .......... .......... .......... .......... .......... 55% 25.7M 22s
300250K .......... .......... .......... .......... .......... 55% 25.4M 22s
300300K .......... .......... .......... .......... .......... 55% 25.4M 22s
300350K .......... .......... .......... .......... .......... 55% 23.0M 21s
300400K .......... .......... .......... .......... .......... 55% 22.8M 21s
300450K .......... .......... .......... .......... .......... 55% 15.6M 21s
300500K .......... .......... .......... .......... .......... 55% 22.9M 21s
300550K .......... .......... .......... .......... .......... 55% 45.5M 21s
300600K .......... .......... .......... .......... .......... 55% 22.6M 21s
300650K .......... .......... .......... .......... .......... 55% 20.7M 21s
300700K .......... .......... .......... .......... .......... 55% 20.9M 21s
300750K .......... .......... .......... .......... .......... 55% 24.6M 21s
300800K .......... .......... .......... .......... .......... 55% 23.6M 21s
300850K .......... .......... .......... .......... .......... 55% 20.8M 21s
300900K .......... .......... .......... .......... .......... 56% 28.9M 21s
300950K .......... .......... .......... .......... .......... 56% 18.0M 21s
301000K .......... .......... .......... .......... .......... 56% 24.1M 21s
301050K .......... .......... .......... .......... .......... 56% 14.4M 21s
301100K .......... .......... .......... .......... .......... 56% 41.7M 21s
301150K .......... .......... .......... .......... .......... 56% 20.6M 21s
301200K .......... .......... .......... .......... .......... 56%  108M 21s
301250K .......... .......... .......... .......... .......... 56% 20.1M 21s
301300K .......... .......... .......... .......... .......... 56% 40.5M 21s
301350K .......... .......... .......... .......... .......... 56% 22.6M 21s
301400K .......... .......... .......... .......... .......... 56% 24.3M 21s
301450K .......... .......... .......... .......... .......... 56% 26.2M 21s
301500K .......... .......... .......... .......... .......... 56% 30.4M 21s
301550K .......... .......... .......... .......... .......... 56% 27.5M 21s
301600K .......... .......... .......... .......... .......... 56% 20.7M 21s
301650K .......... .......... .......... .......... .......... 56% 27.3M 21s
301700K .......... .......... .......... .......... .......... 56% 20.5M 21s
301750K .......... .......... .......... .......... .......... 56% 22.9M 21s
301800K .......... .......... .......... .......... .......... 56% 39.6M 21s
301850K .......... .......... .......... .......... .......... 56% 17.0M 21s
301900K .......... .......... .......... .......... .......... 56% 27.9M 21s
301950K .......... .......... .......... .......... .......... 56% 22.8M 21s
302000K .......... .......... .......... .......... .......... 56% 19.8M 21s
302050K .......... .......... .......... .......... .......... 56% 15.3M 21s
302100K .......... .......... .......... .......... .......... 56% 13.0M 21s
302150K .......... .......... .......... .......... .......... 56% 16.2M 21s
302200K .......... .......... .......... .......... .......... 56% 8.79M 21s
302250K .......... .......... .......... .......... .......... 56% 16.0M 21s
302300K .......... .......... .......... .......... .......... 56% 13.2M 21s
302350K .......... .......... .......... .......... .......... 56% 11.8M 21s
302400K .......... .......... .......... .......... .......... 56% 17.2M 21s
302450K .......... .......... .......... .......... .......... 56% 13.4M 21s
302500K .......... .......... .......... .......... .......... 56% 13.8M 21s
302550K .......... .......... .......... .......... .......... 56% 16.4M 21s
302600K .......... .......... .......... .......... .......... 56% 13.2M 21s
302650K .......... .......... .......... .......... .......... 56% 16.6M 21s
302700K .......... .......... .......... .......... .......... 56% 19.9M 21s
302750K .......... .......... .......... .......... .......... 56% 36.7M 21s
302800K .......... .......... .......... .......... .......... 56% 17.0M 21s
302850K .......... .......... .......... .......... .......... 56% 81.4M 21s
302900K .......... .......... .......... .......... .......... 56% 29.0M 21s
302950K .......... .......... .......... .......... .......... 56% 11.4M 21s
303000K .......... .......... .......... .......... .......... 56% 18.3M 21s
303050K .......... .......... .......... .......... .......... 56% 17.2M 21s
303100K .......... .......... .......... .......... .......... 56% 18.8M 21s
303150K .......... .......... .......... .......... .......... 56% 20.4M 21s
303200K .......... .......... .......... .......... .......... 56% 16.4M 21s
303250K .......... .......... .......... .......... .......... 56% 18.8M 21s
303300K .......... .......... .......... .......... .......... 56% 24.0M 21s
303350K .......... .......... .......... .......... .......... 56% 18.4M 21s
303400K .......... .......... .......... .......... .......... 56% 20.5M 21s
303450K .......... .......... .......... .......... .......... 56% 22.2M 21s
303500K .......... .......... .......... .......... .......... 56% 14.8M 21s
303550K .......... .......... .......... .......... .......... 56% 26.7M 21s
303600K .......... .......... .......... .......... .......... 56% 22.4M 21s
303650K .......... .......... .......... .......... .......... 56% 21.0M 21s
303700K .......... .......... .......... .......... .......... 56% 21.7M 21s
303750K .......... .......... .......... .......... .......... 56% 21.7M 21s
303800K .......... .......... .......... .......... .......... 56% 21.1M 21s
303850K .......... .......... .......... .......... .......... 56% 18.7M 21s
303900K .......... .......... .......... .......... .......... 56% 11.3M 21s
303950K .......... .......... .......... .......... .......... 56%  101M 21s
304000K .......... .......... .......... .......... .......... 56% 16.2M 21s
304050K .......... .......... .......... .......... .......... 56% 20.7M 21s
304100K .......... .......... .......... .......... .......... 56% 30.0M 21s
304150K .......... .......... .......... .......... .......... 56% 29.4M 21s
304200K .......... .......... .......... .......... .......... 56% 17.8M 21s
304250K .......... .......... .......... .......... .......... 56% 33.4M 21s
304300K .......... .......... .......... .......... .......... 56% 19.1M 21s
304350K .......... .......... .......... .......... .......... 56% 20.7M 21s
304400K .......... .......... .......... .......... .......... 56% 21.9M 21s
304450K .......... .......... .......... .......... .......... 56% 22.0M 21s
304500K .......... .......... .......... .......... .......... 56% 29.8M 21s
304550K .......... .......... .......... .......... .......... 56% 11.5M 21s
304600K .......... .......... .......... .......... .......... 56% 18.8M 21s
304650K .......... .......... .......... .......... .......... 56% 19.1M 21s
304700K .......... .......... .......... .......... .......... 56% 21.7M 21s
304750K .......... .......... .......... .......... .......... 56% 18.2M 21s
304800K .......... .......... .......... .......... .......... 56% 24.9M 21s
304850K .......... .......... .......... .......... .......... 56% 13.8M 21s
304900K .......... .......... .......... .......... .......... 56% 25.6M 21s
304950K .......... .......... .......... .......... .......... 56% 15.2M 21s
305000K .......... .......... .......... .......... .......... 56% 18.2M 21s
305050K .......... .......... .......... .......... .......... 56% 18.3M 21s
305100K .......... .......... .......... .......... .......... 56% 15.5M 21s
305150K .......... .......... .......... .......... .......... 56% 23.2M 21s
305200K .......... .......... .......... .......... .......... 56% 12.6M 21s
305250K .......... .......... .......... .......... .......... 56% 10.2M 21s
305300K .......... .......... .......... .......... .......... 56% 10.6M 21s
305350K .......... .......... .......... .......... .......... 56% 8.52M 21s
305400K .......... .......... .......... .......... .......... 56% 14.4M 21s
305450K .......... .......... .......... .......... .......... 56% 14.7M 21s
305500K .......... .......... .......... .......... .......... 56% 16.1M 21s
305550K .......... .......... .......... .......... .......... 56% 19.9M 21s
305600K .......... .......... .......... .......... .......... 56% 12.9M 21s
305650K .......... .......... .......... .......... .......... 56% 16.2M 21s
305700K .......... .......... .......... .......... .......... 56% 15.0M 21s
305750K .......... .......... .......... .......... .......... 56% 15.9M 21s
305800K .......... .......... .......... .......... .......... 56% 18.7M 21s
305850K .......... .......... .......... .......... .......... 56% 14.3M 21s
305900K .......... .......... .......... .......... .......... 56% 37.2M 21s
305950K .......... .......... .......... .......... .......... 56% 27.7M 21s
306000K .......... .......... .......... .......... .......... 56% 34.3M 21s
306050K .......... .......... .......... .......... .......... 56% 17.8M 21s
306100K .......... .......... .......... .......... .......... 56%  103M 21s
306150K .......... .......... .......... .......... .......... 56% 26.8M 21s
306200K .......... .......... .......... .......... .......... 56% 24.2M 21s
306250K .......... .......... .......... .......... .......... 56% 38.8M 21s
306300K .......... .......... .......... .......... .......... 57% 21.9M 21s
306350K .......... .......... .......... .......... .......... 57% 26.1M 21s
306400K .......... .......... .......... .......... .......... 57% 23.1M 21s
306450K .......... .......... .......... .......... .......... 57% 36.4M 21s
306500K .......... .......... .......... .......... .......... 57% 22.1M 21s
306550K .......... .......... .......... .......... .......... 57% 26.7M 21s
306600K .......... .......... .......... .......... .......... 57% 20.8M 21s
306650K .......... .......... .......... .......... .......... 57% 32.2M 21s
306700K .......... .......... .......... .......... .......... 57% 20.8M 21s
306750K .......... .......... .......... .......... .......... 57% 24.8M 21s
306800K .......... .......... .......... .......... .......... 57% 38.1M 21s
306850K .......... .......... .......... .......... .......... 57% 21.1M 21s
306900K .......... .......... .......... .......... .......... 57% 19.9M 21s
306950K .......... .......... .......... .......... .......... 57% 22.5M 21s
307000K .......... .......... .......... .......... .......... 57% 25.3M 21s
307050K .......... .......... .......... .......... .......... 57% 40.4M 21s
307100K .......... .......... .......... .......... .......... 57% 21.8M 21s
307150K .......... .......... .......... .......... .......... 57% 10.1M 21s
307200K .......... .......... .......... .......... .......... 57% 22.0M 21s
307250K .......... .......... .......... .......... .......... 57%  128M 21s
307300K .......... .......... .......... .......... .......... 57%  112M 21s
307350K .......... .......... .......... .......... .......... 57% 14.0M 21s
307400K .......... .......... .......... .......... .......... 57%  131M 21s
307450K .......... .......... .......... .......... .......... 57% 32.4M 21s
307500K .......... .......... .......... .......... .......... 57% 23.9M 21s
307550K .......... .......... .......... .......... .......... 57% 44.5M 21s
307600K .......... .......... .......... .......... .......... 57% 24.8M 21s
307650K .......... .......... .......... .......... .......... 57% 30.0M 21s
307700K .......... .......... .......... .......... .......... 57% 22.6M 21s
307750K .......... .......... .......... .......... .......... 57% 37.5M 21s
307800K .......... .......... .......... .......... .......... 57% 24.3M 21s
307850K .......... .......... .......... .......... .......... 57% 26.9M 21s
307900K .......... .......... .......... .......... .......... 57% 24.2M 21s
307950K .......... .......... .......... .......... .......... 57% 29.4M 21s
308000K .......... .......... .......... .......... .......... 57% 30.3M 21s
308050K .......... .......... .......... .......... .......... 57% 39.7M 21s
308100K .......... .......... .......... .......... .......... 57% 21.5M 21s
308150K .......... .......... .......... .......... .......... 57% 46.6M 21s
308200K .......... .......... .......... .......... .......... 57% 26.8M 21s
308250K .......... .......... .......... .......... .......... 57% 28.2M 21s
308300K .......... .......... .......... .......... .......... 57% 26.9M 21s
308350K .......... .......... .......... .......... .......... 57% 24.5M 21s
308400K .......... .......... .......... .......... .......... 57% 40.0M 21s
308450K .......... .......... .......... .......... .......... 57% 32.9M 20s
308500K .......... .......... .......... .......... .......... 57% 14.9M 20s
308550K .......... .......... .......... .......... .......... 57%  121M 20s
308600K .......... .......... .......... .......... .......... 57% 21.2M 20s
308650K .......... .......... .......... .......... .......... 57% 95.6M 20s
308700K .......... .......... .......... .......... .......... 57% 20.3M 20s
308750K .......... .......... .......... .......... .......... 57% 25.0M 20s
308800K .......... .......... .......... .......... .......... 57% 22.4M 20s
308850K .......... .......... .......... .......... .......... 57% 14.5M 20s
308900K .......... .......... .......... .......... .......... 57% 17.1M 20s
308950K .......... .......... .......... .......... .......... 57% 14.7M 20s
309000K .......... .......... .......... .......... .......... 57% 19.9M 20s
309050K .......... .......... .......... .......... .......... 57% 16.6M 20s
309100K .......... .......... .......... .......... .......... 57% 20.9M 20s
309150K .......... .......... .......... .......... .......... 57% 17.7M 20s
309200K .......... .......... .......... .......... .......... 57% 17.2M 20s
309250K .......... .......... .......... .......... .......... 57% 23.1M 20s
309300K .......... .......... .......... .......... .......... 57% 22.3M 20s
309350K .......... .......... .......... .......... .......... 57% 13.2M 20s
309400K .......... .......... .......... .......... .......... 57% 13.1M 20s
309450K .......... .......... .......... .......... .......... 57% 12.2M 20s
309500K .......... .......... .......... .......... .......... 57% 16.3M 20s
309550K .......... .......... .......... .......... .......... 57% 12.5M 20s
309600K .......... .......... .......... .......... .......... 57% 29.0M 20s
309650K .......... .......... .......... .......... .......... 57% 15.6M 20s
309700K .......... .......... .......... .......... .......... 57% 15.2M 20s
309750K .......... .......... .......... .......... .......... 57% 15.3M 20s
309800K .......... .......... .......... .......... .......... 57% 12.9M 20s
309850K .......... .......... .......... .......... .......... 57% 14.4M 20s
309900K .......... .......... .......... .......... .......... 57% 13.1M 20s
309950K .......... .......... .......... .......... .......... 57% 12.5M 20s
310000K .......... .......... .......... .......... .......... 57% 16.0M 20s
310050K .......... .......... .......... .......... .......... 57% 15.3M 20s
310100K .......... .......... .......... .......... .......... 57% 12.5M 20s
310150K .......... .......... .......... .......... .......... 57% 17.7M 20s
310200K .......... .......... .......... .......... .......... 57% 13.2M 20s
310250K .......... .......... .......... .......... .......... 57% 12.6M 20s
310300K .......... .......... .......... .......... .......... 57% 13.8M 20s
310350K .......... .......... .......... .......... .......... 57% 18.8M 20s
310400K .......... .......... .......... .......... .......... 57% 22.4M 20s
310450K .......... .......... .......... .......... .......... 57% 55.9M 20s
310500K .......... .......... .......... .......... .......... 57% 13.0M 20s
310550K .......... .......... .......... .......... .......... 57% 18.6M 20s
310600K .......... .......... .......... .......... .......... 57%  101M 20s
310650K .......... .......... .......... .......... .......... 57% 27.4M 20s
310700K .......... .......... .......... .......... .......... 57% 31.0M 20s
310750K .......... .......... .......... .......... .......... 57% 24.8M 20s
310800K .......... .......... .......... .......... .......... 57% 16.0M 20s
310850K .......... .......... .......... .......... .......... 57% 19.5M 20s
310900K .......... .......... .......... .......... .......... 57% 25.0M 20s
310950K .......... .......... .......... .......... .......... 57% 12.5M 20s
311000K .......... .......... .......... .......... .......... 57% 45.4M 20s
311050K .......... .......... .......... .......... .......... 57% 27.0M 20s
311100K .......... .......... .......... .......... .......... 57% 23.9M 20s
311150K .......... .......... .......... .......... .......... 57% 23.8M 20s
311200K .......... .......... .......... .......... .......... 57% 19.0M 20s
311250K .......... .......... .......... .......... .......... 57% 22.4M 20s
311300K .......... .......... .......... .......... .......... 57% 21.4M 20s
311350K .......... .......... .......... .......... .......... 57% 20.1M 20s
311400K .......... .......... .......... .......... .......... 57% 23.1M 20s
311450K .......... .......... .......... .......... .......... 57% 20.4M 20s
311500K .......... .......... .......... .......... .......... 57% 30.4M 20s
311550K .......... .......... .......... .......... .......... 57% 23.1M 20s
311600K .......... .......... .......... .......... .......... 57% 16.6M 20s
311650K .......... .......... .......... .......... .......... 58% 14.7M 20s
311700K .......... .......... .......... .......... .......... 58% 91.1M 20s
311750K .......... .......... .......... .......... .......... 58% 23.0M 20s
311800K .......... .......... .......... .......... .......... 58% 40.9M 20s
311850K .......... .......... .......... .......... .......... 58% 21.2M 20s
311900K .......... .......... .......... .......... .......... 58% 36.3M 20s
311950K .......... .......... .......... .......... .......... 58% 23.7M 20s
312000K .......... .......... .......... .......... .......... 58% 25.8M 20s
312050K .......... .......... .......... .......... .......... 58% 21.4M 20s
312100K .......... .......... .......... .......... .......... 58% 22.9M 20s
312150K .......... .......... .......... .......... .......... 58% 19.6M 20s
312200K .......... .......... .......... .......... .......... 58% 19.9M 20s
312250K .......... .......... .......... .......... .......... 58% 16.4M 20s
312300K .......... .......... .......... .......... .......... 58% 22.1M 20s
312350K .......... .......... .......... .......... .......... 58% 16.9M 20s
312400K .......... .......... .......... .......... .......... 58% 26.2M 20s
312450K .......... .......... .......... .......... .......... 58% 16.5M 20s
312500K .......... .......... .......... .......... .......... 58% 18.4M 20s
312550K .......... .......... .......... .......... .......... 58% 20.8M 20s
312600K .......... .......... .......... .......... .......... 58% 15.2M 20s
312650K .......... .......... .......... .......... .......... 58% 10.2M 20s
312700K .......... .......... .......... .......... .......... 58% 8.68M 20s
312750K .......... .......... .......... .......... .......... 58% 13.0M 20s
312800K .......... .......... .......... .......... .......... 58% 16.3M 20s
312850K .......... .......... .......... .......... .......... 58% 12.8M 20s
312900K .......... .......... .......... .......... .......... 58% 13.0M 20s
312950K .......... .......... .......... .......... .......... 58% 13.7M 20s
313000K .......... .......... .......... .......... .......... 58% 12.9M 20s
313050K .......... .......... .......... .......... .......... 58% 15.6M 20s
313100K .......... .......... .......... .......... .......... 58% 11.8M 20s
313150K .......... .......... .......... .......... .......... 58% 13.4M 20s
313200K .......... .......... .......... .......... .......... 58% 20.0M 20s
313250K .......... .......... .......... .......... .......... 58% 38.9M 20s
313300K .......... .......... .......... .......... .......... 58% 12.8M 20s
313350K .......... .......... .......... .......... .......... 58% 48.2M 20s
313400K .......... .......... .......... .......... .......... 58% 28.6M 20s
313450K .......... .......... .......... .......... .......... 58% 20.7M 20s
313500K .......... .......... .......... .......... .......... 58% 17.7M 20s
313550K .......... .......... .......... .......... .......... 58% 19.5M 20s
313600K .......... .......... .......... .......... .......... 58% 13.3M 20s
313650K .......... .......... .......... .......... .......... 58% 17.6M 20s
313700K .......... .......... .......... .......... .......... 58% 15.1M 20s
313750K .......... .......... .......... .......... .......... 58% 15.7M 20s
313800K .......... .......... .......... .......... .......... 58% 17.2M 20s
313850K .......... .......... .......... .......... .......... 58% 17.0M 20s
313900K .......... .......... .......... .......... .......... 58% 21.5M 20s
313950K .......... .......... .......... .......... .......... 58% 16.1M 20s
314000K .......... .......... .......... .......... .......... 58% 16.3M 20s
314050K .......... .......... .......... .......... .......... 58% 22.2M 20s
314100K .......... .......... .......... .......... .......... 58% 13.3M 20s
314150K .......... .......... .......... .......... .......... 58% 9.07M 20s
314200K .......... .......... .......... .......... .......... 58% 11.3M 20s
314250K .......... .......... .......... .......... .......... 58% 11.9M 20s
314300K .......... .......... .......... .......... .......... 58% 14.6M 20s
314350K .......... .......... .......... .......... .......... 58% 11.5M 20s
314400K .......... .......... .......... .......... .......... 58% 12.9M 20s
314450K .......... .......... .......... .......... .......... 58% 12.0M 20s
314500K .......... .......... .......... .......... .......... 58% 17.1M 20s
314550K .......... .......... .......... .......... .......... 58% 15.3M 20s
314600K .......... .......... .......... .......... .......... 58% 12.5M 20s
314650K .......... .......... .......... .......... .......... 58% 42.1M 20s
314700K .......... .......... .......... .......... .......... 58% 43.5M 20s
314750K .......... .......... .......... .......... .......... 58% 21.4M 20s
314800K .......... .......... .......... .......... .......... 58% 18.9M 20s
314850K .......... .......... .......... .......... .......... 58%  110M 20s
314900K .......... .......... .......... .......... .......... 58%  161M 20s
314950K .......... .......... .......... .......... .......... 58%  145M 20s
315000K .......... .......... .......... .......... .......... 58% 43.8M 20s
315050K .......... .......... .......... .......... .......... 58% 36.2M 20s
315100K .......... .......... .......... .......... .......... 58% 32.6M 20s
315150K .......... .......... .......... .......... .......... 58% 40.3M 20s
315200K .......... .......... .......... .......... .......... 58% 30.7M 20s
315250K .......... .......... .......... .......... .......... 58% 36.9M 20s
315300K .......... .......... .......... .......... .......... 58% 57.2M 20s
315350K .......... .......... .......... .......... .......... 58% 36.6M 20s
315400K .......... .......... .......... .......... .......... 58% 49.8M 20s
315450K .......... .......... .......... .......... .......... 58% 31.7M 20s
315500K .......... .......... .......... .......... .......... 58% 44.2M 20s
315550K .......... .......... .......... .......... .......... 58% 48.4M 20s
315600K .......... .......... .......... .......... .......... 58% 36.3M 20s
315650K .......... .......... .......... .......... .......... 58% 37.6M 20s
315700K .......... .......... .......... .......... .......... 58% 37.1M 20s
315750K .......... .......... .......... .......... .......... 58% 47.9M 20s
315800K .......... .......... .......... .......... .......... 58% 52.2M 20s
315850K .......... .......... .......... .......... .......... 58% 38.1M 20s
315900K .......... .......... .......... .......... .......... 58% 35.5M 20s
315950K .......... .......... .......... .......... .......... 58% 45.0M 20s
316000K .......... .......... .......... .......... .......... 58% 54.0M 20s
316050K .......... .......... .......... .......... .......... 58% 50.1M 20s
316100K .......... .......... .......... .......... .......... 58% 27.4M 20s
316150K .......... .......... .......... .......... .......... 58% 47.9M 20s
316200K .......... .......... .......... .......... .......... 58% 55.4M 20s
316250K .......... .......... .......... .......... .......... 58% 51.0M 20s
316300K .......... .......... .......... .......... .......... 58% 71.1M 20s
316350K .......... .......... .......... .......... .......... 58% 53.2M 20s
316400K .......... .......... .......... .......... .......... 58% 18.5M 20s
316450K .......... .......... .......... .......... .......... 58% 94.4M 20s
316500K .......... .......... .......... .......... .......... 58%  128M 20s
316550K .......... .......... .......... .......... .......... 58%  132M 20s
316600K .......... .......... .......... .......... .......... 58% 79.3M 20s
316650K .......... .......... .......... .......... .......... 58% 92.0M 20s
316700K .......... .......... .......... .......... .......... 58% 50.8M 20s
316750K .......... .......... .......... .......... .......... 58% 53.6M 20s
316800K .......... .......... .......... .......... .......... 58%  122M 20s
316850K .......... .......... .......... .......... .......... 58% 54.9M 19s
316900K .......... .......... .......... .......... .......... 58%  105M 19s
316950K .......... .......... .......... .......... .......... 58% 46.3M 19s
317000K .......... .......... .......... .......... .......... 58% 62.3M 19s
317050K .......... .......... .......... .......... .......... 59% 58.3M 19s
317100K .......... .......... .......... .......... .......... 59% 41.5M 19s
317150K .......... .......... .......... .......... .......... 59% 41.6M 19s
317200K .......... .......... .......... .......... .......... 59% 36.7M 19s
317250K .......... .......... .......... .......... .......... 59% 56.2M 19s
317300K .......... .......... .......... .......... .......... 59% 65.2M 19s
317350K .......... .......... .......... .......... .......... 59% 29.6M 19s
317400K .......... .......... .......... .......... .......... 59% 98.8M 19s
317450K .......... .......... .......... .......... .......... 59% 35.2M 19s
317500K .......... .......... .......... .......... .......... 59% 49.6M 19s
317550K .......... .......... .......... .......... .......... 59% 49.1M 19s
317600K .......... .......... .......... .......... .......... 59% 40.3M 19s
317650K .......... .......... .......... .......... .......... 59% 41.5M 19s
317700K .......... .......... .......... .......... .......... 59% 41.6M 19s
317750K .......... .......... .......... .......... .......... 59% 60.7M 19s
317800K .......... .......... .......... .......... .......... 59% 40.2M 19s
317850K .......... .......... .......... .......... .......... 59% 19.1M 19s
317900K .......... .......... .......... .......... .......... 59% 48.1M 19s
317950K .......... .......... .......... .......... .......... 59% 71.7M 19s
318000K .......... .......... .......... .......... .......... 59% 45.9M 19s
318050K .......... .......... .......... .......... .......... 59% 46.5M 19s
318100K .......... .......... .......... .......... .......... 59% 43.9M 19s
318150K .......... .......... .......... .......... .......... 59% 43.7M 19s
318200K .......... .......... .......... .......... .......... 59% 42.5M 19s
318250K .......... .......... .......... .......... .......... 59% 66.1M 19s
318300K .......... .......... .......... .......... .......... 59% 42.6M 19s
318350K .......... .......... .......... .......... .......... 59% 54.0M 19s
318400K .......... .......... .......... .......... .......... 59% 30.3M 19s
318450K .......... .......... .......... .......... .......... 59% 15.3M 19s
318500K .......... .......... .......... .......... .......... 59% 98.8M 19s
318550K .......... .......... .......... .......... .......... 59%  124M 19s
318600K .......... .......... .......... .......... .......... 59% 12.0M 19s
318650K .......... .......... .......... .......... .......... 59%  166M 19s
318700K .......... .......... .......... .......... .......... 59% 37.6M 19s
318750K .......... .......... .......... .......... .......... 59% 44.2M 19s
318800K .......... .......... .......... .......... .......... 59% 24.7M 19s
318850K .......... .......... .......... .......... .......... 59% 18.0M 19s
318900K .......... .......... .......... .......... .......... 59% 24.8M 19s
318950K .......... .......... .......... .......... .......... 59% 19.3M 19s
319000K .......... .......... .......... .......... .......... 59% 25.5M 19s
319050K .......... .......... .......... .......... .......... 59% 21.5M 19s
319100K .......... .......... .......... .......... .......... 59% 20.2M 19s
319150K .......... .......... .......... .......... .......... 59% 17.4M 19s
319200K .......... .......... .......... .......... .......... 59% 17.9M 19s
319250K .......... .......... .......... .......... .......... 59% 21.0M 19s
319300K .......... .......... .......... .......... .......... 59% 25.0M 19s
319350K .......... .......... .......... .......... .......... 59% 17.2M 19s
319400K .......... .......... .......... .......... .......... 59% 40.5M 19s
319450K .......... .......... .......... .......... .......... 59% 19.1M 19s
319500K .......... .......... .......... .......... .......... 59% 23.0M 19s
319550K .......... .......... .......... .......... .......... 59% 20.2M 19s
319600K .......... .......... .......... .......... .......... 59% 13.0M 19s
319650K .......... .......... .......... .......... .......... 59% 29.8M 19s
319700K .......... .......... .......... .......... .......... 59% 13.6M 19s
319750K .......... .......... .......... .......... .......... 59% 34.3M 19s
319800K .......... .......... .......... .......... .......... 59% 27.8M 19s
319850K .......... .......... .......... .......... .......... 59% 18.2M 19s
319900K .......... .......... .......... .......... .......... 59% 21.8M 19s
319950K .......... .......... .......... .......... .......... 59% 22.2M 19s
320000K .......... .......... .......... .......... .......... 59% 34.9M 19s
320050K .......... .......... .......... .......... .......... 59% 21.5M 19s
320100K .......... .......... .......... .......... .......... 59% 27.8M 19s
320150K .......... .......... .......... .......... .......... 59% 19.5M 19s
320200K .......... .......... .......... .......... .......... 59% 32.8M 19s
320250K .......... .......... .......... .......... .......... 59% 18.0M 19s
320300K .......... .......... .......... .......... .......... 59% 23.0M 19s
320350K .......... .......... .......... .......... .......... 59% 23.4M 19s
320400K .......... .......... .......... .......... .......... 59% 36.2M 19s
320450K .......... .......... .......... .......... .......... 59% 22.3M 19s
320500K .......... .......... .......... .......... .......... 59% 24.9M 19s
320550K .......... .......... .......... .......... .......... 59% 31.0M 19s
320600K .......... .......... .......... .......... .......... 59% 24.0M 19s
320650K .......... .......... .......... .......... .......... 59% 21.7M 19s
320700K .......... .......... .......... .......... .......... 59% 41.3M 19s
320750K .......... .......... .......... .......... .......... 59% 38.4M 19s
320800K .......... .......... .......... .......... .......... 59% 84.3M 19s
320850K .......... .......... .......... .......... .......... 59% 41.7M 19s
320900K .......... .......... .......... .......... .......... 59% 59.5M 19s
320950K .......... .......... .......... .......... .......... 59% 23.7M 19s
321000K .......... .......... .......... .......... .......... 59% 80.7M 19s
321050K .......... .......... .......... .......... .......... 59% 14.7M 19s
321100K .......... .......... .......... .......... .......... 59% 89.8M 19s
321150K .......... .......... .......... .......... .......... 59%  138M 19s
321200K .......... .......... .......... .......... .......... 59% 29.0M 19s
321250K .......... .......... .......... .......... .......... 59% 31.9M 19s
321300K .......... .......... .......... .......... .......... 59% 40.4M 19s
321350K .......... .......... .......... .......... .......... 59% 33.4M 19s
321400K .......... .......... .......... .......... .......... 59% 23.4M 19s
321450K .......... .......... .......... .......... .......... 59% 30.0M 19s
321500K .......... .......... .......... .......... .......... 59% 25.3M 19s
321550K .......... .......... .......... .......... .......... 59% 15.7M 19s
321600K .......... .......... .......... .......... .......... 59% 24.1M 19s
321650K .......... .......... .......... .......... .......... 59% 18.6M 19s
321700K .......... .......... .......... .......... .......... 59% 15.5M 19s
321750K .......... .......... .......... .......... .......... 59% 23.7M 19s
321800K .......... .......... .......... .......... .......... 59% 18.6M 19s
321850K .......... .......... .......... .......... .......... 59% 16.2M 19s
321900K .......... .......... .......... .......... .......... 59% 21.9M 19s
321950K .......... .......... .......... .......... .......... 59% 18.2M 19s
322000K .......... .......... .......... .......... .......... 59% 22.8M 19s
322050K .......... .......... .......... .......... .......... 59% 15.0M 19s
322100K .......... .......... .......... .......... .......... 59% 18.3M 19s
322150K .......... .......... .......... .......... .......... 59% 30.3M 19s
322200K .......... .......... .......... .......... .......... 59% 94.3M 19s
322250K .......... .......... .......... .......... .......... 59% 11.6M 19s
322300K .......... .......... .......... .......... .......... 59%  100M 19s
322350K .......... .......... .......... .......... .......... 59% 12.9M 19s
322400K .......... .......... .......... .......... .......... 60% 19.6M 19s
322450K .......... .......... .......... .......... .......... 60% 26.8M 19s
322500K .......... .......... .......... .......... .......... 60% 25.5M 19s
322550K .......... .......... .......... .......... .......... 60% 22.3M 19s
322600K .......... .......... .......... .......... .......... 60% 19.6M 19s
322650K .......... .......... .......... .......... .......... 60% 23.5M 19s
322700K .......... .......... .......... .......... .......... 60% 24.6M 19s
322750K .......... .......... .......... .......... .......... 60% 27.4M 19s
322800K .......... .......... .......... .......... .......... 60% 21.4M 19s
322850K .......... .......... .......... .......... .......... 60% 19.5M 19s
322900K .......... .......... .......... .......... .......... 60% 32.2M 19s
322950K .......... .......... .......... .......... .......... 60% 18.1M 19s
323000K .......... .......... .......... .......... .......... 60% 20.6M 19s
323050K .......... .......... .......... .......... .......... 60% 24.6M 19s
323100K .......... .......... .......... .......... .......... 60% 23.1M 19s
323150K .......... .......... .......... .......... .......... 60% 21.3M 19s
323200K .......... .......... .......... .......... .......... 60% 17.4M 19s
323250K .......... .......... .......... .......... .......... 60% 15.0M 19s
323300K .......... .......... .......... .......... .......... 60% 10.4M 19s
323350K .......... .......... .......... .......... .......... 60% 20.0M 19s
323400K .......... .......... .......... .......... .......... 60% 15.1M 19s
323450K .......... .......... .......... .......... .......... 60% 10.9M 19s
323500K .......... .......... .......... .......... .......... 60% 15.9M 19s
323550K .......... .......... .......... .......... .......... 60% 16.0M 19s
323600K .......... .......... .......... .......... .......... 60% 11.0M 19s
323650K .......... .......... .......... .......... .......... 60% 13.5M 19s
323700K .......... .......... .......... .......... .......... 60% 10.9M 19s
323750K .......... .......... .......... .......... .......... 60% 16.1M 19s
323800K .......... .......... .......... .......... .......... 60% 18.7M 19s
323850K .......... .......... .......... .......... .......... 60% 11.5M 19s
323900K .......... .......... .......... .......... .......... 60% 15.0M 19s
323950K .......... .......... .......... .......... .......... 60% 13.1M 19s
324000K .......... .......... .......... .......... .......... 60% 14.5M 19s
324050K .......... .......... .......... .......... .......... 60% 18.5M 19s
324100K .......... .......... .......... .......... .......... 60% 10.1M 19s
324150K .......... .......... .......... .......... .......... 60% 45.0M 19s
324200K .......... .......... .......... .......... .......... 60% 21.6M 19s
324250K .......... .......... .......... .......... .......... 60% 23.4M 19s
324300K .......... .......... .......... .......... .......... 60% 16.8M 19s
324350K .......... .......... .......... .......... .......... 60% 17.6M 19s
324400K .......... .......... .......... .......... .......... 60% 19.8M 19s
324450K .......... .......... .......... .......... .......... 60% 17.8M 19s
324500K .......... .......... .......... .......... .......... 60% 12.1M 19s
324550K .......... .......... .......... .......... .......... 60% 17.0M 19s
324600K .......... .......... .......... .......... .......... 60% 11.5M 19s
324650K .......... .......... .......... .......... .......... 60% 10.9M 19s
324700K .......... .......... .......... .......... .......... 60% 10.3M 19s
324750K .......... .......... .......... .......... .......... 60% 7.55M 19s
324800K .......... .......... .......... .......... .......... 60% 7.83M 19s
324850K .......... .......... .......... .......... .......... 60% 6.30M 19s
324900K .......... .......... .......... .......... .......... 60% 7.91M 19s
324950K .......... .......... .......... .......... .......... 60% 6.96M 19s
325000K .......... .......... .......... .......... .......... 60% 9.42M 19s
325050K .......... .......... .......... .......... .......... 60% 10.8M 19s
325100K .......... .......... .......... .......... .......... 60% 20.2M 19s
325150K .......... .......... .......... .......... .......... 60% 27.7M 19s
325200K .......... .......... .......... .......... .......... 60% 17.4M 19s
325250K .......... .......... .......... .......... .......... 60% 34.1M 19s
325300K .......... .......... .......... .......... .......... 60% 22.0M 19s
325350K .......... .......... .......... .......... .......... 60% 24.9M 19s
325400K .......... .......... .......... .......... .......... 60% 20.2M 19s
325450K .......... .......... .......... .......... .......... 60% 7.30M 18s
325500K .......... .......... .......... .......... .......... 60% 36.2M 18s
325550K .......... .......... .......... .......... .......... 60% 12.5M 18s
325600K .......... .......... .......... .......... .......... 60% 9.83M 18s
325650K .......... .......... .......... .......... .......... 60% 10.4M 18s
325700K .......... .......... .......... .......... .......... 60% 10.3M 18s
325750K .......... .......... .......... .......... .......... 60% 12.4M 18s
325800K .......... .......... .......... .......... .......... 60% 12.4M 18s
325850K .......... .......... .......... .......... .......... 60% 11.7M 18s
325900K .......... .......... .......... .......... .......... 60% 10.1M 18s
325950K .......... .......... .......... .......... .......... 60% 14.1M 18s
326000K .......... .......... .......... .......... .......... 60% 14.8M 18s
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326100K .......... .......... .......... .......... .......... 60% 16.1M 18s
326150K .......... .......... .......... .......... .......... 60% 33.0M 18s
326200K .......... .......... .......... .......... .......... 60% 22.0M 18s
326250K .......... .......... .......... .......... .......... 60% 20.2M 18s
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326500K .......... .......... .......... .......... .......... 60% 24.5M 18s
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326600K .......... .......... .......... .......... .......... 60% 19.8M 18s
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326700K .......... .......... .......... .......... .......... 60% 29.3M 18s
326750K .......... .......... .......... .......... .......... 60% 27.9M 18s
326800K .......... .......... .......... .......... .......... 60% 31.3M 18s
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326900K .......... .......... .......... .......... .......... 60% 26.0M 18s
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327000K .......... .......... .......... .......... .......... 60% 38.1M 18s
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327100K .......... .......... .......... .......... .......... 60% 33.9M 18s
327150K .......... .......... .......... .......... .......... 60%  126M 18s
327200K .......... .......... .......... .......... .......... 60%  112M 18s
327250K .......... .......... .......... .......... .......... 60% 11.3M 18s
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327350K .......... .......... .......... .......... .......... 60% 97.7M 18s
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327450K .......... .......... .......... .......... .......... 60% 28.6M 18s
327500K .......... .......... .......... .......... .......... 60%  119M 18s
327550K .......... .......... .......... .......... .......... 60% 25.7M 18s
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327750K .......... .......... .......... .......... .......... 60% 12.7M 18s
327800K .......... .......... .......... .......... .......... 61% 22.6M 18s
327850K .......... .......... .......... .......... .......... 61% 19.9M 18s
327900K .......... .......... .......... .......... .......... 61% 22.4M 18s
327950K .......... .......... .......... .......... .......... 61% 16.1M 18s
328000K .......... .......... .......... .......... .......... 61% 22.7M 18s
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328100K .......... .......... .......... .......... .......... 61% 17.3M 18s
328150K .......... .......... .......... .......... .......... 61% 18.6M 18s
328200K .......... .......... .......... .......... .......... 61% 17.4M 18s
328250K .......... .......... .......... .......... .......... 61% 15.7M 18s
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328350K .......... .......... .......... .......... .......... 61% 9.62M 18s
328400K .......... .......... .......... .......... .......... 61% 12.0M 18s
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328500K .......... .......... .......... .......... .......... 61% 15.8M 18s
328550K .......... .......... .......... .......... .......... 61% 13.1M 18s
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329000K .......... .......... .......... .......... .......... 61% 18.8M 18s
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329100K .......... .......... .......... .......... .......... 61% 13.6M 18s
329150K .......... .......... .......... .......... .......... 61% 30.3M 18s
329200K .......... .......... .......... .......... .......... 61% 24.3M 18s
329250K .......... .......... .......... .......... .......... 61% 20.7M 18s
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329350K .......... .......... .......... .......... .......... 61% 18.6M 18s
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329550K .......... .......... .......... .......... .......... 61% 13.6M 18s
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329900K .......... .......... .......... .......... .......... 61% 18.2M 18s
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330000K .......... .......... .......... .......... .......... 61% 20.0M 18s
330050K .......... .......... .......... .......... .......... 61% 16.9M 18s
330100K .......... .......... .......... .......... .......... 61% 8.83M 18s
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330200K .......... .......... .......... .......... .......... 61% 26.2M 18s
330250K .......... .......... .......... .......... .......... 61% 23.5M 18s
330300K .......... .......... .......... .......... .......... 61% 23.1M 18s
330350K .......... .......... .......... .......... .......... 61% 25.2M 18s
330400K .......... .......... .......... .......... .......... 61% 22.0M 18s
330450K .......... .......... .......... .......... .......... 61% 35.1M 18s
330500K .......... .......... .......... .......... .......... 61% 26.1M 18s
330550K .......... .......... .......... .......... .......... 61% 28.9M 18s
330600K .......... .......... .......... .......... .......... 61% 26.2M 18s
330650K .......... .......... .......... .......... .......... 61% 22.8M 18s
330700K .......... .......... .......... .......... .......... 61% 28.6M 18s
330750K .......... .......... .......... .......... .......... 61% 21.2M 18s
330800K .......... .......... .......... .......... .......... 61% 29.5M 18s
330850K .......... .......... .......... .......... .......... 61% 29.9M 18s
330900K .......... .......... .......... .......... .......... 61% 27.8M 18s
330950K .......... .......... .......... .......... .......... 61% 33.9M 18s
331000K .......... .......... .......... .......... .......... 61% 31.5M 18s
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331100K .......... .......... .......... .......... .......... 61% 34.5M 18s
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331200K .......... .......... .......... .......... .......... 61% 56.1M 18s
331250K .......... .......... .......... .......... .......... 61% 76.4M 18s
331300K .......... .......... .......... .......... .......... 61% 51.9M 18s
331350K .......... .......... .......... .......... .......... 61% 68.6M 18s
331400K .......... .......... .......... .......... .......... 61%  101M 18s
331450K .......... .......... .......... .......... .......... 61% 11.6M 18s
331500K .......... .......... .......... .......... .......... 61% 97.3M 18s
331550K .......... .......... .......... .......... .......... 61%  116M 18s
331600K .......... .......... .......... .......... .......... 61%  112M 18s
331650K .......... .......... .......... .......... .......... 61% 98.6M 18s
331700K .......... .......... .......... .......... .......... 61%  145M 18s
331750K .......... .......... .......... .......... .......... 61%  180M 18s
331800K .......... .......... .......... .......... .......... 61% 72.8M 18s
331850K .......... .......... .......... .......... .......... 61% 44.5M 18s
331900K .......... .......... .......... .......... .......... 61% 75.0M 18s
331950K .......... .......... .......... .......... .......... 61% 22.7M 18s
332000K .......... .......... .......... .......... .......... 61% 36.0M 18s
332050K .......... .......... .......... .......... .......... 61%  105M 18s
332100K .......... .......... .......... .......... .......... 61% 33.6M 18s
332150K .......... .......... .......... .......... .......... 61% 31.2M 18s
332200K .......... .......... .......... .......... .......... 61% 27.3M 18s
332250K .......... .......... .......... .......... .......... 61% 30.2M 18s
332300K .......... .......... .......... .......... .......... 61% 27.8M 18s
332350K .......... .......... .......... .......... .......... 61% 19.9M 18s
332400K .......... .......... .......... .......... .......... 61% 35.8M 18s
332450K .......... .......... .......... .......... .......... 61% 8.25M 18s
332500K .......... .......... .......... .......... .......... 61% 36.0M 18s
332550K .......... .......... .......... .......... .......... 61% 24.9M 18s
332600K .......... .......... .......... .......... .......... 61% 31.3M 18s
332650K .......... .......... .......... .......... .......... 61% 24.1M 18s
332700K .......... .......... .......... .......... .......... 61% 34.1M 18s
332750K .......... .......... .......... .......... .......... 61% 29.3M 18s
332800K .......... .......... .......... .......... .......... 61% 35.5M 18s
332850K .......... .......... .......... .......... .......... 61% 23.1M 18s
332900K .......... .......... .......... .......... .......... 61% 27.2M 18s
332950K .......... .......... .......... .......... .......... 61% 24.3M 18s
333000K .......... .......... .......... .......... .......... 61% 31.7M 18s
333050K .......... .......... .......... .......... .......... 61% 14.1M 18s
333100K .......... .......... .......... .......... .......... 61% 61.0M 18s
333150K .......... .......... .......... .......... .......... 62% 28.7M 18s
333200K .......... .......... .......... .......... .......... 62% 40.3M 18s
333250K .......... .......... .......... .......... .......... 62% 40.6M 18s
333300K .......... .......... .......... .......... .......... 62% 53.7M 18s
333350K .......... .......... .......... .......... .......... 62% 19.8M 18s
333400K .......... .......... .......... .......... .......... 62% 23.2M 18s
333450K .......... .......... .......... .......... .......... 62% 20.9M 18s
333500K .......... .......... .......... .......... .......... 62% 21.1M 18s
333550K .......... .......... .......... .......... .......... 62% 36.7M 18s
333600K .......... .......... .......... .......... .......... 62% 13.3M 18s
333650K .......... .......... .......... .......... .......... 62% 30.7M 18s
333700K .......... .......... .......... .......... .......... 62% 15.5M 18s
333750K .......... .......... .......... .......... .......... 62% 17.0M 18s
333800K .......... .......... .......... .......... .......... 62% 25.8M 18s
333850K .......... .......... .......... .......... .......... 62% 14.6M 18s
333900K .......... .......... .......... .......... .......... 62% 15.2M 18s
333950K .......... .......... .......... .......... .......... 62% 15.3M 18s
334000K .......... .......... .......... .......... .......... 62% 20.9M 18s
334050K .......... .......... .......... .......... .......... 62% 10.7M 18s
334100K .......... .......... .......... .......... .......... 62% 10.8M 18s
334150K .......... .......... .......... .......... .......... 62% 12.6M 18s
334200K .......... .......... .......... .......... .......... 62% 10.4M 18s
334250K .......... .......... .......... .......... .......... 62% 11.1M 18s
334300K .......... .......... .......... .......... .......... 62% 9.81M 18s
334350K .......... .......... .......... .......... .......... 62% 10.4M 17s
334400K .......... .......... .......... .......... .......... 62% 9.50M 17s
334450K .......... .......... .......... .......... .......... 62% 9.70M 17s
334500K .......... .......... .......... .......... .......... 62% 11.2M 17s
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334600K .......... .......... .......... .......... .......... 62% 23.4M 17s
334650K .......... .......... .......... .......... .......... 62% 9.67M 17s
334700K .......... .......... .......... .......... .......... 62% 21.1M 17s
334750K .......... .......... .......... .......... .......... 62% 16.3M 17s
334800K .......... .......... .......... .......... .......... 62% 12.8M 17s
334850K .......... .......... .......... .......... .......... 62% 13.8M 17s
334900K .......... .......... .......... .......... .......... 62% 16.7M 17s
334950K .......... .......... .......... .......... .......... 62% 17.1M 17s
335000K .......... .......... .......... .......... .......... 62% 14.7M 17s
335050K .......... .......... .......... .......... .......... 62% 15.9M 17s
335100K .......... .......... .......... .......... .......... 62% 15.1M 17s
335150K .......... .......... .......... .......... .......... 62% 17.1M 17s
335200K .......... .......... .......... .......... .......... 62% 14.0M 17s
335250K .......... .......... .......... .......... .......... 62% 9.67M 17s
335300K .......... .......... .......... .......... .......... 62% 15.6M 17s
335350K .......... .......... .......... .......... .......... 62% 11.2M 17s
335400K .......... .......... .......... .......... .......... 62% 13.4M 17s
335450K .......... .......... .......... .......... .......... 62% 9.42M 17s
335500K .......... .......... .......... .......... .......... 62% 16.6M 17s
335550K .......... .......... .......... .......... .......... 62% 23.9M 17s
335600K .......... .......... .......... .......... .......... 62% 14.3M 17s
335650K .......... .......... .......... .......... .......... 62% 17.3M 17s
335700K .......... .......... .......... .......... .......... 62% 19.5M 17s
335750K .......... .......... .......... .......... .......... 62% 16.3M 17s
335800K .......... .......... .......... .......... .......... 62% 19.1M 17s
335850K .......... .......... .......... .......... .......... 62% 14.0M 17s
335900K .......... .......... .......... .......... .......... 62% 24.2M 17s
335950K .......... .......... .......... .......... .......... 62% 12.9M 17s
336000K .......... .......... .......... .......... .......... 62% 17.6M 17s
336050K .......... .......... .......... .......... .......... 62% 21.8M 17s
336100K .......... .......... .......... .......... .......... 62% 18.2M 17s
336150K .......... .......... .......... .......... .......... 62% 33.1M 17s
336200K .......... .......... .......... .......... .......... 62% 32.7M 17s
336250K .......... .......... .......... .......... .......... 62% 60.6M 17s
336300K .......... .......... .......... .......... .......... 62% 23.6M 17s
336350K .......... .......... .......... .......... .......... 62% 20.0M 17s
336400K .......... .......... .......... .......... .......... 62% 50.0M 17s
336450K .......... .......... .......... .......... .......... 62% 23.4M 17s
336500K .......... .......... .......... .......... .......... 62% 20.3M 17s
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336650K .......... .......... .......... .......... .......... 62% 24.4M 17s
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336900K .......... .......... .......... .......... .......... 62% 22.5M 17s
336950K .......... .......... .......... .......... .......... 62% 18.9M 17s
337000K .......... .......... .......... .......... .......... 62% 23.7M 17s
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337100K .......... .......... .......... .......... .......... 62% 20.6M 17s
337150K .......... .......... .......... .......... .......... 62% 18.9M 17s
337200K .......... .......... .......... .......... .......... 62% 11.4M 17s
337250K .......... .......... .......... .......... .......... 62% 20.8M 17s
337300K .......... .......... .......... .......... .......... 62% 27.2M 17s
337350K .......... .......... .......... .......... .......... 62% 13.8M 17s
337400K .......... .......... .......... .......... .......... 62% 21.6M 17s
337450K .......... .......... .......... .......... .......... 62% 12.2M 17s
337500K .......... .......... .......... .......... .......... 62% 14.7M 17s
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337700K .......... .......... .......... .......... .......... 62% 11.5M 17s
337750K .......... .......... .......... .......... .......... 62% 13.3M 17s
337800K .......... .......... .......... .......... .......... 62% 14.7M 17s
337850K .......... .......... .......... .......... .......... 62% 10.8M 17s
337900K .......... .......... .......... .......... .......... 62% 8.89M 17s
337950K .......... .......... .......... .......... .......... 62% 20.9M 17s
338000K .......... .......... .......... .......... .......... 62% 13.0M 17s
338050K .......... .......... .......... .......... .......... 62% 22.5M 17s
338100K .......... .......... .......... .......... .......... 62% 20.0M 17s
338150K .......... .......... .......... .......... .......... 62% 14.8M 17s
338200K .......... .......... .......... .......... .......... 62% 15.7M 17s
338250K .......... .......... .......... .......... .......... 62% 19.8M 17s
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338350K .......... .......... .......... .......... .......... 62% 10.9M 17s
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338500K .......... .......... .......... .......... .......... 62% 13.3M 17s
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338600K .......... .......... .......... .......... .......... 63% 10.5M 17s
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338700K .......... .......... .......... .......... .......... 63% 17.8M 17s
338750K .......... .......... .......... .......... .......... 63% 62.3M 17s
338800K .......... .......... .......... .......... .......... 63% 25.5M 17s
338850K .......... .......... .......... .......... .......... 63% 18.7M 17s
338900K .......... .......... .......... .......... .......... 63% 23.7M 17s
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339000K .......... .......... .......... .......... .......... 63% 22.7M 17s
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339100K .......... .......... .......... .......... .......... 63% 20.8M 17s
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339200K .......... .......... .......... .......... .......... 63% 21.6M 17s
339250K .......... .......... .......... .......... .......... 63% 19.1M 17s
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340000K .......... .......... .......... .......... .......... 63% 14.2M 17s
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340200K .......... .......... .......... .......... .......... 63% 33.9M 17s
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340300K .......... .......... .......... .......... .......... 63%  139M 17s
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340500K .......... .......... .......... .......... .......... 63% 34.5M 17s
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340600K .......... .......... .......... .......... .......... 63% 33.9M 17s
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340900K .......... .......... .......... .......... .......... 63% 26.6M 17s
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342000K .......... .......... .......... .......... .......... 63% 14.3M 17s
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342150K .......... .......... .......... .......... .......... 63% 14.5M 17s
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342250K .......... .......... .......... .......... .......... 63% 21.8M 17s
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343000K .......... .......... .......... .......... .......... 63% 22.8M 17s
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343100K .......... .......... .......... .......... .......... 63% 14.7M 17s
343150K .......... .......... .......... .......... .......... 63% 20.1M 17s
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343250K .......... .......... .......... .......... .......... 63% 20.8M 17s
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343400K .......... .......... .......... .......... .......... 63% 19.5M 17s
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343550K .......... .......... .......... .......... .......... 63% 17.7M 17s
343600K .......... .......... .......... .......... .......... 63% 57.6M 17s
343650K .......... .......... .......... .......... .......... 63% 16.8M 17s
343700K .......... .......... .......... .......... .......... 63% 36.6M 17s
343750K .......... .......... .......... .......... .......... 63% 22.3M 17s
343800K .......... .......... .......... .......... .......... 63% 26.5M 17s
343850K .......... .......... .......... .......... .......... 63% 17.4M 17s
343900K .......... .......... .......... .......... .......... 64% 21.9M 16s
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344000K .......... .......... .......... .......... .......... 64% 20.0M 16s
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344250K .......... .......... .......... .......... .......... 64% 24.2M 16s
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345000K .......... .......... .......... .......... .......... 64% 20.5M 16s
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345100K .......... .......... .......... .......... .......... 64% 16.2M 16s
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345200K .......... .......... .......... .......... .......... 64% 15.3M 16s
345250K .......... .......... .......... .......... .......... 64% 14.1M 16s
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345400K .......... .......... .......... .......... .......... 64% 9.92M 16s
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345600K .......... .......... .......... .......... .......... 64% 10.7M 16s
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345800K .......... .......... .......... .......... .......... 64% 10.4M 16s
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345900K .......... .......... .......... .......... .......... 64% 10.8M 16s
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346000K .......... .......... .......... .......... .......... 64% 13.1M 16s
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346100K .......... .......... .......... .......... .......... 64% 17.6M 16s
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346200K .......... .......... .......... .......... .......... 64% 15.3M 16s
346250K .......... .......... .......... .......... .......... 64% 24.0M 16s
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346350K .......... .......... .......... .......... .......... 64% 15.2M 16s
346400K .......... .......... .......... .......... .......... 64% 15.3M 16s
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346500K .......... .......... .......... .......... .......... 64% 15.1M 16s
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346600K .......... .......... .......... .......... .......... 64% 17.8M 16s
346650K .......... .......... .......... .......... .......... 64% 21.5M 16s
346700K .......... .......... .......... .......... .......... 64% 15.8M 16s
346750K .......... .......... .......... .......... .......... 64% 25.5M 16s
346800K .......... .......... .......... .......... .......... 64% 23.2M 16s
346850K .......... .......... .......... .......... .......... 64% 17.5M 16s
346900K .......... .......... .......... .......... .......... 64% 51.6M 16s
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347000K .......... .......... .......... .......... .......... 64%  118M 16s
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347100K .......... .......... .......... .......... .......... 64% 21.8M 16s
347150K .......... .......... .......... .......... .......... 64% 17.3M 16s
347200K .......... .......... .......... .......... .......... 64% 30.6M 16s
347250K .......... .......... .......... .......... .......... 64% 28.8M 16s
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348000K .......... .......... .......... .......... .......... 64% 21.9M 16s
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348100K .......... .......... .......... .......... .......... 64% 33.1M 16s
348150K .......... .......... .......... .......... .......... 64% 69.6M 16s
348200K .......... .......... .......... .......... .......... 64% 37.4M 16s
348250K .......... .......... .......... .......... .......... 64% 69.3M 16s
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348700K .......... .......... .......... .......... .......... 64% 23.5M 16s
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350000K .......... .......... .......... .......... .......... 65% 21.8M 16s
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350300K .......... .......... .......... .......... .......... 65% 22.3M 16s
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350400K .......... .......... .......... .......... .......... 65% 23.7M 16s
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350500K .......... .......... .......... .......... .......... 65% 28.7M 16s
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350650K .......... .......... .......... .......... .......... 65% 31.9M 16s
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350750K .......... .......... .......... .......... .......... 65% 21.5M 16s
350800K .......... .......... .......... .......... .......... 65%  142M 16s
350850K .......... .......... .......... .......... .......... 65% 11.9M 16s
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350950K .......... .......... .......... .......... .......... 65% 19.9M 16s
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352000K .......... .......... .......... .......... .......... 65% 10.1M 16s
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352150K .......... .......... .......... .......... .......... 65% 9.65M 16s
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352250K .......... .......... .......... .......... .......... 65% 10.9M 16s
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352800K .......... .......... .......... .......... .......... 65% 18.0M 16s
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353000K .......... .......... .......... .......... .......... 65% 1.92M 16s
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353250K .......... .......... .......... .......... .......... 65% 19.7M 16s
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356100K .......... .......... .......... .......... .......... 66% 16.0M 15s
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358000K .......... .......... .......... .......... .......... 66% 20.7M 15s
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358250K .......... .......... .......... .......... .......... 66% 16.3M 15s
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359950K .......... .......... .......... .......... .......... 66% 7.66M 15s
360000K .......... .......... .......... .......... .......... 66% 9.35M 15s
360050K .......... .......... .......... .......... .......... 67% 11.3M 15s
360100K .......... .......... .......... .......... .......... 67% 9.29M 15s
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360200K .......... .......... .......... .......... .......... 67% 7.75M 15s
360250K .......... .......... .......... .......... .......... 67% 10.4M 15s
360300K .......... .......... .......... .......... .......... 67% 9.15M 15s
360350K .......... .......... .......... .......... .......... 67% 8.29M 15s
360400K .......... .......... .......... .......... .......... 67% 4.14M 15s
360450K .......... .......... .......... .......... .......... 67% 17.0M 15s
360500K .......... .......... .......... .......... .......... 67% 21.2M 15s
360550K .......... .......... .......... .......... .......... 67% 20.6M 15s
360600K .......... .......... .......... .......... .......... 67% 15.3M 15s
360650K .......... .......... .......... .......... .......... 67% 24.0M 15s
360700K .......... .......... .......... .......... .......... 67% 18.3M 15s
360750K .......... .......... .......... .......... .......... 67% 19.7M 15s
360800K .......... .......... .......... .......... .......... 67% 22.3M 15s
360850K .......... .......... .......... .......... .......... 67% 16.4M 15s
360900K .......... .......... .......... .......... .......... 67% 20.9M 15s
360950K .......... .......... .......... .......... .......... 67% 20.0M 15s
361000K .......... .......... .......... .......... .......... 67% 17.3M 15s
361050K .......... .......... .......... .......... .......... 67% 19.2M 15s
361100K .......... .......... .......... .......... .......... 67% 19.9M 15s
361150K .......... .......... .......... .......... .......... 67% 28.2M 15s
361200K .......... .......... .......... .......... .......... 67% 21.5M 15s
361250K .......... .......... .......... .......... .......... 67% 31.6M 15s
361300K .......... .......... .......... .......... .......... 67% 51.7M 15s
361350K .......... .......... .......... .......... .......... 67% 15.5M 15s
361400K .......... .......... .......... .......... .......... 67% 31.9M 15s
361450K .......... .......... .......... .......... .......... 67% 39.4M 15s
361500K .......... .......... .......... .......... .......... 67% 35.4M 15s
361550K .......... .......... .......... .......... .......... 67% 22.0M 15s
361600K .......... .......... .......... .......... .......... 67% 20.6M 15s
361650K .......... .......... .......... .......... .......... 67% 19.8M 15s
361700K .......... .......... .......... .......... .......... 67% 18.3M 15s
361750K .......... .......... .......... .......... .......... 67% 20.8M 15s
361800K .......... .......... .......... .......... .......... 67% 23.8M 15s
361850K .......... .......... .......... .......... .......... 67% 20.4M 15s
361900K .......... .......... .......... .......... .......... 67% 3.95M 15s
361950K .......... .......... .......... .......... .......... 67% 20.7M 15s
362000K .......... .......... .......... .......... .......... 67% 8.83M 15s
362050K .......... .......... .......... .......... .......... 67% 21.9M 15s
362100K .......... .......... .......... .......... .......... 67% 18.0M 15s
362150K .......... .......... .......... .......... .......... 67% 10.6M 15s
362200K .......... .......... .......... .......... .......... 67% 16.1M 15s
362250K .......... .......... .......... .......... .......... 67% 14.6M 15s
362300K .......... .......... .......... .......... .......... 67% 19.1M 15s
362350K .......... .......... .......... .......... .......... 67% 15.2M 15s
362400K .......... .......... .......... .......... .......... 67% 14.5M 15s
362450K .......... .......... .......... .......... .......... 67% 15.4M 15s
362500K .......... .......... .......... .......... .......... 67% 26.3M 15s
362550K .......... .......... .......... .......... .......... 67% 15.2M 15s
362600K .......... .......... .......... .......... .......... 67% 16.3M 15s
362650K .......... .......... .......... .......... .......... 67% 19.4M 15s
362700K .......... .......... .......... .......... .......... 67% 13.4M 15s
362750K .......... .......... .......... .......... .......... 67% 14.9M 15s
362800K .......... .......... .......... .......... .......... 67% 19.0M 15s
362850K .......... .......... .......... .......... .......... 67% 16.9M 15s
362900K .......... .......... .......... .......... .......... 67% 5.75M 15s
362950K .......... .......... .......... .......... .......... 67% 17.9M 15s
363000K .......... .......... .......... .......... .......... 67% 12.4M 15s
363050K .......... .......... .......... .......... .......... 67% 16.2M 15s
363100K .......... .......... .......... .......... .......... 67% 26.4M 15s
363150K .......... .......... .......... .......... .......... 67% 23.9M 15s
363200K .......... .......... .......... .......... .......... 67% 15.6M 15s
363250K .......... .......... .......... .......... .......... 67% 23.9M 15s
363300K .......... .......... .......... .......... .......... 67% 20.3M 15s
363350K .......... .......... .......... .......... .......... 67% 18.0M 15s
363400K .......... .......... .......... .......... .......... 67% 24.2M 15s
363450K .......... .......... .......... .......... .......... 67% 19.3M 15s
363500K .......... .......... .......... .......... .......... 67% 21.1M 15s
363550K .......... .......... .......... .......... .......... 67% 17.6M 15s
363600K .......... .......... .......... .......... .......... 67% 18.0M 15s
363650K .......... .......... .......... .......... .......... 67% 22.0M 15s
363700K .......... .......... .......... .......... .......... 67% 19.4M 15s
363750K .......... .......... .......... .......... .......... 67% 13.5M 15s
363800K .......... .......... .......... .......... .......... 67% 38.8M 15s
363850K .......... .......... .......... .......... .......... 67% 23.4M 15s
363900K .......... .......... .......... .......... .......... 67% 21.3M 15s
363950K .......... .......... .......... .......... .......... 67% 5.09M 15s
364000K .......... .......... .......... .......... .......... 67%  117M 15s
364050K .......... .......... .......... .......... .......... 67%  136M 15s
364100K .......... .......... .......... .......... .......... 67%  130M 15s
364150K .......... .......... .......... .......... .......... 67%  189M 15s
364200K .......... .......... .......... .......... .......... 67% 14.9M 15s
364250K .......... .......... .......... .......... .......... 67% 16.5M 15s
364300K .......... .......... .......... .......... .......... 67% 16.1M 15s
364350K .......... .......... .......... .......... .......... 67% 15.4M 15s
364400K .......... .......... .......... .......... .......... 67% 23.2M 15s
364450K .......... .......... .......... .......... .......... 67% 15.8M 15s
364500K .......... .......... .......... .......... .......... 67% 16.6M 15s
364550K .......... .......... .......... .......... .......... 67% 18.4M 15s
364600K .......... .......... .......... .......... .......... 67% 14.1M 15s
364650K .......... .......... .......... .......... .......... 67% 22.9M 15s
364700K .......... .......... .......... .......... .......... 67% 16.9M 15s
364750K .......... .......... .......... .......... .......... 67% 18.7M 15s
364800K .......... .......... .......... .......... .......... 67% 19.2M 15s
364850K .......... .......... .......... .......... .......... 67% 17.2M 15s
364900K .......... .......... .......... .......... .......... 67% 66.9M 15s
364950K .......... .......... .......... .......... .......... 67% 14.9M 15s
365000K .......... .......... .......... .......... .......... 67% 13.7M 15s
365050K .......... .......... .......... .......... .......... 67% 94.3M 15s
365100K .......... .......... .......... .......... .......... 67% 19.3M 15s
365150K .......... .......... .......... .......... .......... 67% 32.7M 15s
365200K .......... .......... .......... .......... .......... 67% 21.8M 15s
365250K .......... .......... .......... .......... .......... 67% 22.6M 15s
365300K .......... .......... .......... .......... .......... 67% 18.8M 15s
365350K .......... .......... .......... .......... .......... 67% 21.4M 15s
365400K .......... .......... .......... .......... .......... 68% 17.6M 15s
365450K .......... .......... .......... .......... .......... 68% 21.3M 15s
365500K .......... .......... .......... .......... .......... 68% 21.4M 15s
365550K .......... .......... .......... .......... .......... 68% 23.7M 15s
365600K .......... .......... .......... .......... .......... 68% 14.5M 15s
365650K .......... .......... .......... .......... .......... 68% 20.7M 15s
365700K .......... .......... .......... .......... .......... 68% 18.4M 15s
365750K .......... .......... .......... .......... .......... 68% 21.3M 15s
365800K .......... .......... .......... .......... .......... 68% 19.7M 15s
365850K .......... .......... .......... .......... .......... 68% 14.8M 15s
365900K .......... .......... .......... .......... .......... 68% 23.6M 15s
365950K .......... .......... .......... .......... .......... 68% 23.0M 15s
366000K .......... .......... .......... .......... .......... 68% 10.1M 15s
366050K .......... .......... .......... .......... .......... 68%  149M 15s
366100K .......... .......... .......... .......... .......... 68% 27.0M 15s
366150K .......... .......... .......... .......... .......... 68% 23.6M 15s
366200K .......... .......... .......... .......... .......... 68% 15.2M 15s
366250K .......... .......... .......... .......... .......... 68%  111M 14s
366300K .......... .......... .......... .......... .......... 68% 29.0M 14s
366350K .......... .......... .......... .......... .......... 68% 27.9M 14s
366400K .......... .......... .......... .......... .......... 68% 31.8M 14s
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366500K .......... .......... .......... .......... .......... 68% 33.7M 14s
366550K .......... .......... .......... .......... .......... 68% 36.5M 14s
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366650K .......... .......... .......... .......... .......... 68% 39.3M 14s
366700K .......... .......... .......... .......... .......... 68% 28.7M 14s
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366800K .......... .......... .......... .......... .......... 68% 48.8M 14s
366850K .......... .......... .......... .......... .......... 68% 30.9M 14s
366900K .......... .......... .......... .......... .......... 68% 29.3M 14s
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367000K .......... .......... .......... .......... .......... 68% 25.6M 14s
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367100K .......... .......... .......... .......... .......... 68% 23.3M 14s
367150K .......... .......... .......... .......... .......... 68% 30.6M 14s
367200K .......... .......... .......... .......... .......... 68% 24.9M 14s
367250K .......... .......... .......... .......... .......... 68% 35.0M 14s
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367400K .......... .......... .......... .......... .......... 68% 49.1M 14s
367450K .......... .......... .......... .......... .......... 68% 13.2M 14s
367500K .......... .......... .......... .......... .......... 68%  103M 14s
367550K .......... .......... .......... .......... .......... 68% 20.2M 14s
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367850K .......... .......... .......... .......... .......... 68% 16.7M 14s
367900K .......... .......... .......... .......... .......... 68% 18.5M 14s
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368000K .......... .......... .......... .......... .......... 68% 20.0M 14s
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368100K .......... .......... .......... .......... .......... 68% 15.8M 14s
368150K .......... .......... .......... .......... .......... 68% 21.0M 14s
368200K .......... .......... .......... .......... .......... 68% 14.0M 14s
368250K .......... .......... .......... .......... .......... 68% 20.9M 14s
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368350K .......... .......... .......... .......... .......... 68% 15.4M 14s
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368450K .......... .......... .......... .......... .......... 68% 18.9M 14s
368500K .......... .......... .......... .......... .......... 68% 10.4M 14s
368550K .......... .......... .......... .......... .......... 68% 99.4M 14s
368600K .......... .......... .......... .......... .......... 68% 27.2M 14s
368650K .......... .......... .......... .......... .......... 68% 45.6M 14s
368700K .......... .......... .......... .......... .......... 68% 16.5M 14s
368750K .......... .......... .......... .......... .......... 68% 46.5M 14s
368800K .......... .......... .......... .......... .......... 68% 31.4M 14s
368850K .......... .......... .......... .......... .......... 68% 20.1M 14s
368900K .......... .......... .......... .......... .......... 68% 7.52M 14s
368950K .......... .......... .......... .......... .......... 68% 7.98M 14s
369000K .......... .......... .......... .......... .......... 68% 19.2M 14s
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369100K .......... .......... .......... .......... .......... 68% 20.3M 14s
369150K .......... .......... .......... .......... .......... 68% 30.0M 14s
369200K .......... .......... .......... .......... .......... 68% 17.9M 14s
369250K .......... .......... .......... .......... .......... 68% 22.2M 14s
369300K .......... .......... .......... .......... .......... 68% 32.1M 14s
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369450K .......... .......... .......... .......... .......... 68% 23.7M 14s
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369600K .......... .......... .......... .......... .......... 68% 84.5M 14s
369650K .......... .......... .......... .......... .......... 68% 13.2M 14s
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369750K .......... .......... .......... .......... .......... 68% 38.7M 14s
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369850K .......... .......... .......... .......... .......... 68% 38.5M 14s
369900K .......... .......... .......... .......... .......... 68% 23.0M 14s
369950K .......... .......... .......... .......... .......... 68% 14.6M 14s
370000K .......... .......... .......... .......... .......... 68% 21.8M 14s
370050K .......... .......... .......... .......... .......... 68% 20.2M 14s
370100K .......... .......... .......... .......... .......... 68% 14.0M 14s
370150K .......... .......... .......... .......... .......... 68% 18.8M 14s
370200K .......... .......... .......... .......... .......... 68% 14.0M 14s
370250K .......... .......... .......... .......... .......... 68% 16.5M 14s
370300K .......... .......... .......... .......... .......... 68% 22.5M 14s
370350K .......... .......... .......... .......... .......... 68% 15.9M 14s
370400K .......... .......... .......... .......... .......... 68% 17.4M 14s
370450K .......... .......... .......... .......... .......... 68% 18.1M 14s
370500K .......... .......... .......... .......... .......... 68% 16.6M 14s
370550K .......... .......... .......... .......... .......... 68% 10.3M 14s
370600K .......... .......... .......... .......... .......... 68% 10.7M 14s
370650K .......... .......... .......... .......... .......... 68% 11.6M 14s
370700K .......... .......... .......... .......... .......... 68% 11.7M 14s
370750K .......... .......... .......... .......... .......... 68% 16.4M 14s
370800K .......... .......... .......... .......... .......... 69% 15.8M 14s
370850K .......... .......... .......... .......... .......... 69% 11.7M 14s
370900K .......... .......... .......... .......... .......... 69% 17.4M 14s
370950K .......... .......... .......... .......... .......... 69% 12.9M 14s
371000K .......... .......... .......... .......... .......... 69% 12.9M 14s
371050K .......... .......... .......... .......... .......... 69% 15.9M 14s
371100K .......... .......... .......... .......... .......... 69% 3.58M 14s
371150K .......... .......... .......... .......... .......... 69% 29.4M 14s
371200K .......... .......... .......... .......... .......... 69% 22.9M 14s
371250K .......... .......... .......... .......... .......... 69% 33.6M 14s
371300K .......... .......... .......... .......... .......... 69% 41.9M 14s
371350K .......... .......... .......... .......... .......... 69% 26.7M 14s
371400K .......... .......... .......... .......... .......... 69% 27.3M 14s
371450K .......... .......... .......... .......... .......... 69% 18.3M 14s
371500K .......... .......... .......... .......... .......... 69% 19.1M 14s
371550K .......... .......... .......... .......... .......... 69% 20.5M 14s
371600K .......... .......... .......... .......... .......... 69% 16.4M 14s
371650K .......... .......... .......... .......... .......... 69% 19.9M 14s
371700K .......... .......... .......... .......... .......... 69% 18.0M 14s
371750K .......... .......... .......... .......... .......... 69% 24.1M 14s
371800K .......... .......... .......... .......... .......... 69% 25.8M 14s
371850K .......... .......... .......... .......... .......... 69% 21.9M 14s
371900K .......... .......... .......... .......... .......... 69% 21.5M 14s
371950K .......... .......... .......... .......... .......... 69% 19.0M 14s
372000K .......... .......... .......... .......... .......... 69% 18.6M 14s
372050K .......... .......... .......... .......... .......... 69% 18.5M 14s
372100K .......... .......... .......... .......... .......... 69% 18.9M 14s
372150K .......... .......... .......... .......... .......... 69% 22.9M 14s
372200K .......... .......... .......... .......... .......... 69% 21.5M 14s
372250K .......... .......... .......... .......... .......... 69% 34.2M 14s
372300K .......... .......... .......... .......... .......... 69% 20.9M 14s
372350K .......... .......... .......... .......... .......... 69% 19.8M 14s
372400K .......... .......... .......... .......... .......... 69% 19.6M 14s
372450K .......... .......... .......... .......... .......... 69% 19.4M 14s
372500K .......... .......... .......... .......... .......... 69% 13.8M 14s
372550K .......... .......... .......... .......... .......... 69% 24.2M 14s
372600K .......... .......... .......... .......... .......... 69% 15.9M 14s
372650K .......... .......... .......... .......... .......... 69% 17.6M 14s
372700K .......... .......... .......... .......... .......... 69% 15.1M 14s
372750K .......... .......... .......... .......... .......... 69% 21.8M 14s
372800K .......... .......... .......... .......... .......... 69% 15.0M 14s
372850K .......... .......... .......... .......... .......... 69% 14.9M 14s
372900K .......... .......... .......... .......... .......... 69%  430K 14s
372950K .......... .......... .......... .......... .......... 69%  118M 14s
373000K .......... .......... .......... .......... .......... 69% 96.9M 14s
373050K .......... .......... .......... .......... .......... 69%  138M 14s
373100K .......... .......... .......... .......... .......... 69% 85.5M 14s
373150K .......... .......... .......... .......... .......... 69% 76.9M 14s
373200K .......... .......... .......... .......... .......... 69% 24.7M 14s
373250K .......... .......... .......... .......... .......... 69% 21.7M 14s
373300K .......... .......... .......... .......... .......... 69%  135M 14s
373350K .......... .......... .......... .......... .......... 69% 27.3M 14s
373400K .......... .......... .......... .......... .......... 69% 27.2M 14s
373450K .......... .......... .......... .......... .......... 69% 28.1M 14s
373500K .......... .......... .......... .......... .......... 69% 24.9M 14s
373550K .......... .......... .......... .......... .......... 69% 31.2M 14s
373600K .......... .......... .......... .......... .......... 69% 31.1M 14s
373650K .......... .......... .......... .......... .......... 69% 22.5M 14s
373700K .......... .......... .......... .......... .......... 69% 24.7M 14s
373750K .......... .......... .......... .......... .......... 69% 36.5M 14s
373800K .......... .......... .......... .......... .......... 69% 31.3M 14s
373850K .......... .......... .......... .......... .......... 69% 28.0M 14s
373900K .......... .......... .......... .......... .......... 69% 36.2M 14s
373950K .......... .......... .......... .......... .......... 69% 26.0M 14s
374000K .......... .......... .......... .......... .......... 69% 35.3M 14s
374050K .......... .......... .......... .......... .......... 69% 25.9M 14s
374100K .......... .......... .......... .......... .......... 69% 37.4M 14s
374150K .......... .......... .......... .......... .......... 69% 25.0M 14s
374200K .......... .......... .......... .......... .......... 69% 21.2M 14s
374250K .......... .......... .......... .......... .......... 69% 20.4M 14s
374300K .......... .......... .......... .......... .......... 69% 36.0M 14s
374350K .......... .......... .......... .......... .......... 69% 35.2M 14s
374400K .......... .......... .......... .......... .......... 69% 26.7M 14s
374450K .......... .......... .......... .......... .......... 69% 25.2M 14s
374500K .......... .......... .......... .......... .......... 69% 13.6M 14s
374550K .......... .......... .......... .......... .......... 69%  126M 14s
374600K .......... .......... .......... .......... .......... 69% 28.1M 14s
374650K .......... .......... .......... .......... .......... 69%  130M 14s
374700K .......... .......... .......... .......... .......... 69% 67.5M 14s
374750K .......... .......... .......... .......... .......... 69% 21.9M 14s
374800K .......... .......... .......... .......... .......... 69% 66.3M 14s
374850K .......... .......... .......... .......... .......... 69% 92.1M 14s
374900K .......... .......... .......... .......... .......... 69% 29.0M 14s
374950K .......... .......... .......... .......... .......... 69% 88.5M 14s
375000K .......... .......... .......... .......... .......... 69% 24.9M 14s
375050K .......... .......... .......... .......... .......... 69% 30.0M 14s
375100K .......... .......... .......... .......... .......... 69% 27.2M 14s
375150K .......... .......... .......... .......... .......... 69% 25.2M 14s
375200K .......... .......... .......... .......... .......... 69% 25.6M 14s
375250K .......... .......... .......... .......... .......... 69% 23.6M 14s
375300K .......... .......... .......... .......... .......... 69% 22.7M 14s
375350K .......... .......... .......... .......... .......... 69% 22.4M 14s
375400K .......... .......... .......... .......... .......... 69% 34.3M 14s
375450K .......... .......... .......... .......... .......... 69% 23.2M 14s
375500K .......... .......... .......... .......... .......... 69% 35.6M 14s
375550K .......... .......... .......... .......... .......... 69% 23.0M 14s
375600K .......... .......... .......... .......... .......... 69% 23.7M 14s
375650K .......... .......... .......... .......... .......... 69% 33.0M 14s
375700K .......... .......... .......... .......... .......... 69% 20.1M 14s
375750K .......... .......... .......... .......... .......... 69% 29.2M 14s
375800K .......... .......... .......... .......... .......... 69% 21.1M 14s
375850K .......... .......... .......... .......... .......... 69% 22.5M 14s
375900K .......... .......... .......... .......... .......... 69% 29.2M 14s
375950K .......... .......... .......... .......... .......... 69% 29.3M 14s
376000K .......... .......... .......... .......... .......... 69% 17.5M 14s
376050K .......... .......... .......... .......... .......... 69%  120M 14s
376100K .......... .......... .......... .......... .......... 69% 13.8M 14s
376150K .......... .......... .......... .......... .......... 70% 25.9M 14s
376200K .......... .......... .......... .......... .......... 70% 29.9M 14s
376250K .......... .......... .......... .......... .......... 70% 8.06M 14s
376300K .......... .......... .......... .......... .......... 70%  217M 14s
376350K .......... .......... .......... .......... .......... 70% 27.4M 14s
376400K .......... .......... .......... .......... .......... 70% 19.1M 14s
376450K .......... .......... .......... .......... .......... 70% 14.4M 14s
376500K .......... .......... .......... .......... .......... 70% 22.5M 14s
376550K .......... .......... .......... .......... .......... 70% 19.8M 13s
376600K .......... .......... .......... .......... .......... 70% 14.1M 13s
376650K .......... .......... .......... .......... .......... 70% 20.9M 13s
376700K .......... .......... .......... .......... .......... 70% 14.9M 13s
376750K .......... .......... .......... .......... .......... 70% 21.0M 13s
376800K .......... .......... .......... .......... .......... 70% 19.9M 13s
376850K .......... .......... .......... .......... .......... 70% 16.1M 13s
376900K .......... .......... .......... .......... .......... 70% 26.3M 13s
376950K .......... .......... .......... .......... .......... 70% 12.5M 13s
377000K .......... .......... .......... .......... .......... 70% 15.7M 13s
377050K .......... .......... .......... .......... .......... 70% 19.6M 13s
377100K .......... .......... .......... .......... .......... 70% 19.8M 13s
377150K .......... .......... .......... .......... .......... 70% 17.1M 13s
377200K .......... .......... .......... .......... .......... 70% 27.4M 13s
377250K .......... .......... .......... .......... .......... 70% 2.35M 13s
377300K .......... .......... .......... .......... .......... 70% 35.7M 13s
377350K .......... .......... .......... .......... .......... 70% 14.9M 13s
377400K .......... .......... .......... .......... .......... 70% 30.0M 13s
377450K .......... .......... .......... .......... .......... 70% 20.4M 13s
377500K .......... .......... .......... .......... .......... 70% 28.9M 13s
377550K .......... .......... .......... .......... .......... 70% 30.9M 13s
377600K .......... .......... .......... .......... .......... 70% 11.3M 13s
377650K .......... .......... .......... .......... .......... 70% 19.9M 13s
377700K .......... .......... .......... .......... .......... 70% 13.1M 13s
377750K .......... .......... .......... .......... .......... 70% 14.8M 13s
377800K .......... .......... .......... .......... .......... 70% 7.77M 13s
377850K .......... .......... .......... .......... .......... 70% 14.8M 13s
377900K .......... .......... .......... .......... .......... 70% 15.0M 13s
377950K .......... .......... .......... .......... .......... 70% 9.43M 13s
378000K .......... .......... .......... .......... .......... 70% 16.4M 13s
378050K .......... .......... .......... .......... .......... 70% 14.8M 13s
378100K .......... .......... .......... .......... .......... 70% 14.6M 13s
378150K .......... .......... .......... .......... .......... 70% 14.6M 13s
378200K .......... .......... .......... .......... .......... 70% 15.8M 13s
378250K .......... .......... .......... .......... .......... 70% 26.4M 13s
378300K .......... .......... .......... .......... .......... 70% 16.1M 13s
378350K .......... .......... .......... .......... .......... 70% 22.4M 13s
378400K .......... .......... .......... .......... .......... 70% 33.7M 13s
378450K .......... .......... .......... .......... .......... 70% 19.8M 13s
378500K .......... .......... .......... .......... .......... 70% 19.2M 13s
378550K .......... .......... .......... .......... .......... 70% 25.5M 13s
378600K .......... .......... .......... .......... .......... 70% 13.7M 13s
378650K .......... .......... .......... .......... .......... 70% 18.4M 13s
378700K .......... .......... .......... .......... .......... 70% 14.9M 13s
378750K .......... .......... .......... .......... .......... 70% 22.1M 13s
378800K .......... .......... .......... .......... .......... 70% 16.4M 13s
378850K .......... .......... .......... .......... .......... 70% 14.8M 13s
378900K .......... .......... .......... .......... .......... 70% 17.1M 13s
378950K .......... .......... .......... .......... .......... 70% 12.3M 13s
379000K .......... .......... .......... .......... .......... 70% 20.4M 13s
379050K .......... .......... .......... .......... .......... 70% 9.80M 13s
379100K .......... .......... .......... .......... .......... 70% 11.4M 13s
379150K .......... .......... .......... .......... .......... 70% 19.3M 13s
379200K .......... .......... .......... .......... .......... 70% 9.91M 13s
379250K .......... .......... .......... .......... .......... 70%  486K 13s
379300K .......... .......... .......... .......... .......... 70% 21.7M 13s
379350K .......... .......... .......... .......... .......... 70%  101M 13s
379400K .......... .......... .......... .......... .......... 70%  127M 13s
379450K .......... .......... .......... .......... .......... 70%  107M 13s
379500K .......... .......... .......... .......... .......... 70%  138M 13s
379550K .......... .......... .......... .......... .......... 70% 23.8M 13s
379600K .......... .......... .......... .......... .......... 70% 21.7M 13s
379650K .......... .......... .......... .......... .......... 70% 33.8M 13s
379700K .......... .......... .......... .......... .......... 70% 21.1M 13s
379750K .......... .......... .......... .......... .......... 70% 39.4M 13s
379800K .......... .......... .......... .......... .......... 70% 34.4M 13s
379850K .......... .......... .......... .......... .......... 70% 28.1M 13s
379900K .......... .......... .......... .......... .......... 70% 35.7M 13s
379950K .......... .......... .......... .......... .......... 70% 22.2M 13s
380000K .......... .......... .......... .......... .......... 70% 39.6M 13s
380050K .......... .......... .......... .......... .......... 70% 20.3M 13s
380100K .......... .......... .......... .......... .......... 70% 32.0M 13s
380150K .......... .......... .......... .......... .......... 70% 24.2M 13s
380200K .......... .......... .......... .......... .......... 70% 34.7M 13s
380250K .......... .......... .......... .......... .......... 70% 35.0M 13s
380300K .......... .......... .......... .......... .......... 70% 25.8M 13s
380350K .......... .......... .......... .......... .......... 70% 17.4M 13s
380400K .......... .......... .......... .......... .......... 70% 23.4M 13s
380450K .......... .......... .......... .......... .......... 70% 32.3M 13s
380500K .......... .......... .......... .......... .......... 70% 32.5M 13s
380550K .......... .......... .......... .......... .......... 70% 30.3M 13s
380600K .......... .......... .......... .......... .......... 70% 20.2M 13s
380650K .......... .......... .......... .......... .......... 70% 19.3M 13s
380700K .......... .......... .......... .......... .......... 70% 81.1M 13s
380750K .......... .......... .......... .......... .......... 70% 21.4M 13s
380800K .......... .......... .......... .......... .......... 70% 29.3M 13s
380850K .......... .......... .......... .......... .......... 70% 22.2M 13s
380900K .......... .......... .......... .......... .......... 70% 15.0M 13s
380950K .......... .......... .......... .......... .......... 70% 16.8M 13s
381000K .......... .......... .......... .......... .......... 70% 15.3M 13s
381050K .......... .......... .......... .......... .......... 70% 15.3M 13s
381100K .......... .......... .......... .......... .......... 70% 16.4M 13s
381150K .......... .......... .......... .......... .......... 70% 15.0M 13s
381200K .......... .......... .......... .......... .......... 70% 16.6M 13s
381250K .......... .......... .......... .......... .......... 70% 19.4M 13s
381300K .......... .......... .......... .......... .......... 70% 15.5M 13s
381350K .......... .......... .......... .......... .......... 70% 10.0M 13s
381400K .......... .......... .......... .......... .......... 70% 20.8M 13s
381450K .......... .......... .......... .......... .......... 70% 26.4M 13s
381500K .......... .......... .......... .......... .......... 70% 30.2M 13s
381550K .......... .......... .......... .......... .......... 71% 16.6M 13s
381600K .......... .......... .......... .......... .......... 71% 25.6M 13s
381650K .......... .......... .......... .......... .......... 71% 58.6M 13s
381700K .......... .......... .......... .......... .......... 71% 20.1M 13s
381750K .......... .......... .......... .......... .......... 71% 20.5M 13s
381800K .......... .......... .......... .......... .......... 71% 23.7M 13s
381850K .......... .......... .......... .......... .......... 71% 20.5M 13s
381900K .......... .......... .......... .......... .......... 71% 18.1M 13s
381950K .......... .......... .......... .......... .......... 71% 19.1M 13s
382000K .......... .......... .......... .......... .......... 71% 24.7M 13s
382050K .......... .......... .......... .......... .......... 71% 22.1M 13s
382100K .......... .......... .......... .......... .......... 71% 19.0M 13s
382150K .......... .......... .......... .......... .......... 71% 18.7M 13s
382200K .......... .......... .......... .......... .......... 71% 20.8M 13s
382250K .......... .......... .......... .......... .......... 71% 20.4M 13s
382300K .......... .......... .......... .......... .......... 71% 20.5M 13s
382350K .......... .......... .......... .......... .......... 71% 21.3M 13s
382400K .......... .......... .......... .......... .......... 71% 15.8M 13s
382450K .......... .......... .......... .......... .......... 71% 20.1M 13s
382500K .......... .......... .......... .......... .......... 71% 22.5M 13s
382550K .......... .......... .......... .......... .......... 71% 35.5M 13s
382600K .......... .......... .......... .......... .......... 71% 31.9M 13s
382650K .......... .......... .......... .......... .......... 71% 83.5M 13s
382700K .......... .......... .......... .......... .......... 71% 19.7M 13s
382750K .......... .......... .......... .......... .......... 71%  142M 13s
382800K .......... .......... .......... .......... .......... 71% 24.0M 13s
382850K .......... .......... .......... .......... .......... 71% 61.8M 13s
382900K .......... .......... .......... .......... .......... 71% 32.9M 13s
382950K .......... .......... .......... .......... .......... 71% 28.4M 13s
383000K .......... .......... .......... .......... .......... 71% 43.8M 13s
383050K .......... .......... .......... .......... .......... 71% 23.9M 13s
383100K .......... .......... .......... .......... .......... 71% 20.4M 13s
383150K .......... .......... .......... .......... .......... 71% 21.6M 13s
383200K .......... .......... .......... .......... .......... 71% 19.5M 13s
383250K .......... .......... .......... .......... .......... 71% 24.6M 13s
383300K .......... .......... .......... .......... .......... 71% 27.0M 13s
383350K .......... .......... .......... .......... .......... 71% 19.0M 13s
383400K .......... .......... .......... .......... .......... 71% 22.0M 13s
383450K .......... .......... .......... .......... .......... 71% 15.8M 13s
383500K .......... .......... .......... .......... .......... 71% 37.1M 13s
383550K .......... .......... .......... .......... .......... 71% 24.8M 13s
383600K .......... .......... .......... .......... .......... 71% 19.6M 13s
383650K .......... .......... .......... .......... .......... 71% 22.0M 13s
383700K .......... .......... .......... .......... .......... 71% 22.6M 13s
383750K .......... .......... .......... .......... .......... 71% 18.3M 13s
383800K .......... .......... .......... .......... .......... 71% 16.0M 13s
383850K .......... .......... .......... .......... .......... 71% 19.6M 13s
383900K .......... .......... .......... .......... .......... 71% 18.5M 13s
383950K .......... .......... .......... .......... .......... 71% 54.0M 13s
384000K .......... .......... .......... .......... .......... 71% 28.4M 13s
384050K .......... .......... .......... .......... .......... 71% 29.0M 13s
384100K .......... .......... .......... .......... .......... 71% 20.3M 13s
384150K .......... .......... .......... .......... .......... 71% 23.1M 13s
384200K .......... .......... .......... .......... .......... 71% 20.5M 13s
384250K .......... .......... .......... .......... .......... 71% 31.3M 13s
384300K .......... .......... .......... .......... .......... 71% 23.1M 13s
384350K .......... .......... .......... .......... .......... 71% 22.8M 13s
384400K .......... .......... .......... .......... .......... 71% 24.0M 13s
384450K .......... .......... .......... .......... .......... 71% 13.9M 13s
384500K .......... .......... .......... .......... .......... 71% 32.8M 13s
384550K .......... .......... .......... .......... .......... 71% 15.7M 13s
384600K .......... .......... .......... .......... .......... 71% 29.8M 13s
384650K .......... .......... .......... .......... .......... 71% 19.3M 13s
384700K .......... .......... .......... .......... .......... 71% 15.9M 13s
384750K .......... .......... .......... .......... .......... 71% 8.73M 13s
384800K .......... .......... .......... .......... .......... 71% 5.07M 13s
384850K .......... .......... .......... .......... .......... 71% 5.82M 13s
384900K .......... .......... .......... .......... .......... 71% 6.14M 13s
384950K .......... .......... .......... .......... .......... 71% 5.45M 13s
385000K .......... .......... .......... .......... .......... 71% 6.72M 13s
385050K .......... .......... .......... .......... .......... 71% 7.08M 13s
385100K .......... .......... .......... .......... .......... 71% 12.3M 13s
385150K .......... .......... .......... .......... .......... 71% 25.5M 13s
385200K .......... .......... .......... .......... .......... 71% 16.2M 13s
385250K .......... .......... .......... .......... .......... 71% 47.0M 13s
385300K .......... .......... .......... .......... .......... 71% 20.7M 13s
385350K .......... .......... .......... .......... .......... 71% 17.7M 13s
385400K .......... .......... .......... .......... .......... 71% 23.6M 13s
385450K .......... .......... .......... .......... .......... 71% 14.3M 13s
385500K .......... .......... .......... .......... .......... 71% 19.6M 13s
385550K .......... .......... .......... .......... .......... 71% 39.2M 13s
385600K .......... .......... .......... .......... .......... 71% 21.0M 13s
385650K .......... .......... .......... .......... .......... 71% 23.1M 13s
385700K .......... .......... .......... .......... .......... 71% 20.0M 13s
385750K .......... .......... .......... .......... .......... 71% 21.3M 13s
385800K .......... .......... .......... .......... .......... 71% 24.0M 13s
385850K .......... .......... .......... .......... .......... 71% 20.8M 13s
385900K .......... .......... .......... .......... .......... 71% 22.4M 13s
385950K .......... .......... .......... .......... .......... 71% 23.4M 13s
386000K .......... .......... .......... .......... .......... 71% 22.6M 13s
386050K .......... .......... .......... .......... .......... 71% 29.4M 13s
386100K .......... .......... .......... .......... .......... 71% 31.0M 13s
386150K .......... .......... .......... .......... .......... 71% 15.9M 13s
386200K .......... .......... .......... .......... .......... 71% 23.3M 13s
386250K .......... .......... .......... .......... .......... 71%  117M 13s
386300K .......... .......... .......... .......... .......... 71% 21.2M 13s
386350K .......... .......... .......... .......... .......... 71% 22.0M 13s
386400K .......... .......... .......... .......... .......... 71% 70.0M 13s
386450K .......... .......... .......... .......... .......... 71% 12.8M 13s
386500K .......... .......... .......... .......... .......... 71% 14.7M 13s
386550K .......... .......... .......... .......... .......... 71% 22.6M 13s
386600K .......... .......... .......... .......... .......... 71% 21.3M 13s
386650K .......... .......... .......... .......... .......... 71% 15.4M 13s
386700K .......... .......... .......... .......... .......... 71% 19.7M 13s
386750K .......... .......... .......... .......... .......... 71% 17.5M 13s
386800K .......... .......... .......... .......... .......... 71% 17.6M 13s
386850K .......... .......... .......... .......... .......... 71% 14.0M 13s
386900K .......... .......... .......... .......... .......... 72% 17.9M 13s
386950K .......... .......... .......... .......... .......... 72% 17.7M 13s
387000K .......... .......... .......... .......... .......... 72% 19.7M 13s
387050K .......... .......... .......... .......... .......... 72% 9.64M 13s
387100K .......... .......... .......... .......... .......... 72% 16.2M 13s
387150K .......... .......... .......... .......... .......... 72% 15.4M 13s
387200K .......... .......... .......... .......... .......... 72% 14.3M 13s
387250K .......... .......... .......... .......... .......... 72% 16.2M 13s
387300K .......... .......... .......... .......... .......... 72% 91.8M 13s
387350K .......... .......... .......... .......... .......... 72% 18.4M 12s
387400K .......... .......... .......... .......... .......... 72% 31.9M 12s
387450K .......... .......... .......... .......... .......... 72% 25.9M 12s
387500K .......... .......... .......... .......... .......... 72% 17.3M 12s
387550K .......... .......... .......... .......... .......... 72% 32.5M 12s
387600K .......... .......... .......... .......... .......... 72% 21.5M 12s
387650K .......... .......... .......... .......... .......... 72% 30.0M 12s
387700K .......... .......... .......... .......... .......... 72% 21.8M 12s
387750K .......... .......... .......... .......... .......... 72% 32.8M 12s
387800K .......... .......... .......... .......... .......... 72% 23.2M 12s
387850K .......... .......... .......... .......... .......... 72% 33.5M 12s
387900K .......... .......... .......... .......... .......... 72% 20.0M 12s
387950K .......... .......... .......... .......... .......... 72% 18.9M 12s
388000K .......... .......... .......... .......... .......... 72% 36.2M 12s
388050K .......... .......... .......... .......... .......... 72% 22.5M 12s
388100K .......... .......... .......... .......... .......... 72% 28.4M 12s
388150K .......... .......... .......... .......... .......... 72% 25.7M 12s
388200K .......... .......... .......... .......... .......... 72% 28.2M 12s
388250K .......... .......... .......... .......... .......... 72% 54.4M 12s
388300K .......... .......... .......... .......... .......... 72% 26.6M 12s
388350K .......... .......... .......... .......... .......... 72% 50.1M 12s
388400K .......... .......... .......... .......... .......... 72% 23.3M 12s
388450K .......... .......... .......... .......... .......... 72% 82.3M 12s
388500K .......... .......... .......... .......... .......... 72% 22.5M 12s
388550K .......... .......... .......... .......... .......... 72% 63.9M 12s
388600K .......... .......... .......... .......... .......... 72% 23.1M 12s
388650K .......... .......... .......... .......... .......... 72% 30.9M 12s
388700K .......... .......... .......... .......... .......... 72% 22.5M 12s
388750K .......... .......... .......... .......... .......... 72% 29.7M 12s
388800K .......... .......... .......... .......... .......... 72% 24.6M 12s
388850K .......... .......... .......... .......... .......... 72% 18.7M 12s
388900K .......... .......... .......... .......... .......... 72% 32.6M 12s
388950K .......... .......... .......... .......... .......... 72% 30.9M 12s
389000K .......... .......... .......... .......... .......... 72% 22.6M 12s
389050K .......... .......... .......... .......... .......... 72% 26.3M 12s
389100K .......... .......... .......... .......... .......... 72% 23.3M 12s
389150K .......... .......... .......... .......... .......... 72% 34.7M 12s
389200K .......... .......... .......... .......... .......... 72% 20.4M 12s
389250K .......... .......... .......... .......... .......... 72% 24.1M 12s
389300K .......... .......... .......... .......... .......... 72% 31.5M 12s
389350K .......... .......... .......... .......... .......... 72% 20.8M 12s
389400K .......... .......... .......... .......... .......... 72% 17.8M 12s
389450K .......... .......... .......... .......... .......... 72% 13.8M 12s
389500K .......... .......... .......... .......... .......... 72% 16.8M 12s
389550K .......... .......... .......... .......... .......... 72% 13.1M 12s
389600K .......... .......... .......... .......... .......... 72% 12.4M 12s
389650K .......... .......... .......... .......... .......... 72% 18.3M 12s
389700K .......... .......... .......... .......... .......... 72% 11.3M 12s
389750K .......... .......... .......... .......... .......... 72% 14.5M 12s
389800K .......... .......... .......... .......... .......... 72% 11.6M 12s
389850K .......... .......... .......... .......... .......... 72% 13.3M 12s
389900K .......... .......... .......... .......... .......... 72% 17.0M 12s
389950K .......... .......... .......... .......... .......... 72% 12.5M 12s
390000K .......... .......... .......... .......... .......... 72% 13.8M 12s
390050K .......... .......... .......... .......... .......... 72% 15.1M 12s
390100K .......... .......... .......... .......... .......... 72% 18.8M 12s
390150K .......... .......... .......... .......... .......... 72% 34.5M 12s
390200K .......... .......... .......... .......... .......... 72% 29.1M 12s
390250K .......... .......... .......... .......... .......... 72% 33.1M 12s
390300K .......... .......... .......... .......... .......... 72% 24.1M 12s
390350K .......... .......... .......... .......... .......... 72% 93.7M 12s
390400K .......... .......... .......... .......... .......... 72% 33.5M 12s
390450K .......... .......... .......... .......... .......... 72% 17.7M 12s
390500K .......... .......... .......... .......... .......... 72%  127M 12s
390550K .......... .......... .......... .......... .......... 72% 17.1M 12s
390600K .......... .......... .......... .......... .......... 72% 33.2M 12s
390650K .......... .......... .......... .......... .......... 72% 34.0M 12s
390700K .......... .......... .......... .......... .......... 72% 33.6M 12s
390750K .......... .......... .......... .......... .......... 72% 28.7M 12s
390800K .......... .......... .......... .......... .......... 72% 32.4M 12s
390850K .......... .......... .......... .......... .......... 72% 35.1M 12s
390900K .......... .......... .......... .......... .......... 72% 35.5M 12s
390950K .......... .......... .......... .......... .......... 72% 25.2M 12s
391000K .......... .......... .......... .......... .......... 72% 33.7M 12s
391050K .......... .......... .......... .......... .......... 72% 33.7M 12s
391100K .......... .......... .......... .......... .......... 72% 32.8M 12s
391150K .......... .......... .......... .......... .......... 72% 35.3M 12s
391200K .......... .......... .......... .......... .......... 72% 31.3M 12s
391250K .......... .......... .......... .......... .......... 72% 35.2M 12s
391300K .......... .......... .......... .......... .......... 72% 34.3M 12s
391350K .......... .......... .......... .......... .......... 72% 40.5M 12s
391400K .......... .......... .......... .......... .......... 72% 35.2M 12s
391450K .......... .......... .......... .......... .......... 72% 29.7M 12s
391500K .......... .......... .......... .......... .......... 72% 33.8M 12s
391550K .......... .......... .......... .......... .......... 72% 32.1M 12s
391600K .......... .......... .......... .......... .......... 72% 12.7M 12s
391650K .......... .......... .......... .......... .......... 72% 89.3M 12s
391700K .......... .......... .......... .......... .......... 72% 28.2M 12s
391750K .......... .......... .......... .......... .......... 72% 10.6M 12s
391800K .......... .......... .......... .......... .......... 72%  140M 12s
391850K .......... .......... .......... .......... .......... 72%  130M 12s
391900K .......... .......... .......... .......... .......... 72% 29.1M 12s
391950K .......... .......... .......... .......... .......... 72% 15.5M 12s
392000K .......... .......... .......... .......... .......... 72% 56.8M 12s
392050K .......... .......... .......... .......... .......... 72% 32.5M 12s
392100K .......... .......... .......... .......... .......... 72% 23.1M 12s
392150K .......... .......... .......... .......... .......... 72% 25.4M 12s
392200K .......... .......... .......... .......... .......... 72% 17.2M 12s
392250K .......... .......... .......... .......... .......... 73% 20.3M 12s
392300K .......... .......... .......... .......... .......... 73% 21.9M 12s
392350K .......... .......... .......... .......... .......... 73% 13.6M 12s
392400K .......... .......... .......... .......... .......... 73% 17.7M 12s
392450K .......... .......... .......... .......... .......... 73% 11.3M 12s
392500K .......... .......... .......... .......... .......... 73% 18.3M 12s
392550K .......... .......... .......... .......... .......... 73% 19.4M 12s
392600K .......... .......... .......... .......... .......... 73% 12.7M 12s
392650K .......... .......... .......... .......... .......... 73% 20.2M 12s
392700K .......... .......... .......... .......... .......... 73% 13.8M 12s
392750K .......... .......... .......... .......... .......... 73% 25.4M 12s
392800K .......... .......... .......... .......... .......... 73% 19.6M 12s
392850K .......... .......... .......... .......... .......... 73% 20.2M 12s
392900K .......... .......... .......... .......... .......... 73% 23.2M 12s
392950K .......... .......... .......... .......... .......... 73% 29.6M 12s
393000K .......... .......... .......... .......... .......... 73% 28.2M 12s
393050K .......... .......... .......... .......... .......... 73% 35.9M 12s
393100K .......... .......... .......... .......... .......... 73% 17.3M 12s
393150K .......... .......... .......... .......... .......... 73% 34.1M 12s
393200K .......... .......... .......... .......... .......... 73% 33.5M 12s
393250K .......... .......... .......... .......... .......... 73% 27.3M 12s
393300K .......... .......... .......... .......... .......... 73% 36.0M 12s
393350K .......... .......... .......... .......... .......... 73% 31.7M 12s
393400K .......... .......... .......... .......... .......... 73% 30.7M 12s
393450K .......... .......... .......... .......... .......... 73% 35.5M 12s
393500K .......... .......... .......... .......... .......... 73% 37.2M 12s
393550K .......... .......... .......... .......... .......... 73% 17.2M 12s
393600K .......... .......... .......... .......... .......... 73% 35.1M 12s
393650K .......... .......... .......... .......... .......... 73% 18.3M 12s
393700K .......... .......... .......... .......... .......... 73% 35.3M 12s
393750K .......... .......... .......... .......... .......... 73% 19.4M 12s
393800K .......... .......... .......... .......... .......... 73% 43.1M 12s
393850K .......... .......... .......... .......... .......... 73% 27.7M 12s
393900K .......... .......... .......... .......... .......... 73% 52.4M 12s
393950K .......... .......... .......... .......... .......... 73% 49.8M 12s
394000K .......... .......... .......... .......... .......... 73% 41.8M 12s
394050K .......... .......... .......... .......... .......... 73%  103M 12s
394100K .......... .......... .......... .......... .......... 73% 39.0M 12s
394150K .......... .......... .......... .......... .......... 73% 99.4M 12s
394200K .......... .......... .......... .......... .......... 73% 40.5M 12s
394250K .......... .......... .......... .......... .......... 73% 91.4M 12s
394300K .......... .......... .......... .......... .......... 73% 19.0M 12s
394350K .......... .......... .......... .......... .......... 73%  123M 12s
394400K .......... .......... .......... .......... .......... 73%  112M 12s
394450K .......... .......... .......... .......... .......... 73% 70.3M 12s
394500K .......... .......... .......... .......... .......... 73% 42.1M 12s
394550K .......... .......... .......... .......... .......... 73%  107M 12s
394600K .......... .......... .......... .......... .......... 73% 90.3M 12s
394650K .......... .......... .......... .......... .......... 73% 5.10M 12s
394700K .......... .......... .......... .......... .......... 73% 6.12M 12s
394750K .......... .......... .......... .......... .......... 73% 38.6M 12s
394800K .......... .......... .......... .......... .......... 73% 40.0M 12s
394850K .......... .......... .......... .......... .......... 73% 32.7M 12s
394900K .......... .......... .......... .......... .......... 73% 33.6M 12s
394950K .......... .......... .......... .......... .......... 73% 31.6M 12s
395000K .......... .......... .......... .......... .......... 73% 25.9M 12s
395050K .......... .......... .......... .......... .......... 73% 53.6M 12s
395100K .......... .......... .......... .......... .......... 73% 23.3M 12s
395150K .......... .......... .......... .......... .......... 73% 46.7M 12s
395200K .......... .......... .......... .......... .......... 73% 28.7M 12s
395250K .......... .......... .......... .......... .......... 73% 40.0M 12s
395300K .......... .......... .......... .......... .......... 73% 45.1M 12s
395350K .......... .......... .......... .......... .......... 73% 25.9M 12s
395400K .......... .......... .......... .......... .......... 73% 23.6M 12s
395450K .......... .......... .......... .......... .......... 73% 17.8M 12s
395500K .......... .......... .......... .......... .......... 73% 15.6M 12s
395550K .......... .......... .......... .......... .......... 73% 91.4M 12s
395600K .......... .......... .......... .......... .......... 73% 17.5M 12s
395650K .......... .......... .......... .......... .......... 73% 25.4M 12s
395700K .......... .......... .......... .......... .......... 73% 13.2M 12s
395750K .......... .......... .......... .......... .......... 73% 15.7M 12s
395800K .......... .......... .......... .......... .......... 73% 31.4M 12s
395850K .......... .......... .......... .......... .......... 73% 18.5M 12s
395900K .......... .......... .......... .......... .......... 73% 26.7M 12s
395950K .......... .......... .......... .......... .......... 73% 17.7M 12s
396000K .......... .......... .......... .......... .......... 73% 19.8M 12s
396050K .......... .......... .......... .......... .......... 73% 25.1M 12s
396100K .......... .......... .......... .......... .......... 73% 18.4M 12s
396150K .......... .......... .......... .......... .......... 73% 23.0M 12s
396200K .......... .......... .......... .......... .......... 73% 16.8M 12s
396250K .......... .......... .......... .......... .......... 73% 23.1M 12s
396300K .......... .......... .......... .......... .......... 73% 28.0M 12s
396350K .......... .......... .......... .......... .......... 73% 32.8M 12s
396400K .......... .......... .......... .......... .......... 73% 26.7M 12s
396450K .......... .......... .......... .......... .......... 73% 82.3M 12s
396500K .......... .......... .......... .......... .......... 73% 36.8M 12s
396550K .......... .......... .......... .......... .......... 73% 65.6M 12s
396600K .......... .......... .......... .......... .......... 73% 17.6M 12s
396650K .......... .......... .......... .......... .......... 73% 53.8M 12s
396700K .......... .......... .......... .......... .......... 73% 28.4M 12s
396750K .......... .......... .......... .......... .......... 73% 61.5M 12s
396800K .......... .......... .......... .......... .......... 73% 34.5M 12s
396850K .......... .......... .......... .......... .......... 73% 22.1M 12s
396900K .......... .......... .......... .......... .......... 73% 36.8M 12s
396950K .......... .......... .......... .......... .......... 73% 27.8M 12s
397000K .......... .......... .......... .......... .......... 73% 25.4M 12s
397050K .......... .......... .......... .......... .......... 73% 25.6M 12s
397100K .......... .......... .......... .......... .......... 73% 26.4M 12s
397150K .......... .......... .......... .......... .......... 73% 20.2M 12s
397200K .......... .......... .......... .......... .......... 73% 36.9M 12s
397250K .......... .......... .......... .......... .......... 73% 21.1M 12s
397300K .......... .......... .......... .......... .......... 73% 28.3M 12s
397350K .......... .......... .......... .......... .......... 73% 17.9M 12s
397400K .......... .......... .......... .......... .......... 73% 31.7M 12s
397450K .......... .......... .......... .......... .......... 73% 26.2M 12s
397500K .......... .......... .......... .......... .......... 73% 27.0M 11s
397550K .......... .......... .......... .......... .......... 73% 17.2M 11s
397600K .......... .......... .......... .......... .......... 73% 36.0M 11s
397650K .......... .......... .......... .......... .......... 74% 35.7M 11s
397700K .......... .......... .......... .......... .......... 74% 26.2M 11s
397750K .......... .......... .......... .......... .......... 74% 34.0M 11s
397800K .......... .......... .......... .......... .......... 74% 85.8M 11s
397850K .......... .......... .......... .......... .......... 74% 21.1M 11s
397900K .......... .......... .......... .......... .......... 74% 44.0M 11s
397950K .......... .......... .......... .......... .......... 74% 93.9M 11s
398000K .......... .......... .......... .......... .......... 74% 26.2M 11s
398050K .......... .......... .......... .......... .......... 74% 63.3M 11s
398100K .......... .......... .......... .......... .......... 74% 39.2M 11s
398150K .......... .......... .......... .......... .......... 74%  112M 11s
398200K .......... .......... .......... .......... .......... 74% 27.2M 11s
398250K .......... .......... .......... .......... .......... 74% 34.3M 11s
398300K .......... .......... .......... .......... .......... 74% 34.1M 11s
398350K .......... .......... .......... .......... .......... 74% 33.5M 11s
398400K .......... .......... .......... .......... .......... 74% 36.4M 11s
398450K .......... .......... .......... .......... .......... 74% 32.0M 11s
398500K .......... .......... .......... .......... .......... 74% 42.2M 11s
398550K .......... .......... .......... .......... .......... 74% 42.1M 11s
398600K .......... .......... .......... .......... .......... 74% 23.7M 11s
398650K .......... .......... .......... .......... .......... 74% 35.1M 11s
398700K .......... .......... .......... .......... .......... 74% 38.5M 11s
398750K .......... .......... .......... .......... .......... 74% 19.1M 11s
398800K .......... .......... .......... .......... .......... 74% 28.5M 11s
398850K .......... .......... .......... .......... .......... 74% 38.1M 11s
398900K .......... .......... .......... .......... .......... 74% 38.6M 11s
398950K .......... .......... .......... .......... .......... 74% 34.0M 11s
399000K .......... .......... .......... .......... .......... 74% 33.5M 11s
399050K .......... .......... .......... .......... .......... 74% 42.2M 11s
399100K .......... .......... .......... .......... .......... 74% 29.2M 11s
399150K .......... .......... .......... .......... .......... 74% 41.5M 11s
399200K .......... .......... .......... .......... .......... 74% 24.5M 11s
399250K .......... .......... .......... .......... .......... 74% 45.9M 11s
399300K .......... .......... .......... .......... .......... 74% 39.3M 11s
399350K .......... .......... .......... .......... .......... 74% 36.1M 11s
399400K .......... .......... .......... .......... .......... 74% 36.2M 11s
399450K .......... .......... .......... .......... .......... 74% 26.5M 11s
399500K .......... .......... .......... .......... .......... 74% 83.6M 11s
399550K .......... .......... .......... .......... .......... 74% 27.9M 11s
399600K .......... .......... .......... .......... .......... 74% 88.9M 11s
399650K .......... .......... .......... .......... .......... 74% 13.7M 11s
399700K .......... .......... .......... .......... .......... 74% 66.9M 11s
399750K .......... .......... .......... .......... .......... 74%  145M 11s
399800K .......... .......... .......... .......... .......... 74% 24.8M 11s
399850K .......... .......... .......... .......... .......... 74%  114M 11s
399900K .......... .......... .......... .......... .......... 74% 32.6M 11s
399950K .......... .......... .......... .......... .......... 74% 33.2M 11s
400000K .......... .......... .......... .......... .......... 74% 34.9M 11s
400050K .......... .......... .......... .......... .......... 74% 27.8M 11s
400100K .......... .......... .......... .......... .......... 74% 31.7M 11s
400150K .......... .......... .......... .......... .......... 74% 6.92M 11s
400200K .......... .......... .......... .......... .......... 74% 19.8M 11s
400250K .......... .......... .......... .......... .......... 74% 36.1M 11s
400300K .......... .......... .......... .......... .......... 74% 34.4M 11s
400350K .......... .......... .......... .......... .......... 74% 26.5M 11s
400400K .......... .......... .......... .......... .......... 74% 32.9M 11s
400450K .......... .......... .......... .......... .......... 74% 29.8M 11s
400500K .......... .......... .......... .......... .......... 74% 46.7M 11s
400550K .......... .......... .......... .......... .......... 74% 32.9M 11s
400600K .......... .......... .......... .......... .......... 74% 27.7M 11s
400650K .......... .......... .......... .......... .......... 74% 44.5M 11s
400700K .......... .......... .......... .......... .......... 74% 30.7M 11s
400750K .......... .......... .......... .......... .......... 74% 38.2M 11s
400800K .......... .......... .......... .......... .......... 74% 4.32M 11s
400850K .......... .......... .......... .......... .......... 74% 19.1M 11s
400900K .......... .......... .......... .......... .......... 74% 22.5M 11s
400950K .......... .......... .......... .......... .......... 74% 20.0M 11s
401000K .......... .......... .......... .......... .......... 74% 31.3M 11s
401050K .......... .......... .......... .......... .......... 74% 18.4M 11s
401100K .......... .......... .......... .......... .......... 74% 13.5M 11s
401150K .......... .......... .......... .......... .......... 74% 93.7M 11s
401200K .......... .......... .......... .......... .......... 74% 17.6M 11s
401250K .......... .......... .......... .......... .......... 74% 24.5M 11s
401300K .......... .......... .......... .......... .......... 74% 36.2M 11s
401350K .......... .......... .......... .......... .......... 74% 23.3M 11s
401400K .......... .......... .......... .......... .......... 74% 32.1M 11s
401450K .......... .......... .......... .......... .......... 74% 21.9M 11s
401500K .......... .......... .......... .......... .......... 74% 31.5M 11s
401550K .......... .......... .......... .......... .......... 74% 31.7M 11s
401600K .......... .......... .......... .......... .......... 74% 21.3M 11s
401650K .......... .......... .......... .......... .......... 74% 32.1M 11s
401700K .......... .......... .......... .......... .......... 74% 25.8M 11s
401750K .......... .......... .......... .......... .......... 74% 27.4M 11s
401800K .......... .......... .......... .......... .......... 74% 24.5M 11s
401850K .......... .......... .......... .......... .......... 74% 14.3M 11s
401900K .......... .......... .......... .......... .......... 74% 30.9M 11s
401950K .......... .......... .......... .......... .......... 74% 20.6M 11s
402000K .......... .......... .......... .......... .......... 74% 40.3M 11s
402050K .......... .......... .......... .......... .......... 74% 29.9M 11s
402100K .......... .......... .......... .......... .......... 74% 25.6M 11s
402150K .......... .......... .......... .......... .......... 74%  117M 11s
402200K .......... .......... .......... .......... .......... 74% 35.7M 11s
402250K .......... .......... .......... .......... .......... 74%  112M 11s
402300K .......... .......... .......... .......... .......... 74% 48.9M 11s
402350K .......... .......... .......... .......... .......... 74% 71.7M 11s
402400K .......... .......... .......... .......... .......... 74% 45.0M 11s
402450K .......... .......... .......... .......... .......... 74% 65.5M 11s
402500K .......... .......... .......... .......... .......... 74% 21.1M 11s
402550K .......... .......... .......... .......... .......... 74%  152M 11s
402600K .......... .......... .......... .......... .......... 74%  147M 11s
402650K .......... .......... .......... .......... .......... 74% 95.7M 11s
402700K .......... .......... .......... .......... .......... 74% 40.6M 11s
402750K .......... .......... .......... .......... .......... 74% 87.8M 11s
402800K .......... .......... .......... .......... .......... 74% 46.6M 11s
402850K .......... .......... .......... .......... .......... 74% 52.4M 11s
402900K .......... .......... .......... .......... .......... 74% 59.7M 11s
402950K .......... .......... .......... .......... .......... 74% 45.7M 11s
403000K .......... .......... .......... .......... .......... 75% 57.4M 11s
403050K .......... .......... .......... .......... .......... 75% 44.3M 11s
403100K .......... .......... .......... .......... .......... 75% 69.4M 11s
403150K .......... .......... .......... .......... .......... 75% 53.0M 11s
403200K .......... .......... .......... .......... .......... 75% 49.6M 11s
403250K .......... .......... .......... .......... .......... 75% 59.4M 11s
403300K .......... .......... .......... .......... .......... 75% 74.5M 11s
403350K .......... .......... .......... .......... .......... 75% 44.7M 11s
403400K .......... .......... .......... .......... .......... 75% 54.5M 11s
403450K .......... .......... .......... .......... .......... 75% 49.4M 11s
403500K .......... .......... .......... .......... .......... 75% 62.0M 11s
403550K .......... .......... .......... .......... .......... 75% 74.4M 11s
403600K .......... .......... .......... .......... .......... 75% 43.2M 11s
403650K .......... .......... .......... .......... .......... 75% 49.3M 11s
403700K .......... .......... .......... .......... .......... 75% 37.4M 11s
403750K .......... .......... .......... .......... .......... 75%  101M 11s
403800K .......... .......... .......... .......... .......... 75% 42.6M 11s
403850K .......... .......... .......... .......... .......... 75% 52.1M 11s
403900K .......... .......... .......... .......... .......... 75% 47.7M 11s
403950K .......... .......... .......... .......... .......... 75% 66.6M 11s
404000K .......... .......... .......... .......... .......... 75% 44.8M 11s
404050K .......... .......... .......... .......... .......... 75% 63.0M 11s
404100K .......... .......... .......... .......... .......... 75% 55.3M 11s
404150K .......... .......... .......... .......... .......... 75% 45.0M 11s
404200K .......... .......... .......... .......... .......... 75% 65.8M 11s
404250K .......... .......... .......... .......... .......... 75% 50.3M 11s
404300K .......... .......... .......... .......... .......... 75% 72.9M 11s
404350K .......... .......... .......... .......... .......... 75% 42.3M 11s
404400K .......... .......... .......... .......... .......... 75% 41.6M 11s
404450K .......... .......... .......... .......... .......... 75% 55.2M 11s
404500K .......... .......... .......... .......... .......... 75% 52.4M 11s
404550K .......... .......... .......... .......... .......... 75% 36.2M 11s
404600K .......... .......... .......... .......... .......... 75% 94.3M 11s
404650K .......... .......... .......... .......... .......... 75% 83.3M 11s
404700K .......... .......... .......... .......... .......... 75% 20.6M 11s
404750K .......... .......... .......... .......... .......... 75% 62.5M 11s
404800K .......... .......... .......... .......... .......... 75%  113M 11s
404850K .......... .......... .......... .......... .......... 75% 49.6M 11s
404900K .......... .......... .......... .......... .......... 75% 73.8M 11s
404950K .......... .......... .......... .......... .......... 75% 92.5M 11s
405000K .......... .......... .......... .......... .......... 75% 53.1M 11s
405050K .......... .......... .......... .......... .......... 75% 14.8M 11s
405100K .......... .......... .......... .......... .......... 75% 29.9M 11s
405150K .......... .......... .......... .......... .......... 75% 35.0M 11s
405200K .......... .......... .......... .......... .......... 75% 22.5M 11s
405250K .......... .......... .......... .......... .......... 75% 28.7M 11s
405300K .......... .......... .......... .......... .......... 75% 31.7M 11s
405350K .......... .......... .......... .......... .......... 75% 32.0M 11s
405400K .......... .......... .......... .......... .......... 75% 39.4M 11s
405450K .......... .......... .......... .......... .......... 75% 38.0M 11s
405500K .......... .......... .......... .......... .......... 75% 18.1M 11s
405550K .......... .......... .......... .......... .......... 75% 32.6M 11s
405600K .......... .......... .......... .......... .......... 75% 38.9M 11s
405650K .......... .......... .......... .......... .......... 75% 38.8M 11s
405700K .......... .......... .......... .......... .......... 75% 32.7M 11s
405750K .......... .......... .......... .......... .......... 75% 46.2M 11s
405800K .......... .......... .......... .......... .......... 75% 39.5M 11s
405850K .......... .......... .......... .......... .......... 75% 29.5M 11s
405900K .......... .......... .......... .......... .......... 75% 39.7M 11s
405950K .......... .......... .......... .......... .......... 75% 10.4M 11s
406000K .......... .......... .......... .......... .......... 75% 28.4M 11s
406050K .......... .......... .......... .......... .......... 75% 38.5M 11s
406100K .......... .......... .......... .......... .......... 75% 44.3M 11s
406150K .......... .......... .......... .......... .......... 75% 37.1M 11s
406200K .......... .......... .......... .......... .......... 75% 40.1M 11s
406250K .......... .......... .......... .......... .......... 75% 14.9M 11s
406300K .......... .......... .......... .......... .......... 75% 9.22M 11s
406350K .......... .......... .......... .......... .......... 75% 72.2M 11s
406400K .......... .......... .......... .......... .......... 75% 86.6M 11s
406450K .......... .......... .......... .......... .......... 75%  103M 11s
406500K .......... .......... .......... .......... .......... 75%  120M 11s
406550K .......... .......... .......... .......... .......... 75%  105M 11s
406600K .......... .......... .......... .......... .......... 75%  108M 11s
406650K .......... .......... .......... .......... .......... 75% 23.1M 11s
406700K .......... .......... .......... .......... .......... 75% 88.9M 11s
406750K .......... .......... .......... .......... .......... 75% 38.4M 11s
406800K .......... .......... .......... .......... .......... 75% 35.6M 11s
406850K .......... .......... .......... .......... .......... 75% 23.8M 11s
406900K .......... .......... .......... .......... .......... 75% 29.3M 11s
406950K .......... .......... .......... .......... .......... 75% 28.8M 11s
407000K .......... .......... .......... .......... .......... 75% 39.5M 11s
407050K .......... .......... .......... .......... .......... 75% 11.5M 11s
407100K .......... .......... .......... .......... .......... 75% 18.0M 11s
407150K .......... .......... .......... .......... .......... 75% 33.5M 11s
407200K .......... .......... .......... .......... .......... 75% 32.3M 11s
407250K .......... .......... .......... .......... .......... 75% 17.6M 11s
407300K .......... .......... .......... .......... .......... 75% 31.6M 11s
407350K .......... .......... .......... .......... .......... 75% 31.5M 11s
407400K .......... .......... .......... .......... .......... 75% 17.1M 11s
407450K .......... .......... .......... .......... .......... 75% 36.7M 11s
407500K .......... .......... .......... .......... .......... 75% 29.6M 11s
407550K .......... .......... .......... .......... .......... 75% 30.7M 11s
407600K .......... .......... .......... .......... .......... 75% 19.3M 10s
407650K .......... .......... .......... .......... .......... 75% 29.4M 10s
407700K .......... .......... .......... .......... .......... 75% 94.1M 10s
407750K .......... .......... .......... .......... .......... 75% 26.2M 10s
407800K .......... .......... .......... .......... .......... 75%  109M 10s
407850K .......... .......... .......... .......... .......... 75% 25.6M 10s
407900K .......... .......... .......... .......... .......... 75%  106M 10s
407950K .......... .......... .......... .......... .......... 75% 26.4M 10s
408000K .......... .......... .......... .......... .......... 75% 66.5M 10s
408050K .......... .......... .......... .......... .......... 75% 43.5M 10s
408100K .......... .......... .......... .......... .......... 75% 18.6M 10s
408150K .......... .......... .......... .......... .......... 75% 56.8M 10s
408200K .......... .......... .......... .......... .......... 75% 49.6M 10s
408250K .......... .......... .......... .......... .......... 75% 84.0M 10s
408300K .......... .......... .......... .......... .......... 75% 51.2M 10s
408350K .......... .......... .......... .......... .......... 75% 73.0M 10s
408400K .......... .......... .......... .......... .......... 76% 37.8M 10s
408450K .......... .......... .......... .......... .......... 76% 28.9M 10s
408500K .......... .......... .......... .......... .......... 76% 35.1M 10s
408550K .......... .......... .......... .......... .......... 76% 35.1M 10s
408600K .......... .......... .......... .......... .......... 76% 33.0M 10s
408650K .......... .......... .......... .......... .......... 76% 27.9M 10s
408700K .......... .......... .......... .......... .......... 76% 28.9M 10s
408750K .......... .......... .......... .......... .......... 76% 42.7M 10s
408800K .......... .......... .......... .......... .......... 76% 31.1M 10s
408850K .......... .......... .......... .......... .......... 76% 32.8M 10s
408900K .......... .......... .......... .......... .......... 76% 43.9M 10s
408950K .......... .......... .......... .......... .......... 76% 21.3M 10s
409000K .......... .......... .......... .......... .......... 76% 31.4M 10s
409050K .......... .......... .......... .......... .......... 76% 27.7M 10s
409100K .......... .......... .......... .......... .......... 76% 19.7M 10s
409150K .......... .......... .......... .......... .......... 76% 31.1M 10s
409200K .......... .......... .......... .......... .......... 76% 29.3M 10s
409250K .......... .......... .......... .......... .......... 76% 28.7M 10s
409300K .......... .......... .......... .......... .......... 76% 19.1M 10s
409350K .......... .......... .......... .......... .......... 76% 35.3M 10s
409400K .......... .......... .......... .......... .......... 76% 23.5M 10s
409450K .......... .......... .......... .......... .......... 76% 36.3M 10s
409500K .......... .......... .......... .......... .......... 76% 62.1M 10s
409550K .......... .......... .......... .......... .......... 76% 39.7M 10s
409600K .......... .......... .......... .......... .......... 76% 52.7M 10s
409650K .......... .......... .......... .......... .......... 76% 34.8M 10s
409700K .......... .......... .......... .......... .......... 76% 18.7M 10s
409750K .......... .......... .......... .......... .......... 76%  125M 10s
409800K .......... .......... .......... .......... .......... 76% 28.4M 10s
409850K .......... .......... .......... .......... .......... 76% 73.2M 10s
409900K .......... .......... .......... .......... .......... 76% 28.3M 10s
409950K .......... .......... .......... .......... .......... 76% 94.6M 10s
410000K .......... .......... .......... .......... .......... 76% 30.4M 10s
410050K .......... .......... .......... .......... .......... 76% 34.0M 10s
410100K .......... .......... .......... .......... .......... 76% 40.2M 10s
410150K .......... .......... .......... .......... .......... 76% 26.5M 10s
410200K .......... .......... .......... .......... .......... 76% 33.3M 10s
410250K .......... .......... .......... .......... .......... 76% 39.4M 10s
410300K .......... .......... .......... .......... .......... 76% 39.0M 10s
410350K .......... .......... .......... .......... .......... 76% 25.5M 10s
410400K .......... .......... .......... .......... .......... 76% 40.1M 10s
410450K .......... .......... .......... .......... .......... 76% 36.5M 10s
410500K .......... .......... .......... .......... .......... 76% 36.2M 10s
410550K .......... .......... .......... .......... .......... 76% 38.5M 10s
410600K .......... .......... .......... .......... .......... 76% 29.7M 10s
410650K .......... .......... .......... .......... .......... 76% 43.1M 10s
410700K .......... .......... .......... .......... .......... 76% 30.0M 10s
410750K .......... .......... .......... .......... .......... 76% 38.5M 10s
410800K .......... .......... .......... .......... .......... 76% 31.5M 10s
410850K .......... .......... .......... .......... .......... 76% 36.5M 10s
410900K .......... .......... .......... .......... .......... 76% 29.3M 10s
410950K .......... .......... .......... .......... .......... 76% 28.5M 10s
411000K .......... .......... .......... .......... .......... 76% 22.2M 10s
411050K .......... .......... .......... .......... .......... 76% 39.4M 10s
411100K .......... .......... .......... .......... .......... 76% 22.6M 10s
411150K .......... .......... .......... .......... .......... 76% 29.5M 10s
411200K .......... .......... .......... .......... .......... 76% 14.7M 10s
411250K .......... .......... .......... .......... .......... 76% 19.1M 10s
411300K .......... .......... .......... .......... .......... 76% 15.2M 10s
411350K .......... .......... .......... .......... .......... 76% 16.5M 10s
411400K .......... .......... .......... .......... .......... 76% 19.2M 10s
411450K .......... .......... .......... .......... .......... 76% 19.9M 10s
411500K .......... .......... .......... .......... .......... 76% 21.1M 10s
411550K .......... .......... .......... .......... .......... 76% 26.8M 10s
411600K .......... .......... .......... .......... .......... 76% 7.72M 10s
411650K .......... .......... .......... .......... .......... 76% 31.1M 10s
411700K .......... .......... .......... .......... .......... 76% 13.6M 10s
411750K .......... .......... .......... .......... .......... 76% 32.0M 10s
411800K .......... .......... .......... .......... .......... 76% 23.0M 10s
411850K .......... .......... .......... .......... .......... 76% 20.6M 10s
411900K .......... .......... .......... .......... .......... 76% 17.6M 10s
411950K .......... .......... .......... .......... .......... 76% 22.2M 10s
412000K .......... .......... .......... .......... .......... 76% 21.1M 10s
412050K .......... .......... .......... .......... .......... 76% 24.1M 10s
412100K .......... .......... .......... .......... .......... 76% 19.5M 10s
412150K .......... .......... .......... .......... .......... 76% 26.3M 10s
412200K .......... .......... .......... .......... .......... 76% 9.46M 10s
412250K .......... .......... .......... .......... .......... 76%  104M 10s
412300K .......... .......... .......... .......... .......... 76%  140M 10s
412350K .......... .......... .......... .......... .......... 76% 29.1M 10s
412400K .......... .......... .......... .......... .......... 76% 24.7M 10s
412450K .......... .......... .......... .......... .......... 76% 22.5M 10s
412500K .......... .......... .......... .......... .......... 76% 18.2M 10s
412550K .......... .......... .......... .......... .......... 76% 47.3M 10s
412600K .......... .......... .......... .......... .......... 76% 19.6M 10s
412650K .......... .......... .......... .......... .......... 76% 25.9M 10s
412700K .......... .......... .......... .......... .......... 76% 18.6M 10s
412750K .......... .......... .......... .......... .......... 76% 20.2M 10s
412800K .......... .......... .......... .......... .......... 76% 21.6M 10s
412850K .......... .......... .......... .......... .......... 76% 18.5M 10s
412900K .......... .......... .......... .......... .......... 76% 28.1M 10s
412950K .......... .......... .......... .......... .......... 76% 18.5M 10s
413000K .......... .......... .......... .......... .......... 76% 29.7M 10s
413050K .......... .......... .......... .......... .......... 76% 21.6M 10s
413100K .......... .......... .......... .......... .......... 76% 18.5M 10s
413150K .......... .......... .......... .......... .......... 76% 34.1M 10s
413200K .......... .......... .......... .......... .......... 76% 18.8M 10s
413250K .......... .......... .......... .......... .......... 76% 20.7M 10s
413300K .......... .......... .......... .......... .......... 76% 25.1M 10s
413350K .......... .......... .......... .......... .......... 76% 32.6M 10s
413400K .......... .......... .......... .......... .......... 76% 37.0M 10s
413450K .......... .......... .......... .......... .......... 76% 43.9M 10s
413500K .......... .......... .......... .......... .......... 76% 71.2M 10s
413550K .......... .......... .......... .......... .......... 76% 41.8M 10s
413600K .......... .......... .......... .......... .......... 76% 76.4M 10s
413650K .......... .......... .......... .......... .......... 76% 41.2M 10s
413700K .......... .......... .......... .......... .......... 76% 59.9M 10s
413750K .......... .......... .......... .......... .......... 77% 21.6M 10s
413800K .......... .......... .......... .......... .......... 77% 97.9M 10s
413850K .......... .......... .......... .......... .......... 77% 45.5M 10s
413900K .......... .......... .......... .......... .......... 77%  123M 10s
413950K .......... .......... .......... .......... .......... 77% 53.4M 10s
414000K .......... .......... .......... .......... .......... 77% 50.4M 10s
414050K .......... .......... .......... .......... .......... 77% 44.6M 10s
414100K .......... .......... .......... .......... .......... 77% 37.7M 10s
414150K .......... .......... .......... .......... .......... 77% 43.6M 10s
414200K .......... .......... .......... .......... .......... 77% 32.3M 10s
414250K .......... .......... .......... .......... .......... 77% 40.4M 10s
414300K .......... .......... .......... .......... .......... 77% 36.4M 10s
414350K .......... .......... .......... .......... .......... 77% 42.7M 10s
414400K .......... .......... .......... .......... .......... 77% 32.4M 10s
414450K .......... .......... .......... .......... .......... 77% 32.5M 10s
414500K .......... .......... .......... .......... .......... 77% 96.5M 10s
414550K .......... .......... .......... .......... .......... 77% 40.7M 10s
414600K .......... .......... .......... .......... .......... 77% 40.0M 10s
414650K .......... .......... .......... .......... .......... 77% 44.3M 10s
414700K .......... .......... .......... .......... .......... 77% 39.2M 10s
414750K .......... .......... .......... .......... .......... 77% 39.1M 10s
414800K .......... .......... .......... .......... .......... 77% 35.1M 10s
414850K .......... .......... .......... .......... .......... 77% 37.0M 10s
414900K .......... .......... .......... .......... .......... 77% 40.2M 10s
414950K .......... .......... .......... .......... .......... 77% 38.4M 10s
415000K .......... .......... .......... .......... .......... 77% 38.0M 10s
415050K .......... .......... .......... .......... .......... 77% 46.1M 10s
415100K .......... .......... .......... .......... .......... 77% 52.7M 10s
415150K .......... .......... .......... .......... .......... 77% 35.8M 10s
415200K .......... .......... .......... .......... .......... 77% 40.4M 10s
415250K .......... .......... .......... .......... .......... 77% 63.7M 10s
415300K .......... .......... .......... .......... .......... 77% 34.7M 10s
415350K .......... .......... .......... .......... .......... 77% 38.1M 10s
415400K .......... .......... .......... .......... .......... 77% 27.0M 10s
415450K .......... .......... .......... .......... .......... 77% 27.9M 10s
415500K .......... .......... .......... .......... .......... 77% 14.9M 10s
415550K .......... .......... .......... .......... .......... 77%  119M 10s
415600K .......... .......... .......... .......... .......... 77% 92.1M 10s
415650K .......... .......... .......... .......... .......... 77% 36.3M 10s
415700K .......... .......... .......... .......... .......... 77%  104M 10s
415750K .......... .......... .......... .......... .......... 77% 34.0M 10s
415800K .......... .......... .......... .......... .......... 77% 73.9M 10s
415850K .......... .......... .......... .......... .......... 77% 34.2M 10s
415900K .......... .......... .......... .......... .......... 77% 28.0M 10s
415950K .......... .......... .......... .......... .......... 77% 31.1M 10s
416000K .......... .......... .......... .......... .......... 77% 30.3M 10s
416050K .......... .......... .......... .......... .......... 77% 38.0M 10s
416100K .......... .......... .......... .......... .......... 77% 30.7M 10s
416150K .......... .......... .......... .......... .......... 77% 35.7M 10s
416200K .......... .......... .......... .......... .......... 77% 30.6M 10s
416250K .......... .......... .......... .......... .......... 77% 24.9M 10s
416300K .......... .......... .......... .......... .......... 77% 38.4M 10s
416350K .......... .......... .......... .......... .......... 77% 36.3M 10s
416400K .......... .......... .......... .......... .......... 77% 35.5M 10s
416450K .......... .......... .......... .......... .......... 77% 29.3M 10s
416500K .......... .......... .......... .......... .......... 77% 31.5M 10s
416550K .......... .......... .......... .......... .......... 77% 37.9M 10s
416600K .......... .......... .......... .......... .......... 77% 38.5M 10s
416650K .......... .......... .......... .......... .......... 77% 38.1M 10s
416700K .......... .......... .......... .......... .......... 77% 28.8M 10s
416750K .......... .......... .......... .......... .......... 77% 41.7M 10s
416800K .......... .......... .......... .......... .......... 77% 37.0M 10s
416850K .......... .......... .......... .......... .......... 77% 31.6M 10s
416900K .......... .......... .......... .......... .......... 77% 31.9M 10s
416950K .......... .......... .......... .......... .......... 77% 32.8M 10s
417000K .......... .......... .......... .......... .......... 77% 11.9M 10s
417050K .......... .......... .......... .......... .......... 77% 19.0M 10s
417100K .......... .......... .......... .......... .......... 77% 26.8M 10s
417150K .......... .......... .......... .......... .......... 77% 13.6M 10s
417200K .......... .......... .......... .......... .......... 77% 4.88M 10s
417250K .......... .......... .......... .......... .......... 77% 91.3M 10s
417300K .......... .......... .......... .......... .......... 77% 74.9M 10s
417350K .......... .......... .......... .......... .......... 77% 70.9M 10s
417400K .......... .......... .......... .......... .......... 77%  130M 10s
417450K .......... .......... .......... .......... .......... 77%  122M 10s
417500K .......... .......... .......... .......... .......... 77% 82.5M 10s
417550K .......... .......... .......... .......... .......... 77% 31.0M 10s
417600K .......... .......... .......... .......... .......... 77% 25.7M 10s
417650K .......... .......... .......... .......... .......... 77% 25.6M 10s
417700K .......... .......... .......... .......... .......... 77% 26.8M 10s
417750K .......... .......... .......... .......... .......... 77% 30.3M 10s
417800K .......... .......... .......... .......... .......... 77% 21.5M 10s
417850K .......... .......... .......... .......... .......... 77% 33.0M 10s
417900K .......... .......... .......... .......... .......... 77% 38.2M 10s
417950K .......... .......... .......... .......... .......... 77% 21.5M 10s
418000K .......... .......... .......... .......... .......... 77% 28.9M 10s
418050K .......... .......... .......... .......... .......... 77% 13.1M 10s
418100K .......... .......... .......... .......... .......... 77% 33.8M 10s
418150K .......... .......... .......... .......... .......... 77% 22.5M 10s
418200K .......... .......... .......... .......... .......... 77% 27.2M 9s
418250K .......... .......... .......... .......... .......... 77% 25.9M 9s
418300K .......... .......... .......... .......... .......... 77% 3.76M 9s
418350K .......... .......... .......... .......... .......... 77% 24.4M 9s
418400K .......... .......... .......... .......... .......... 77% 90.6M 9s
418450K .......... .......... .......... .......... .......... 77% 17.0M 9s
418500K .......... .......... .......... .......... .......... 77% 93.7M 9s
418550K .......... .......... .......... .......... .......... 77% 23.3M 9s
418600K .......... .......... .......... .......... .......... 77% 27.9M 9s
418650K .......... .......... .......... .......... .......... 77% 41.5M 9s
418700K .......... .......... .......... .......... .......... 77% 27.9M 9s
418750K .......... .......... .......... .......... .......... 77% 30.7M 9s
418800K .......... .......... .......... .......... .......... 77% 27.5M 9s
418850K .......... .......... .......... .......... .......... 77% 25.6M 9s
418900K .......... .......... .......... .......... .......... 77% 30.9M 9s
418950K .......... .......... .......... .......... .......... 77% 28.9M 9s
419000K .......... .......... .......... .......... .......... 77% 33.7M 9s
419050K .......... .......... .......... .......... .......... 77% 34.3M 9s
419100K .......... .......... .......... .......... .......... 77% 23.8M 9s
419150K .......... .......... .......... .......... .......... 78% 34.1M 9s
419200K .......... .......... .......... .......... .......... 78% 27.9M 9s
419250K .......... .......... .......... .......... .......... 78% 36.7M 9s
419300K .......... .......... .......... .......... .......... 78% 37.2M 9s
419350K .......... .......... .......... .......... .......... 78% 27.5M 9s
419400K .......... .......... .......... .......... .......... 78% 37.2M 9s
419450K .......... .......... .......... .......... .......... 78% 36.0M 9s
419500K .......... .......... .......... .......... .......... 78% 21.3M 9s
419550K .......... .......... .......... .......... .......... 78% 34.1M 9s
419600K .......... .......... .......... .......... .......... 78% 35.3M 9s
419650K .......... .......... .......... .......... .......... 78% 42.8M 9s
419700K .......... .......... .......... .......... .......... 78% 54.2M 9s
419750K .......... .......... .......... .......... .......... 78% 79.0M 9s
419800K .......... .......... .......... .......... .......... 78% 57.1M 9s
419850K .......... .......... .......... .......... .......... 78% 21.0M 9s
419900K .......... .......... .......... .......... .......... 78%  117M 9s
419950K .......... .......... .......... .......... .......... 78% 99.6M 9s
420000K .......... .......... .......... .......... .......... 78% 36.9M 9s
420050K .......... .......... .......... .......... .......... 78% 67.2M 9s
420100K .......... .......... .......... .......... .......... 78%  140M 9s
420150K .......... .......... .......... .......... .......... 78% 46.5M 9s
420200K .......... .......... .......... .......... .......... 78% 43.1M 9s
420250K .......... .......... .......... .......... .......... 78% 30.1M 9s
420300K .......... .......... .......... .......... .......... 78% 47.9M 9s
420350K .......... .......... .......... .......... .......... 78% 38.1M 9s
420400K .......... .......... .......... .......... .......... 78% 52.1M 9s
420450K .......... .......... .......... .......... .......... 78% 35.3M 9s
420500K .......... .......... .......... .......... .......... 78% 36.3M 9s
420550K .......... .......... .......... .......... .......... 78% 36.1M 9s
420600K .......... .......... .......... .......... .......... 78% 36.5M 9s
420650K .......... .......... .......... .......... .......... 78% 39.3M 9s
420700K .......... .......... .......... .......... .......... 78% 36.3M 9s
420750K .......... .......... .......... .......... .......... 78% 56.6M 9s
420800K .......... .......... .......... .......... .......... 78% 52.4M 9s
420850K .......... .......... .......... .......... .......... 78% 36.4M 9s
420900K .......... .......... .......... .......... .......... 78% 57.9M 9s
420950K .......... .......... .......... .......... .......... 78% 33.3M 9s
421000K .......... .......... .......... .......... .......... 78% 58.0M 9s
421050K .......... .......... .......... .......... .......... 78% 56.7M 9s
421100K .......... .......... .......... .......... .......... 78% 35.2M 9s
421150K .......... .......... .......... .......... .......... 78% 35.7M 9s
421200K .......... .......... .......... .......... .......... 78% 36.9M 9s
421250K .......... .......... .......... .......... .......... 78% 51.1M 9s
421300K .......... .......... .......... .......... .......... 78% 33.5M 9s
421350K .......... .......... .......... .......... .......... 78% 30.1M 9s
421400K .......... .......... .......... .......... .......... 78% 38.8M 9s
421450K .......... .......... .......... .......... .......... 78% 42.9M 9s
421500K .......... .......... .......... .......... .......... 78% 49.1M 9s
421550K .......... .......... .......... .......... .......... 78% 34.5M 9s
421600K .......... .......... .......... .......... .......... 78% 59.0M 9s
421650K .......... .......... .......... .......... .......... 78% 44.7M 9s
421700K .......... .......... .......... .......... .......... 78% 25.1M 9s
421750K .......... .......... .......... .......... .......... 78% 97.9M 9s
421800K .......... .......... .......... .......... .......... 78% 19.1M 9s
421850K .......... .......... .......... .......... .......... 78% 75.8M 9s
421900K .......... .......... .......... .......... .......... 78% 76.3M 9s
421950K .......... .......... .......... .......... .......... 78% 45.3M 9s
422000K .......... .......... .......... .......... .......... 78% 66.0M 9s
422050K .......... .......... .......... .......... .......... 78%  132M 9s
422100K .......... .......... .......... .......... .......... 78% 82.2M 9s
422150K .......... .......... .......... .......... .......... 78% 37.6M 9s
422200K .......... .......... .......... .......... .......... 78% 31.8M 9s
422250K .......... .......... .......... .......... .......... 78% 24.8M 9s
422300K .......... .......... .......... .......... .......... 78% 20.8M 9s
422350K .......... .......... .......... .......... .......... 78% 34.5M 9s
422400K .......... .......... .......... .......... .......... 78% 36.1M 9s
422450K .......... .......... .......... .......... .......... 78% 31.7M 9s
422500K .......... .......... .......... .......... .......... 78% 36.4M 9s
422550K .......... .......... .......... .......... .......... 78% 39.3M 9s
422600K .......... .......... .......... .......... .......... 78% 6.69M 9s
422650K .......... .......... .......... .......... .......... 78% 34.1M 9s
422700K .......... .......... .......... .......... .......... 78% 24.4M 9s
422750K .......... .......... .......... .......... .......... 78% 36.2M 9s
422800K .......... .......... .......... .......... .......... 78% 39.5M 9s
422850K .......... .......... .......... .......... .......... 78% 36.3M 9s
422900K .......... .......... .......... .......... .......... 78% 33.5M 9s
422950K .......... .......... .......... .......... .......... 78% 14.2M 9s
423000K .......... .......... .......... .......... .......... 78% 38.4M 9s
423050K .......... .......... .......... .......... .......... 78% 35.2M 9s
423100K .......... .......... .......... .......... .......... 78% 33.0M 9s
423150K .......... .......... .......... .......... .......... 78% 84.5M 9s
423200K .......... .......... .......... .......... .......... 78% 25.4M 9s
423250K .......... .......... .......... .......... .......... 78% 15.3M 9s
423300K .......... .......... .......... .......... .......... 78% 66.9M 9s
423350K .......... .......... .......... .......... .......... 78% 78.5M 9s
423400K .......... .......... .......... .......... .......... 78% 50.5M 9s
423450K .......... .......... .......... .......... .......... 78% 39.5M 9s
423500K .......... .......... .......... .......... .......... 78% 23.4M 9s
423550K .......... .......... .......... .......... .......... 78% 71.2M 9s
423600K .......... .......... .......... .......... .......... 78% 20.5M 9s
423650K .......... .......... .......... .......... .......... 78% 24.5M 9s
423700K .......... .......... .......... .......... .......... 78% 24.3M 9s
423750K .......... .......... .......... .......... .......... 78% 26.6M 9s
423800K .......... .......... .......... .......... .......... 78% 20.8M 9s
423850K .......... .......... .......... .......... .......... 78% 29.4M 9s
423900K .......... .......... .......... .......... .......... 78% 27.8M 9s
423950K .......... .......... .......... .......... .......... 78% 22.7M 9s
424000K .......... .......... .......... .......... .......... 78% 25.5M 9s
424050K .......... .......... .......... .......... .......... 78% 23.3M 9s
424100K .......... .......... .......... .......... .......... 78% 21.8M 9s
424150K .......... .......... .......... .......... .......... 78% 21.6M 9s
424200K .......... .......... .......... .......... .......... 78% 24.3M 9s
424250K .......... .......... .......... .......... .......... 78% 20.4M 9s
424300K .......... .......... .......... .......... .......... 78% 27.2M 9s
424350K .......... .......... .......... .......... .......... 78% 21.4M 9s
424400K .......... .......... .......... .......... .......... 78% 28.8M 9s
424450K .......... .......... .......... .......... .......... 78% 33.5M 9s
424500K .......... .......... .......... .......... .......... 79% 28.0M 9s
424550K .......... .......... .......... .......... .......... 79%  117M 9s
424600K .......... .......... .......... .......... .......... 79% 23.1M 9s
424650K .......... .......... .......... .......... .......... 79% 27.2M 9s
424700K .......... .......... .......... .......... .......... 79% 92.7M 9s
424750K .......... .......... .......... .......... .......... 79% 27.4M 9s
424800K .......... .......... .......... .......... .......... 79%  108M 9s
424850K .......... .......... .......... .......... .......... 79% 15.1M 9s
424900K .......... .......... .......... .......... .......... 79%  111M 9s
424950K .......... .......... .......... .......... .......... 79%  119M 9s
425000K .......... .......... .......... .......... .......... 79% 33.1M 9s
425050K .......... .......... .......... .......... .......... 79% 64.2M 9s
425100K .......... .......... .......... .......... .......... 79% 34.1M 9s
425150K .......... .......... .......... .......... .......... 79% 38.3M 9s
425200K .......... .......... .......... .......... .......... 79% 29.5M 9s
425250K .......... .......... .......... .......... .......... 79% 32.0M 9s
425300K .......... .......... .......... .......... .......... 79% 29.2M 9s
425350K .......... .......... .......... .......... .......... 79% 28.9M 9s
425400K .......... .......... .......... .......... .......... 79% 38.2M 9s
425450K .......... .......... .......... .......... .......... 79% 35.7M 9s
425500K .......... .......... .......... .......... .......... 79% 39.4M 9s
425550K .......... .......... .......... .......... .......... 79% 32.2M 9s
425600K .......... .......... .......... .......... .......... 79% 29.2M 9s
425650K .......... .......... .......... .......... .......... 79% 32.0M 9s
425700K .......... .......... .......... .......... .......... 79% 38.8M 9s
425750K .......... .......... .......... .......... .......... 79% 30.0M 9s
425800K .......... .......... .......... .......... .......... 79% 30.9M 9s
425850K .......... .......... .......... .......... .......... 79% 32.1M 9s
425900K .......... .......... .......... .......... .......... 79% 38.6M 9s
425950K .......... .......... .......... .......... .......... 79% 26.8M 9s
426000K .......... .......... .......... .......... .......... 79% 39.7M 9s
426050K .......... .......... .......... .......... .......... 79% 37.9M 9s
426100K .......... .......... .......... .......... .......... 79% 32.9M 9s
426150K .......... .......... .......... .......... .......... 79% 32.9M 9s
426200K .......... .......... .......... .......... .......... 79% 35.1M 9s
426250K .......... .......... .......... .......... .......... 79% 31.0M 9s
426300K .......... .......... .......... .......... .......... 79% 34.0M 9s
426350K .......... .......... .......... .......... .......... 79% 86.6M 9s
426400K .......... .......... .......... .......... .......... 79% 34.2M 9s
426450K .......... .......... .......... .......... .......... 79% 17.3M 9s
426500K .......... .......... .......... .......... .......... 79%  104M 9s
426550K .......... .......... .......... .......... .......... 79%  108M 9s
426600K .......... .......... .......... .......... .......... 79% 27.1M 9s
426650K .......... .......... .......... .......... .......... 79%  120M 9s
426700K .......... .......... .......... .......... .......... 79% 95.4M 9s
426750K .......... .......... .......... .......... .......... 79% 81.5M 9s
426800K .......... .......... .......... .......... .......... 79% 81.0M 9s
426850K .......... .......... .......... .......... .......... 79% 86.0M 9s
426900K .......... .......... .......... .......... .......... 79% 42.9M 9s
426950K .......... .......... .......... .......... .......... 79% 29.0M 9s
427000K .......... .......... .......... .......... .......... 79% 41.8M 9s
427050K .......... .......... .......... .......... .......... 79% 19.9M 9s
427100K .......... .......... .......... .......... .......... 79% 30.8M 9s
427150K .......... .......... .......... .......... .......... 79% 36.7M 9s
427200K .......... .......... .......... .......... .......... 79% 24.8M 9s
427250K .......... .......... .......... .......... .......... 79% 35.9M 9s
427300K .......... .......... .......... .......... .......... 79% 38.8M 9s
427350K .......... .......... .......... .......... .......... 79% 32.2M 9s
427400K .......... .......... .......... .......... .......... 79% 27.9M 9s
427450K .......... .......... .......... .......... .......... 79% 26.5M 9s
427500K .......... .......... .......... .......... .......... 79% 38.0M 9s
427550K .......... .......... .......... .......... .......... 79% 37.3M 9s
427600K .......... .......... .......... .......... .......... 79% 23.8M 9s
427650K .......... .......... .......... .......... .......... 79% 34.6M 9s
427700K .......... .......... .......... .......... .......... 79% 35.1M 9s
427750K .......... .......... .......... .......... .......... 79% 20.5M 9s
427800K .......... .......... .......... .......... .......... 79% 39.2M 9s
427850K .......... .......... .......... .......... .......... 79% 40.1M 9s
427900K .......... .......... .......... .......... .......... 79% 20.9M 9s
427950K .......... .......... .......... .......... .......... 79% 35.4M 9s
428000K .......... .......... .......... .......... .......... 79% 37.4M 9s
428050K .......... .......... .......... .......... .......... 79% 72.8M 9s
428100K .......... .......... .......... .......... .......... 79% 43.8M 9s
428150K .......... .......... .......... .......... .......... 79% 92.1M 9s
428200K .......... .......... .......... .......... .......... 79% 59.8M 9s
428250K .......... .......... .......... .......... .......... 79% 98.6M 9s
428300K .......... .......... .......... .......... .......... 79% 63.8M 9s
428350K .......... .......... .......... .......... .......... 79% 48.2M 9s
428400K .......... .......... .......... .......... .......... 79% 99.9M 9s
428450K .......... .......... .......... .......... .......... 79% 22.1M 9s
428500K .......... .......... .......... .......... .......... 79%  115M 9s
428550K .......... .......... .......... .......... .......... 79% 85.5M 9s
428600K .......... .......... .......... .......... .......... 79% 55.4M 9s
428650K .......... .......... .......... .......... .......... 79%  115M 9s
428700K .......... .......... .......... .......... .......... 79% 78.6M 9s
428750K .......... .......... .......... .......... .......... 79% 92.3M 9s
428800K .......... .......... .......... .......... .......... 79%  111M 9s
428850K .......... .......... .......... .......... .......... 79%  126M 9s
428900K .......... .......... .......... .......... .......... 79% 69.6M 9s
428950K .......... .......... .......... .......... .......... 79% 63.3M 9s
429000K .......... .......... .......... .......... .......... 79% 58.5M 8s
429050K .......... .......... .......... .......... .......... 79% 43.6M 8s
429100K .......... .......... .......... .......... .......... 79% 52.6M 8s
429150K .......... .......... .......... .......... .......... 79% 40.3M 8s
429200K .......... .......... .......... .......... .......... 79% 42.8M 8s
429250K .......... .......... .......... .......... .......... 79% 98.8M 8s
429300K .......... .......... .......... .......... .......... 79% 33.9M 8s
429350K .......... .......... .......... .......... .......... 79% 34.8M 8s
429400K .......... .......... .......... .......... .......... 79%  102M 8s
429450K .......... .......... .......... .......... .......... 79% 47.0M 8s
429500K .......... .......... .......... .......... .......... 79% 39.6M 8s
429550K .......... .......... .......... .......... .......... 79% 87.3M 8s
429600K .......... .......... .......... .......... .......... 79% 47.3M 8s
429650K .......... .......... .......... .......... .......... 79% 51.2M 8s
429700K .......... .......... .......... .......... .......... 79% 67.0M 8s
429750K .......... .......... .......... .......... .......... 79% 42.7M 8s
429800K .......... .......... .......... .......... .......... 79% 64.2M 8s
429850K .......... .......... .......... .......... .......... 79% 54.5M 8s
429900K .......... .......... .......... .......... .......... 80% 36.8M 8s
429950K .......... .......... .......... .......... .......... 80% 48.3M 8s
430000K .......... .......... .......... .......... .......... 80% 88.5M 8s
430050K .......... .......... .......... .......... .......... 80% 50.3M 8s
430100K .......... .......... .......... .......... .......... 80% 42.7M 8s
430150K .......... .......... .......... .......... .......... 80% 77.5M 8s
430200K .......... .......... .......... .......... .......... 80% 44.7M 8s
430250K .......... .......... .......... .......... .......... 80% 89.1M 8s
430300K .......... .......... .......... .......... .......... 80% 56.2M 8s
430350K .......... .......... .......... .......... .......... 80% 44.2M 8s
430400K .......... .......... .......... .......... .......... 80% 44.6M 8s
430450K .......... .......... .......... .......... .......... 80% 71.5M 8s
430500K .......... .......... .......... .......... .......... 80% 44.8M 8s
430550K .......... .......... .......... .......... .......... 80% 59.7M 8s
430600K .......... .......... .......... .......... .......... 80% 66.2M 8s
430650K .......... .......... .......... .......... .......... 80% 53.8M 8s
430700K .......... .......... .......... .......... .......... 80% 40.6M 8s
430750K .......... .......... .......... .......... .......... 80% 52.5M 8s
430800K .......... .......... .......... .......... .......... 80%  107M 8s
430850K .......... .......... .......... .......... .......... 80% 36.7M 8s
430900K .......... .......... .......... .......... .......... 80% 78.9M 8s
430950K .......... .......... .......... .......... .......... 80% 41.7M 8s
431000K .......... .......... .......... .......... .......... 80% 98.4M 8s
431050K .......... .......... .......... .......... .......... 80% 16.2M 8s
431100K .......... .......... .......... .......... .......... 80%  109M 8s
431150K .......... .......... .......... .......... .......... 80%  114M 8s
431200K .......... .......... .......... .......... .......... 80%  121M 8s
431250K .......... .......... .......... .......... .......... 80% 44.1M 8s
431300K .......... .......... .......... .......... .......... 80%  106M 8s
431350K .......... .......... .......... .......... .......... 80% 88.8M 8s
431400K .......... .......... .......... .......... .......... 80% 81.8M 8s
431450K .......... .......... .......... .......... .......... 80% 40.7M 8s
431500K .......... .......... .......... .......... .......... 80% 63.8M 8s
431550K .......... .......... .......... .......... .......... 80% 60.0M 8s
431600K .......... .......... .......... .......... .......... 80% 36.8M 8s
431650K .......... .......... .......... .......... .......... 80% 39.9M 8s
431700K .......... .......... .......... .......... .......... 80% 40.1M 8s
431750K .......... .......... .......... .......... .......... 80% 93.0M 8s
431800K .......... .......... .......... .......... .......... 80% 12.8M 8s
431850K .......... .......... .......... .......... .......... 80% 31.2M 8s
431900K .......... .......... .......... .......... .......... 80% 49.1M 8s
431950K .......... .......... .......... .......... .......... 80% 70.6M 8s
432000K .......... .......... .......... .......... .......... 80% 50.2M 8s
432050K .......... .......... .......... .......... .......... 80% 43.5M 8s
432100K .......... .......... .......... .......... .......... 80% 52.4M 8s
432150K .......... .......... .......... .......... .......... 80% 42.6M 8s
432200K .......... .......... .......... .......... .......... 80% 51.6M 8s
432250K .......... .......... .......... .......... .......... 80% 48.6M 8s
432300K .......... .......... .......... .......... .......... 80% 64.8M 8s
432350K .......... .......... .......... .......... .......... 80% 47.1M 8s
432400K .......... .......... .......... .......... .......... 80% 40.4M 8s
432450K .......... .......... .......... .......... .......... 80% 51.7M 8s
432500K .......... .......... .......... .......... .......... 80% 57.5M 8s
432550K .......... .......... .......... .......... .......... 80% 58.5M 8s
432600K .......... .......... .......... .......... .......... 80% 36.9M 8s
432650K .......... .......... .......... .......... .......... 80% 39.3M 8s
432700K .......... .......... .......... .......... .......... 80% 76.2M 8s
432750K .......... .......... .......... .......... .......... 80% 55.2M 8s
432800K .......... .......... .......... .......... .......... 80% 31.9M 8s
432850K .......... .......... .......... .......... .......... 80% 48.3M 8s
432900K .......... .......... .......... .......... .......... 80% 78.3M 8s
432950K .......... .......... .......... .......... .......... 80% 40.9M 8s
433000K .......... .......... .......... .......... .......... 80% 55.9M 8s
433050K .......... .......... .......... .......... .......... 80% 54.9M 8s
433100K .......... .......... .......... .......... .......... 80% 31.4M 8s
433150K .......... .......... .......... .......... .......... 80% 66.2M 8s
433200K .......... .......... .......... .......... .......... 80% 45.9M 8s
433250K .......... .......... .......... .......... .......... 80% 87.0M 8s
433300K .......... .......... .......... .......... .......... 80% 23.9M 8s
433350K .......... .......... .......... .......... .......... 80% 38.6M 8s
433400K .......... .......... .......... .......... .......... 80% 52.4M 8s
433450K .......... .......... .......... .......... .......... 80%  108M 8s
433500K .......... .......... .......... .......... .......... 80% 75.9M 8s
433550K .......... .......... .......... .......... .......... 80% 62.0M 8s
433600K .......... .......... .......... .......... .......... 80% 32.7M 8s
433650K .......... .......... .......... .......... .......... 80% 26.6M 8s
433700K .......... .......... .......... .......... .......... 80% 27.4M 8s
433750K .......... .......... .......... .......... .......... 80% 38.9M 8s
433800K .......... .......... .......... .......... .......... 80% 32.5M 8s
433850K .......... .......... .......... .......... .......... 80% 38.8M 8s
433900K .......... .......... .......... .......... .......... 80% 26.6M 8s
433950K .......... .......... .......... .......... .......... 80% 36.9M 8s
434000K .......... .......... .......... .......... .......... 80% 34.4M 8s
434050K .......... .......... .......... .......... .......... 80% 22.4M 8s
434100K .......... .......... .......... .......... .......... 80% 33.1M 8s
434150K .......... .......... .......... .......... .......... 80% 36.6M 8s
434200K .......... .......... .......... .......... .......... 80% 22.4M 8s
434250K .......... .......... .......... .......... .......... 80% 41.9M 8s
434300K .......... .......... .......... .......... .......... 80% 37.7M 8s
434350K .......... .......... .......... .......... .......... 80% 27.2M 8s
434400K .......... .......... .......... .......... .......... 80% 34.3M 8s
434450K .......... .......... .......... .......... .......... 80% 31.5M 8s
434500K .......... .......... .......... .......... .......... 80% 38.1M 8s
434550K .......... .......... .......... .......... .......... 80% 23.8M 8s
434600K .......... .......... .......... .......... .......... 80% 22.1M 8s
434650K .......... .......... .......... .......... .......... 80% 20.9M 8s
434700K .......... .......... .......... .......... .......... 80% 19.4M 8s
434750K .......... .......... .......... .......... .......... 80% 38.4M 8s
434800K .......... .......... .......... .......... .......... 80% 19.2M 8s
434850K .......... .......... .......... .......... .......... 80% 19.2M 8s
434900K .......... .......... .......... .......... .......... 80% 22.1M 8s
434950K .......... .......... .......... .......... .......... 80% 20.4M 8s
435000K .......... .......... .......... .......... .......... 80% 36.7M 8s
435050K .......... .......... .......... .......... .......... 80% 16.5M 8s
435100K .......... .......... .......... .......... .......... 80% 23.2M 8s
435150K .......... .......... .......... .......... .......... 80% 25.0M 8s
435200K .......... .......... .......... .......... .......... 80% 20.8M 8s
435250K .......... .......... .......... .......... .......... 81% 22.1M 8s
435300K .......... .......... .......... .......... .......... 81% 33.2M 8s
435350K .......... .......... .......... .......... .......... 81% 53.7M 8s
435400K .......... .......... .......... .......... .......... 81%  109M 8s
435450K .......... .......... .......... .......... .......... 81% 36.7M 8s
435500K .......... .......... .......... .......... .......... 81% 80.0M 8s
435550K .......... .......... .......... .......... .......... 81% 80.8M 8s
435600K .......... .......... .......... .......... .......... 81% 53.2M 8s
435650K .......... .......... .......... .......... .......... 81%  123M 8s
435700K .......... .......... .......... .......... .......... 81% 33.5M 8s
435750K .......... .......... .......... .......... .......... 81% 50.9M 8s
435800K .......... .......... .......... .......... .......... 81%  105M 8s
435850K .......... .......... .......... .......... .......... 81% 49.3M 8s
435900K .......... .......... .......... .......... .......... 81% 7.65M 8s
435950K .......... .......... .......... .......... .......... 81% 98.4M 8s
436000K .......... .......... .......... .......... .......... 81%  121M 8s
436050K .......... .......... .......... .......... .......... 81%  112M 8s
436100K .......... .......... .......... .......... .......... 81%  113M 8s
436150K .......... .......... .......... .......... .......... 81%  150M 8s
436200K .......... .......... .......... .......... .......... 81% 76.5M 8s
436250K .......... .......... .......... .......... .......... 81%  109M 8s
436300K .......... .......... .......... .......... .......... 81%  141M 8s
436350K .......... .......... .......... .......... .......... 81% 99.9M 8s
436400K .......... .......... .......... .......... .......... 81% 29.9M 8s
436450K .......... .......... .......... .......... .......... 81% 92.5M 8s
436500K .......... .......... .......... .......... .......... 81%  152M 8s
436550K .......... .......... .......... .......... .......... 81%  103M 8s
436600K .......... .......... .......... .......... .......... 81% 75.1M 8s
436650K .......... .......... .......... .......... .......... 81% 55.0M 8s
436700K .......... .......... .......... .......... .......... 81% 37.0M 8s
436750K .......... .......... .......... .......... .......... 81%  101M 8s
436800K .......... .......... .......... .......... .......... 81% 39.1M 8s
436850K .......... .......... .......... .......... .......... 81% 48.4M 8s
436900K .......... .......... .......... .......... .......... 81% 48.2M 8s
436950K .......... .......... .......... .......... .......... 81% 53.7M 8s
437000K .......... .......... .......... .......... .......... 81% 65.0M 8s
437050K .......... .......... .......... .......... .......... 81% 62.1M 8s
437100K .......... .......... .......... .......... .......... 81% 43.6M 8s
437150K .......... .......... .......... .......... .......... 81% 59.3M 8s
437200K .......... .......... .......... .......... .......... 81% 37.1M 8s
437250K .......... .......... .......... .......... .......... 81% 56.4M 8s
437300K .......... .......... .......... .......... .......... 81% 88.6M 8s
437350K .......... .......... .......... .......... .......... 81% 54.4M 8s
437400K .......... .......... .......... .......... .......... 81% 44.9M 8s
437450K .......... .......... .......... .......... .......... 81% 60.7M 8s
437500K .......... .......... .......... .......... .......... 81% 61.2M 8s
437550K .......... .......... .......... .......... .......... 81% 62.9M 8s
437600K .......... .......... .......... .......... .......... 81% 43.1M 8s
437650K .......... .......... .......... .......... .......... 81% 37.3M 8s
437700K .......... .......... .......... .......... .......... 81% 86.4M 8s
437750K .......... .......... .......... .......... .......... 81% 42.2M 8s
437800K .......... .......... .......... .......... .......... 81% 43.5M 8s
437850K .......... .......... .......... .......... .......... 81% 29.6M 8s
437900K .......... .......... .......... .......... .......... 81%  118M 8s
437950K .......... .......... .......... .......... .......... 81% 47.4M 8s
438000K .......... .......... .......... .......... .......... 81% 48.3M 8s
438050K .......... .......... .......... .......... .......... 81% 81.8M 8s
438100K .......... .......... .......... .......... .......... 81% 33.0M 8s
438150K .......... .......... .......... .......... .......... 81% 31.8M 8s
438200K .......... .......... .......... .......... .......... 81% 38.2M 8s
438250K .......... .......... .......... .......... .......... 81% 48.0M 8s
438300K .......... .......... .......... .......... .......... 81% 76.4M 8s
438350K .......... .......... .......... .......... .......... 81% 41.6M 8s
438400K .......... .......... .......... .......... .......... 81% 35.9M 8s
438450K .......... .......... .......... .......... .......... 81% 32.8M 8s
438500K .......... .......... .......... .......... .......... 81% 35.1M 8s
438550K .......... .......... .......... .......... .......... 81% 53.2M 8s
438600K .......... .......... .......... .......... .......... 81% 41.8M 8s
438650K .......... .......... .......... .......... .......... 81% 50.6M 8s
438700K .......... .......... .......... .......... .......... 81% 37.1M 8s
438750K .......... .......... .......... .......... .......... 81% 35.4M 8s
438800K .......... .......... .......... .......... .......... 81% 37.9M 8s
438850K .......... .......... .......... .......... .......... 81% 36.9M 8s
438900K .......... .......... .......... .......... .......... 81% 44.6M 8s
438950K .......... .......... .......... .......... .......... 81% 47.0M 8s
439000K .......... .......... .......... .......... .......... 81% 46.5M 8s
439050K .......... .......... .......... .......... .......... 81% 44.4M 8s
439100K .......... .......... .......... .......... .......... 81% 42.5M 8s
439150K .......... .......... .......... .......... .......... 81% 49.1M 8s
439200K .......... .......... .......... .......... .......... 81% 35.6M 8s
439250K .......... .......... .......... .......... .......... 81% 41.7M 8s
439300K .......... .......... .......... .......... .......... 81% 51.9M 8s
439350K .......... .......... .......... .......... .......... 81% 31.5M 8s
439400K .......... .......... .......... .......... .......... 81% 65.8M 8s
439450K .......... .......... .......... .......... .......... 81% 47.1M 8s
439500K .......... .......... .......... .......... .......... 81% 24.7M 8s
439550K .......... .......... .......... .......... .......... 81%  159M 8s
439600K .......... .......... .......... .......... .......... 81% 35.1M 8s
439650K .......... .......... .......... .......... .......... 81% 79.3M 8s
439700K .......... .......... .......... .......... .......... 81% 14.7M 8s
439750K .......... .......... .......... .......... .......... 81%  100M 8s
439800K .......... .......... .......... .......... .......... 81% 96.9M 8s
439850K .......... .......... .......... .......... .......... 81% 33.8M 8s
439900K .......... .......... .......... .......... .......... 81% 97.9M 8s
439950K .......... .......... .......... .......... .......... 81% 32.8M 8s
440000K .......... .......... .......... .......... .......... 81% 63.5M 7s
440050K .......... .......... .......... .......... .......... 81% 39.0M 7s
440100K .......... .......... .......... .......... .......... 81% 35.1M 7s
440150K .......... .......... .......... .......... .......... 81% 33.6M 7s
440200K .......... .......... .......... .......... .......... 81% 30.4M 7s
440250K .......... .......... .......... .......... .......... 81% 33.4M 7s
440300K .......... .......... .......... .......... .......... 81% 36.8M 7s
440350K .......... .......... .......... .......... .......... 81% 36.9M 7s
440400K .......... .......... .......... .......... .......... 81% 34.5M 7s
440450K .......... .......... .......... .......... .......... 81% 19.2M 7s
440500K .......... .......... .......... .......... .......... 81% 12.6M 7s
440550K .......... .......... .......... .......... .......... 81% 33.1M 7s
440600K .......... .......... .......... .......... .......... 81% 28.0M 7s
440650K .......... .......... .......... .......... .......... 82% 33.7M 7s
440700K .......... .......... .......... .......... .......... 82% 22.1M 7s
440750K .......... .......... .......... .......... .......... 82% 31.6M 7s
440800K .......... .......... .......... .......... .......... 82% 30.6M 7s
440850K .......... .......... .......... .......... .......... 82% 29.7M 7s
440900K .......... .......... .......... .......... .......... 82% 37.0M 7s
440950K .......... .......... .......... .......... .......... 82% 22.4M 7s
441000K .......... .......... .......... .......... .......... 82% 35.8M 7s
441050K .......... .......... .......... .......... .......... 82% 47.0M 7s
441100K .......... .......... .......... .......... .......... 82% 34.3M 7s
441150K .......... .......... .......... .......... .......... 82% 14.2M 7s
441200K .......... .......... .......... .......... .......... 82% 72.3M 7s
441250K .......... .......... .......... .......... .......... 82%  125M 7s
441300K .......... .......... .......... .......... .......... 82% 32.4M 7s
441350K .......... .......... .......... .......... .......... 82% 38.1M 7s
441400K .......... .......... .......... .......... .......... 82% 32.6M 7s
441450K .......... .......... .......... .......... .......... 82%  122M 7s
441500K .......... .......... .......... .......... .......... 82% 36.9M 7s
441550K .......... .......... .......... .......... .......... 82% 31.8M 7s
441600K .......... .......... .......... .......... .......... 82% 37.2M 7s
441650K .......... .......... .......... .......... .......... 82% 35.8M 7s
441700K .......... .......... .......... .......... .......... 82% 36.0M 7s
441750K .......... .......... .......... .......... .......... 82% 25.3M 7s
441800K .......... .......... .......... .......... .......... 82% 32.9M 7s
441850K .......... .......... .......... .......... .......... 82% 36.7M 7s
441900K .......... .......... .......... .......... .......... 82% 34.1M 7s
441950K .......... .......... .......... .......... .......... 82% 36.9M 7s
442000K .......... .......... .......... .......... .......... 82% 42.3M 7s
442050K .......... .......... .......... .......... .......... 82% 30.0M 7s
442100K .......... .......... .......... .......... .......... 82% 26.5M 7s
442150K .......... .......... .......... .......... .......... 82% 34.8M 7s
442200K .......... .......... .......... .......... .......... 82% 28.4M 7s
442250K .......... .......... .......... .......... .......... 82% 37.1M 7s
442300K .......... .......... .......... .......... .......... 82% 34.8M 7s
442350K .......... .......... .......... .......... .......... 82% 14.2M 7s
442400K .......... .......... .......... .......... .......... 82% 27.4M 7s
442450K .......... .......... .......... .......... .......... 82% 28.2M 7s
442500K .......... .......... .......... .......... .......... 82% 41.0M 7s
442550K .......... .......... .......... .......... .......... 82% 30.6M 7s
442600K .......... .......... .......... .......... .......... 82% 41.5M 7s
442650K .......... .......... .......... .......... .......... 82% 27.2M 7s
442700K .......... .......... .......... .......... .......... 82% 29.3M 7s
442750K .......... .......... .......... .......... .......... 82% 34.4M 7s
442800K .......... .......... .......... .......... .......... 82% 18.2M 7s
442850K .......... .......... .......... .......... .......... 82% 61.1M 7s
442900K .......... .......... .......... .......... .......... 82% 32.0M 7s
442950K .......... .......... .......... .......... .......... 82% 24.6M 7s
443000K .......... .......... .......... .......... .......... 82%  142M 7s
443050K .......... .......... .......... .......... .......... 82%  128M 7s
443100K .......... .......... .......... .......... .......... 82% 21.8M 7s
443150K .......... .......... .......... .......... .......... 82% 41.5M 7s
443200K .......... .......... .......... .......... .......... 82% 14.9M 7s
443250K .......... .......... .......... .......... .......... 82% 28.7M 7s
443300K .......... .......... .......... .......... .......... 82% 18.0M 7s
443350K .......... .......... .......... .......... .......... 82% 20.5M 7s
443400K .......... .......... .......... .......... .......... 82% 21.6M 7s
443450K .......... .......... .......... .......... .......... 82% 20.9M 7s
443500K .......... .......... .......... .......... .......... 82% 24.5M 7s
443550K .......... .......... .......... .......... .......... 82% 19.8M 7s
443600K .......... .......... .......... .......... .......... 82% 21.1M 7s
443650K .......... .......... .......... .......... .......... 82% 25.8M 7s
443700K .......... .......... .......... .......... .......... 82% 16.7M 7s
443750K .......... .......... .......... .......... .......... 82% 25.5M 7s
443800K .......... .......... .......... .......... .......... 82% 20.9M 7s
443850K .......... .......... .......... .......... .......... 82% 19.0M 7s
443900K .......... .......... .......... .......... .......... 82% 24.2M 7s
443950K .......... .......... .......... .......... .......... 82% 17.9M 7s
444000K .......... .......... .......... .......... .......... 82% 24.8M 7s
444050K .......... .......... .......... .......... .......... 82% 21.4M 7s
444100K .......... .......... .......... .......... .......... 82% 18.8M 7s
444150K .......... .......... .......... .......... .......... 82% 21.4M 7s
444200K .......... .......... .......... .......... .......... 82% 18.1M 7s
444250K .......... .......... .......... .......... .......... 82% 27.6M 7s
444300K .......... .......... .......... .......... .......... 82% 20.7M 7s
444350K .......... .......... .......... .......... .......... 82% 34.0M 7s
444400K .......... .......... .......... .......... .......... 82% 77.1M 7s
444450K .......... .......... .......... .......... .......... 82% 32.3M 7s
444500K .......... .......... .......... .......... .......... 82%  110M 7s
444550K .......... .......... .......... .......... .......... 82% 61.5M 7s
444600K .......... .......... .......... .......... .......... 82% 56.8M 7s
444650K .......... .......... .......... .......... .......... 82% 93.0M 7s
444700K .......... .......... .......... .......... .......... 82% 40.6M 7s
444750K .......... .......... .......... .......... .......... 82% 84.9M 7s
444800K .......... .......... .......... .......... .......... 82% 59.2M 7s
444850K .......... .......... .......... .......... .......... 82% 45.8M 7s
444900K .......... .......... .......... .......... .......... 82% 43.2M 7s
444950K .......... .......... .......... .......... .......... 82% 47.0M 7s
445000K .......... .......... .......... .......... .......... 82% 86.6M 7s
445050K .......... .......... .......... .......... .......... 82% 54.4M 7s
445100K .......... .......... .......... .......... .......... 82% 92.3M 7s
445150K .......... .......... .......... .......... .......... 82% 64.0M 7s
445200K .......... .......... .......... .......... .......... 82% 78.8M 7s
445250K .......... .......... .......... .......... .......... 82% 41.7M 7s
445300K .......... .......... .......... .......... .......... 82%  117M 7s
445350K .......... .......... .......... .......... .......... 82% 39.6M 7s
445400K .......... .......... .......... .......... .......... 82% 56.6M 7s
445450K .......... .......... .......... .......... .......... 82% 68.5M 7s
445500K .......... .......... .......... .......... .......... 82% 51.6M 7s
445550K .......... .......... .......... .......... .......... 82%  114M 7s
445600K .......... .......... .......... .......... .......... 82% 55.6M 7s
445650K .......... .......... .......... .......... .......... 82% 75.7M 7s
445700K .......... .......... .......... .......... .......... 82% 51.9M 7s
445750K .......... .......... .......... .......... .......... 82% 55.5M 7s
445800K .......... .......... .......... .......... .......... 82% 97.9M 7s
445850K .......... .......... .......... .......... .......... 82% 35.4M 7s
445900K .......... .......... .......... .......... .......... 82%  120M 7s
445950K .......... .......... .......... .......... .......... 82% 53.9M 7s
446000K .......... .......... .......... .......... .......... 83% 43.5M 7s
446050K .......... .......... .......... .......... .......... 83%  128M 7s
446100K .......... .......... .......... .......... .......... 83% 45.3M 7s
446150K .......... .......... .......... .......... .......... 83% 75.1M 7s
446200K .......... .......... .......... .......... .......... 83% 56.3M 7s
446250K .......... .......... .......... .......... .......... 83% 45.7M 7s
446300K .......... .......... .......... .......... .......... 83%  119M 7s
446350K .......... .......... .......... .......... .......... 83% 54.3M 7s
446400K .......... .......... .......... .......... .......... 83%  108M 7s
446450K .......... .......... .......... .......... .......... 83% 44.8M 7s
446500K .......... .......... .......... .......... .......... 83% 44.6M 7s
446550K .......... .......... .......... .......... .......... 83% 99.0M 7s
446600K .......... .......... .......... .......... .......... 83% 64.1M 7s
446650K .......... .......... .......... .......... .......... 83% 88.3M 7s
446700K .......... .......... .......... .......... .......... 83% 59.3M 7s
446750K .......... .......... .......... .......... .......... 83% 75.7M 7s
446800K .......... .......... .......... .......... .......... 83% 44.4M 7s
446850K .......... .......... .......... .......... .......... 83% 50.2M 7s
446900K .......... .......... .......... .......... .......... 83%  107M 7s
446950K .......... .......... .......... .......... .......... 83% 47.9M 7s
447000K .......... .......... .......... .......... .......... 83%  111M 7s
447050K .......... .......... .......... .......... .......... 83% 45.1M 7s
447100K .......... .......... .......... .......... .......... 83% 97.3M 7s
447150K .......... .......... .......... .......... .......... 83% 47.0M 7s
447200K .......... .......... .......... .......... .......... 83% 75.0M 7s
447250K .......... .......... .......... .......... .......... 83% 54.6M 7s
447300K .......... .......... .......... .......... .......... 83%  107M 7s
447350K .......... .......... .......... .......... .......... 83% 41.0M 7s
447400K .......... .......... .......... .......... .......... 83% 77.1M 7s
447450K .......... .......... .......... .......... .......... 83% 51.7M 7s
447500K .......... .......... .......... .......... .......... 83% 52.1M 7s
447550K .......... .......... .......... .......... .......... 83% 74.8M 7s
447600K .......... .......... .......... .......... .......... 83% 49.8M 7s
447650K .......... .......... .......... .......... .......... 83% 95.0M 7s
447700K .......... .......... .......... .......... .......... 83% 39.9M 7s
447750K .......... .......... .......... .......... .......... 83% 49.4M 7s
447800K .......... .......... .......... .......... .......... 83% 91.6M 7s
447850K .......... .......... .......... .......... .......... 83% 43.1M 7s
447900K .......... .......... .......... .......... .......... 83% 88.1M 7s
447950K .......... .......... .......... .......... .......... 83% 50.7M 7s
448000K .......... .......... .......... .......... .......... 83% 75.5M 7s
448050K .......... .......... .......... .......... .......... 83% 63.3M 7s
448100K .......... .......... .......... .......... .......... 83% 35.6M 7s
448150K .......... .......... .......... .......... .......... 83% 96.1M 7s
448200K .......... .......... .......... .......... .......... 83% 75.4M 7s
448250K .......... .......... .......... .......... .......... 83% 54.0M 7s
448300K .......... .......... .......... .......... .......... 83%  117M 7s
448350K .......... .......... .......... .......... .......... 83% 51.5M 7s
448400K .......... .......... .......... .......... .......... 83% 50.7M 7s
448450K .......... .......... .......... .......... .......... 83% 90.4M 7s
448500K .......... .......... .......... .......... .......... 83% 42.7M 7s
448550K .......... .......... .......... .......... .......... 83% 98.4M 7s
448600K .......... .......... .......... .......... .......... 83% 57.6M 7s
448650K .......... .......... .......... .......... .......... 83% 88.5M 7s
448700K .......... .......... .......... .......... .......... 83% 54.0M 7s
448750K .......... .......... .......... .......... .......... 83% 80.4M 7s
448800K .......... .......... .......... .......... .......... 83% 82.2M 7s
448850K .......... .......... .......... .......... .......... 83% 56.0M 7s
448900K .......... .......... .......... .......... .......... 83% 51.1M 7s
448950K .......... .......... .......... .......... .......... 83% 81.1M 7s
449000K .......... .......... .......... .......... .......... 83% 56.5M 7s
449050K .......... .......... .......... .......... .......... 83%  113M 7s
449100K .......... .......... .......... .......... .......... 83% 46.9M 7s
449150K .......... .......... .......... .......... .......... 83% 61.0M 7s
449200K .......... .......... .......... .......... .......... 83% 77.0M 7s
449250K .......... .......... .......... .......... .......... 83% 51.4M 7s
449300K .......... .......... .......... .......... .......... 83%  136M 7s
449350K .......... .......... .......... .......... .......... 83% 44.5M 7s
449400K .......... .......... .......... .......... .......... 83%  114M 7s
449450K .......... .......... .......... .......... .......... 83% 42.2M 7s
449500K .......... .......... .......... .......... .......... 83% 62.2M 7s
449550K .......... .......... .......... .......... .......... 83%  127M 7s
449600K .......... .......... .......... .......... .......... 83% 51.3M 7s
449650K .......... .......... .......... .......... .......... 83% 86.0M 7s
449700K .......... .......... .......... .......... .......... 83% 44.3M 7s
449750K .......... .......... .......... .......... .......... 83%  116M 7s
449800K .......... .......... .......... .......... .......... 83% 43.1M 7s
449850K .......... .......... .......... .......... .......... 83% 95.6M 7s
449900K .......... .......... .......... .......... .......... 83% 58.9M 7s
449950K .......... .......... .......... .......... .......... 83% 86.1M 7s
450000K .......... .......... .......... .......... .......... 83% 77.1M 7s
450050K .......... .......... .......... .......... .......... 83% 69.5M 7s
450100K .......... .......... .......... .......... .......... 83% 47.6M 7s
450150K .......... .......... .......... .......... .......... 83%  136M 7s
450200K .......... .......... .......... .......... .......... 83% 47.0M 7s
450250K .......... .......... .......... .......... .......... 83%  114M 7s
450300K .......... .......... .......... .......... .......... 83% 41.1M 7s
450350K .......... .......... .......... .......... .......... 83% 59.2M 7s
450400K .......... .......... .......... .......... .......... 83% 88.3M 7s
450450K .......... .......... .......... .......... .......... 83% 63.0M 7s
450500K .......... .......... .......... .......... .......... 83% 85.7M 7s
450550K .......... .......... .......... .......... .......... 83% 73.5M 7s
450600K .......... .......... .......... .......... .......... 83% 83.3M 7s
450650K .......... .......... .......... .......... .......... 83% 83.6M 7s
450700K .......... .......... .......... .......... .......... 83% 79.1M 7s
450750K .......... .......... .......... .......... .......... 83% 99.0M 7s
450800K .......... .......... .......... .......... .......... 83% 95.6M 7s
450850K .......... .......... .......... .......... .......... 83% 88.3M 7s
450900K .......... .......... .......... .......... .......... 83% 94.3M 7s
450950K .......... .......... .......... .......... .......... 83% 89.4M 7s
451000K .......... .......... .......... .......... .......... 83%  105M 7s
451050K .......... .......... .......... .......... .......... 83% 60.6M 7s
451100K .......... .......... .......... .......... .......... 83% 89.3M 7s
451150K .......... .......... .......... .......... .......... 83%  101M 7s
451200K .......... .......... .......... .......... .......... 83% 86.9M 7s
451250K .......... .......... .......... .......... .......... 83%  108M 7s
451300K .......... .......... .......... .......... .......... 83% 67.3M 7s
451350K .......... .......... .......... .......... .......... 83% 81.9M 7s
451400K .......... .......... .......... .......... .......... 84%  113M 7s
451450K .......... .......... .......... .......... .......... 84% 62.0M 6s
451500K .......... .......... .......... .......... .......... 84%  129M 6s
451550K .......... .......... .......... .......... .......... 84%  116M 6s
451600K .......... .......... .......... .......... .......... 84% 56.0M 6s
451650K .......... .......... .......... .......... .......... 84%  114M 6s
451700K .......... .......... .......... .......... .......... 84%  101M 6s
451750K .......... .......... .......... .......... .......... 84% 90.6M 6s
451800K .......... .......... .......... .......... .......... 84%  106M 6s
451850K .......... .......... .......... .......... .......... 84% 89.6M 6s
451900K .......... .......... .......... .......... .......... 84%  113M 6s
451950K .......... .......... .......... .......... .......... 84% 62.7M 6s
452000K .......... .......... .......... .......... .......... 84%  114M 6s
452050K .......... .......... .......... .......... .......... 84%  118M 6s
452100K .......... .......... .......... .......... .......... 84% 69.1M 6s
452150K .......... .......... .......... .......... .......... 84%  107M 6s
452200K .......... .......... .......... .......... .......... 84%  106M 6s
452250K .......... .......... .......... .......... .......... 84% 70.1M 6s
452300K .......... .......... .......... .......... .......... 84% 88.9M 6s
452350K .......... .......... .......... .......... .......... 84%  128M 6s
452400K .......... .......... .......... .......... .......... 84% 57.2M 6s
452450K .......... .......... .......... .......... .......... 84%  103M 6s
452500K .......... .......... .......... .......... .......... 84% 97.3M 6s
452550K .......... .......... .......... .......... .......... 84%  103M 6s
452600K .......... .......... .......... .......... .......... 84% 67.7M 6s
452650K .......... .......... .......... .......... .......... 84%  170M 6s
452700K .......... .......... .......... .......... .......... 84% 93.7M 6s
452750K .......... .......... .......... .......... .......... 84% 94.3M 6s
452800K .......... .......... .......... .......... .......... 84%  107M 6s
452850K .......... .......... .......... .......... .......... 84%  109M 6s
452900K .......... .......... .......... .......... .......... 84% 79.8M 6s
452950K .......... .......... .......... .......... .......... 84%  121M 6s
453000K .......... .......... .......... .......... .......... 84% 88.3M 6s
453050K .......... .......... .......... .......... .......... 84% 89.1M 6s
453100K .......... .......... .......... .......... .......... 84%  105M 6s
453150K .......... .......... .......... .......... .......... 84%  135M 6s
453200K .......... .......... .......... .......... .......... 84% 81.0M 6s
453250K .......... .......... .......... .......... .......... 84% 73.4M 6s
453300K .......... .......... .......... .......... .......... 84%  115M 6s
453350K .......... .......... .......... .......... .......... 84% 78.9M 6s
453400K .......... .......... .......... .......... .......... 84%  164M 6s
453450K .......... .......... .......... .......... .......... 84% 80.0M 6s
453500K .......... .......... .......... .......... .......... 84% 98.8M 6s
453550K .......... .......... .......... .......... .......... 84%  125M 6s
453600K .......... .......... .......... .......... .......... 84% 71.4M 6s
453650K .......... .......... .......... .......... .......... 84%  111M 6s
453700K .......... .......... .......... .......... .......... 84% 84.3M 6s
453750K .......... .......... .......... .......... .......... 84%  100M 6s
453800K .......... .......... .......... .......... .......... 84%  134M 6s
453850K .......... .......... .......... .......... .......... 84% 94.4M 6s
453900K .......... .......... .......... .......... .......... 84% 93.9M 6s
453950K .......... .......... .......... .......... .......... 84% 89.3M 6s
454000K .......... .......... .......... .......... .......... 84%  112M 6s
454050K .......... .......... .......... .......... .......... 84% 65.1M 6s
454100K .......... .......... .......... .......... .......... 84%  110M 6s
454150K .......... .......... .......... .......... .......... 84% 62.2M 6s
454200K .......... .......... .......... .......... .......... 84% 83.9M 6s
454250K .......... .......... .......... .......... .......... 84%  124M 6s
454300K .......... .......... .......... .......... .......... 84%  117M 6s
454350K .......... .......... .......... .......... .......... 84% 71.2M 6s
454400K .......... .......... .......... .......... .......... 84%  114M 6s
454450K .......... .......... .......... .......... .......... 84% 81.4M 6s
454500K .......... .......... .......... .......... .......... 84% 98.6M 6s
454550K .......... .......... .......... .......... .......... 84%  131M 6s
454600K .......... .......... .......... .......... .......... 84% 84.2M 6s
454650K .......... .......... .......... .......... .......... 84% 89.9M 6s
454700K .......... .......... .......... .......... .......... 84% 93.9M 6s
454750K .......... .......... .......... .......... .......... 84%  116M 6s
454800K .......... .......... .......... .......... .......... 84%  105M 6s
454850K .......... .......... .......... .......... .......... 84% 93.7M 6s
454900K .......... .......... .......... .......... .......... 84% 14.7M 6s
454950K .......... .......... .......... .......... .......... 84% 92.8M 6s
455000K .......... .......... .......... .......... .......... 84%  169M 6s
455050K .......... .......... .......... .......... .......... 84%  105M 6s
455100K .......... .......... .......... .......... .......... 84% 9.38M 6s
455150K .......... .......... .......... .......... .......... 84%  168M 6s
455200K .......... .......... .......... .......... .......... 84% 88.5M 6s
455250K .......... .......... .......... .......... .......... 84%  104M 6s
455300K .......... .......... .......... .......... .......... 84%  106M 6s
455350K .......... .......... .......... .......... .......... 84% 91.8M 6s
455400K .......... .......... .......... .......... .......... 84%  102M 6s
455450K .......... .......... .......... .......... .......... 84%  123M 6s
455500K .......... .......... .......... .......... .......... 84%  146M 6s
455550K .......... .......... .......... .......... .......... 84%  117M 6s
455600K .......... .......... .......... .......... .......... 84% 49.1M 6s
455650K .......... .......... .......... .......... .......... 84%  134M 6s
455700K .......... .......... .......... .......... .......... 84%  125M 6s
455750K .......... .......... .......... .......... .......... 84%  147M 6s
455800K .......... .......... .......... .......... .......... 84%  169M 6s
455850K .......... .......... .......... .......... .......... 84% 26.9M 6s
455900K .......... .......... .......... .......... .......... 84% 85.2M 6s
455950K .......... .......... .......... .......... .......... 84%  126M 6s
456000K .......... .......... .......... .......... .......... 84%  136M 6s
456050K .......... .......... .......... .......... .......... 84%  119M 6s
456100K .......... .......... .......... .......... .......... 84% 93.4M 6s
456150K .......... .......... .......... .......... .......... 84%  114M 6s
456200K .......... .......... .......... .......... .......... 84% 48.7M 6s
456250K .......... .......... .......... .......... .......... 84% 47.9M 6s
456300K .......... .......... .......... .......... .......... 84%  136M 6s
456350K .......... .......... .......... .......... .......... 84% 42.8M 6s
456400K .......... .......... .......... .......... .......... 84% 35.3M 6s
456450K .......... .......... .......... .......... .......... 84% 50.1M 6s
456500K .......... .......... .......... .......... .......... 84% 80.4M 6s
456550K .......... .......... .......... .......... .......... 84% 50.6M 6s
456600K .......... .......... .......... .......... .......... 84% 49.0M 6s
456650K .......... .......... .......... .......... .......... 84% 53.5M 6s
456700K .......... .......... .......... .......... .......... 84% 66.4M 6s
456750K .......... .......... .......... .......... .......... 85% 49.6M 6s
456800K .......... .......... .......... .......... .......... 85% 75.0M 6s
456850K .......... .......... .......... .......... .......... 85% 53.4M 6s
456900K .......... .......... .......... .......... .......... 85% 60.0M 6s
456950K .......... .......... .......... .......... .......... 85% 52.4M 6s
457000K .......... .......... .......... .......... .......... 85% 97.3M 6s
457050K .......... .......... .......... .......... .......... 85% 54.0M 6s
457100K .......... .......... .......... .......... .......... 85% 36.8M 6s
457150K .......... .......... .......... .......... .......... 85%  118M 6s
457200K .......... .......... .......... .......... .......... 85% 48.5M 6s
457250K .......... .......... .......... .......... .......... 85% 42.9M 6s
457300K .......... .......... .......... .......... .......... 85% 43.0M 6s
457350K .......... .......... .......... .......... .......... 85% 93.5M 6s
457400K .......... .......... .......... .......... .......... 85% 54.1M 6s
457450K .......... .......... .......... .......... .......... 85% 60.8M 6s
457500K .......... .......... .......... .......... .......... 85% 70.2M 6s
457550K .......... .......... .......... .......... .......... 85% 56.4M 6s
457600K .......... .......... .......... .......... .......... 85% 57.4M 6s
457650K .......... .......... .......... .......... .......... 85% 59.7M 6s
457700K .......... .......... .......... .......... .......... 85% 65.6M 6s
457750K .......... .......... .......... .......... .......... 85% 49.5M 6s
457800K .......... .......... .......... .......... .......... 85% 55.4M 6s
457850K .......... .......... .......... .......... .......... 85% 65.3M 6s
457900K .......... .......... .......... .......... .......... 85% 75.9M 6s
457950K .......... .......... .......... .......... .......... 85% 48.2M 6s
458000K .......... .......... .......... .......... .......... 85%  112M 6s
458050K .......... .......... .......... .......... .......... 85%  114M 6s
458100K .......... .......... .......... .......... .......... 85% 38.3M 6s
458150K .......... .......... .......... .......... .......... 85% 12.6M 6s
458200K .......... .......... .......... .......... .......... 85%  100M 6s
458250K .......... .......... .......... .......... .......... 85%  156M 6s
458300K .......... .......... .......... .......... .......... 85%  149M 6s
458350K .......... .......... .......... .......... .......... 85%  134M 6s
458400K .......... .......... .......... .......... .......... 85%  135M 6s
458450K .......... .......... .......... .......... .......... 85%  147M 6s
458500K .......... .......... .......... .......... .......... 85%  146M 6s
458550K .......... .......... .......... .......... .......... 85%  105M 6s
458600K .......... .......... .......... .......... .......... 85%  111M 6s
458650K .......... .......... .......... .......... .......... 85%  119M 6s
458700K .......... .......... .......... .......... .......... 85%  109M 6s
458750K .......... .......... .......... .......... .......... 85% 66.6M 6s
458800K .......... .......... .......... .......... .......... 85%  131M 6s
458850K .......... .......... .......... .......... .......... 85%  102M 6s
458900K .......... .......... .......... .......... .......... 85%  136M 6s
458950K .......... .......... .......... .......... .......... 85% 90.1M 6s
459000K .......... .......... .......... .......... .......... 85%  123M 6s
459050K .......... .......... .......... .......... .......... 85%  151M 6s
459100K .......... .......... .......... .......... .......... 85%  113M 6s
459150K .......... .......... .......... .......... .......... 85%  120M 6s
459200K .......... .......... .......... .......... .......... 85% 76.5M 6s
459250K .......... .......... .......... .......... .......... 85% 46.6M 6s
459300K .......... .......... .......... .......... .......... 85% 47.9M 6s
459350K .......... .......... .......... .......... .......... 85% 86.9M 6s
459400K .......... .......... .......... .......... .......... 85% 33.8M 6s
459450K .......... .......... .......... .......... .......... 85% 83.8M 6s
459500K .......... .......... .......... .......... .......... 85% 42.2M 6s
459550K .......... .......... .......... .......... .......... 85% 66.3M 6s
459600K .......... .......... .......... .......... .......... 85% 60.3M 6s
459650K .......... .......... .......... .......... .......... 85%  131M 6s
459700K .......... .......... .......... .......... .......... 85% 46.8M 6s
459750K .......... .......... .......... .......... .......... 85% 98.0M 6s
459800K .......... .......... .......... .......... .......... 85% 44.9M 6s
459850K .......... .......... .......... .......... .......... 85% 82.6M 6s
459900K .......... .......... .......... .......... .......... 85% 53.2M 6s
459950K .......... .......... .......... .......... .......... 85% 58.1M 6s
460000K .......... .......... .......... .......... .......... 85% 92.0M 6s
460050K .......... .......... .......... .......... .......... 85% 62.7M 6s
460100K .......... .......... .......... .......... .......... 85% 79.1M 6s
460150K .......... .......... .......... .......... .......... 85% 63.1M 6s
460200K .......... .......... .......... .......... .......... 85% 59.3M 6s
460250K .......... .......... .......... .......... .......... 85% 39.7M 6s
460300K .......... .......... .......... .......... .......... 85%  132M 6s
460350K .......... .......... .......... .......... .......... 85% 38.0M 6s
460400K .......... .......... .......... .......... .......... 85% 67.4M 6s
460450K .......... .......... .......... .......... .......... 85% 73.3M 6s
460500K .......... .......... .......... .......... .......... 85% 40.9M 6s
460550K .......... .......... .......... .......... .......... 85% 84.6M 6s
460600K .......... .......... .......... .......... .......... 85% 67.3M 6s
460650K .......... .......... .......... .......... .......... 85% 57.8M 6s
460700K .......... .......... .......... .......... .......... 85% 78.5M 6s
460750K .......... .......... .......... .......... .......... 85% 65.5M 6s
460800K .......... .......... .......... .......... .......... 85% 71.3M 6s
460850K .......... .......... .......... .......... .......... 85% 67.7M 6s
460900K .......... .......... .......... .......... .......... 85% 43.1M 6s
460950K .......... .......... .......... .......... .......... 85%  115M 6s
461000K .......... .......... .......... .......... .......... 85% 47.5M 6s
461050K .......... .......... .......... .......... .......... 85%  122M 6s
461100K .......... .......... .......... .......... .......... 85% 51.3M 6s
461150K .......... .......... .......... .......... .......... 85% 56.0M 6s
461200K .......... .......... .......... .......... .......... 85% 75.0M 6s
461250K .......... .......... .......... .......... .......... 85% 97.1M 6s
461300K .......... .......... .......... .......... .......... 85%  120M 6s
461350K .......... .......... .......... .......... .......... 85% 63.7M 6s
461400K .......... .......... .......... .......... .......... 85% 96.1M 6s
461450K .......... .......... .......... .......... .......... 85%  104M 6s
461500K .......... .......... .......... .......... .......... 85% 84.0M 6s
461550K .......... .......... .......... .......... .......... 85%  101M 6s
461600K .......... .......... .......... .......... .......... 85% 96.5M 6s
461650K .......... .......... .......... .......... .......... 85%  107M 6s
461700K .......... .......... .......... .......... .......... 85% 73.2M 6s
461750K .......... .......... .......... .......... .......... 85%  103M 6s
461800K .......... .......... .......... .......... .......... 85%  108M 6s
461850K .......... .......... .......... .......... .......... 85% 95.0M 6s
461900K .......... .......... .......... .......... .......... 85%  104M 6s
461950K .......... .......... .......... .......... .......... 85% 95.2M 6s
462000K .......... .......... .......... .......... .......... 85%  103M 6s
462050K .......... .......... .......... .......... .......... 85%  111M 6s
462100K .......... .......... .......... .......... .......... 85% 97.3M 6s
462150K .......... .......... .......... .......... .......... 86% 27.2M 6s
462200K .......... .......... .......... .......... .......... 86%  103M 6s
462250K .......... .......... .......... .......... .......... 86% 77.5M 6s
462300K .......... .......... .......... .......... .......... 86%  112M 6s
462350K .......... .......... .......... .......... .......... 86% 80.3M 6s
462400K .......... .......... .......... .......... .......... 86%  131M 6s
462450K .......... .......... .......... .......... .......... 86%  119M 6s
462500K .......... .......... .......... .......... .......... 86%  121M 6s
462550K .......... .......... .......... .......... .......... 86%  120M 6s
462600K .......... .......... .......... .......... .......... 86%  113M 6s
462650K .......... .......... .......... .......... .......... 86%  139M 6s
462700K .......... .......... .......... .......... .......... 86%  102M 6s
462750K .......... .......... .......... .......... .......... 86%  137M 6s
462800K .......... .......... .......... .......... .......... 86%  136M 6s
462850K .......... .......... .......... .......... .......... 86% 96.9M 6s
462900K .......... .......... .......... .......... .......... 86% 68.2M 6s
462950K .......... .......... .......... .......... .......... 86% 98.2M 6s
463000K .......... .......... .......... .......... .......... 86% 87.3M 6s
463050K .......... .......... .......... .......... .......... 86% 88.8M 6s
463100K .......... .......... .......... .......... .......... 86% 68.9M 6s
463150K .......... .......... .......... .......... .......... 86%  128M 5s
463200K .......... .......... .......... .......... .......... 86% 78.0M 5s
463250K .......... .......... .......... .......... .......... 86% 94.4M 5s
463300K .......... .......... .......... .......... .......... 86%  126M 5s
463350K .......... .......... .......... .......... .......... 86% 66.1M 5s
463400K .......... .......... .......... .......... .......... 86%  105M 5s
463450K .......... .......... .......... .......... .......... 86% 74.2M 5s
463500K .......... .......... .......... .......... .......... 86% 99.2M 5s
463550K .......... .......... .......... .......... .......... 86% 92.5M 5s
463600K .......... .......... .......... .......... .......... 86% 78.9M 5s
463650K .......... .......... .......... .......... .......... 86%  119M 5s
463700K .......... .......... .......... .......... .......... 86% 77.1M 5s
463750K .......... .......... .......... .......... .......... 86% 78.3M 5s
463800K .......... .......... .......... .......... .......... 86% 93.2M 5s
463850K .......... .......... .......... .......... .......... 86% 86.6M 5s
463900K .......... .......... .......... .......... .......... 86% 92.7M 5s
463950K .......... .......... .......... .......... .......... 86% 64.6M 5s
464000K .......... .......... .......... .......... .......... 86%  110M 5s
464050K .......... .......... .......... .......... .......... 86%  105M 5s
464100K .......... .......... .......... .......... .......... 86% 50.1M 5s
464150K .......... .......... .......... .......... .......... 86%  107M 5s
464200K .......... .......... .......... .......... .......... 86%  104M 5s
464250K .......... .......... .......... .......... .......... 86% 74.7M 5s
464300K .......... .......... .......... .......... .......... 86% 56.5M 5s
464350K .......... .......... .......... .......... .......... 86% 59.5M 5s
464400K .......... .......... .......... .......... .......... 86%  110M 5s
464450K .......... .......... .......... .......... .......... 86% 97.5M 5s
464500K .......... .......... .......... .......... .......... 86% 54.1M 5s
464550K .......... .......... .......... .......... .......... 86%  111M 5s
464600K .......... .......... .......... .......... .......... 86% 44.2M 5s
464650K .......... .......... .......... .......... .......... 86% 93.5M 5s
464700K .......... .......... .......... .......... .......... 86% 54.5M 5s
464750K .......... .......... .......... .......... .......... 86%  107M 5s
464800K .......... .......... .......... .......... .......... 86%  119M 5s
464850K .......... .......... .......... .......... .......... 86% 45.4M 5s
464900K .......... .......... .......... .......... .......... 86%  121M 5s
464950K .......... .......... .......... .......... .......... 86% 39.9M 5s
465000K .......... .......... .......... .......... .......... 86%  133M 5s
465050K .......... .......... .......... .......... .......... 86% 75.4M 5s
465100K .......... .......... .......... .......... .......... 86% 75.6M 5s
465150K .......... .......... .......... .......... .......... 86%  124M 5s
465200K .......... .......... .......... .......... .......... 86% 51.3M 5s
465250K .......... .......... .......... .......... .......... 86%  110M 5s
465300K .......... .......... .......... .......... .......... 86% 92.1M 5s
465350K .......... .......... .......... .......... .......... 86% 78.5M 5s
465400K .......... .......... .......... .......... .......... 86% 90.6M 5s
465450K .......... .......... .......... .......... .......... 86% 90.3M 5s
465500K .......... .......... .......... .......... .......... 86%  116M 5s
465550K .......... .......... .......... .......... .......... 86%  107M 5s
465600K .......... .......... .......... .......... .......... 86% 82.1M 5s
465650K .......... .......... .......... .......... .......... 86%  118M 5s
465700K .......... .......... .......... .......... .......... 86% 87.2M 5s
465750K .......... .......... .......... .......... .......... 86%  127M 5s
465800K .......... .......... .......... .......... .......... 86% 98.6M 5s
465850K .......... .......... .......... .......... .......... 86% 68.9M 5s
465900K .......... .......... .......... .......... .......... 86%  103M 5s
465950K .......... .......... .......... .......... .......... 86% 91.6M 5s
466000K .......... .......... .......... .......... .......... 86%  105M 5s
466050K .......... .......... .......... .......... .......... 86%  107M 5s
466100K .......... .......... .......... .......... .......... 86% 93.0M 5s
466150K .......... .......... .......... .......... .......... 86%  111M 5s
466200K .......... .......... .......... .......... .......... 86% 86.0M 5s
466250K .......... .......... .......... .......... .......... 86%  111M 5s
466300K .......... .......... .......... .......... .......... 86%  110M 5s
466350K .......... .......... .......... .......... .......... 86% 76.7M 5s
466400K .......... .......... .......... .......... .......... 86% 43.4M 5s
466450K .......... .......... .......... .......... .......... 86% 58.3M 5s
466500K .......... .......... .......... .......... .......... 86%  160M 5s
466550K .......... .......... .......... .......... .......... 86%  138M 5s
466600K .......... .......... .......... .......... .......... 86%  120M 5s
466650K .......... .......... .......... .......... .......... 86%  104M 5s
466700K .......... .......... .......... .......... .......... 86% 26.0M 5s
466750K .......... .......... .......... .......... .......... 86%  109M 5s
466800K .......... .......... .......... .......... .......... 86%  131M 5s
466850K .......... .......... .......... .......... .......... 86%  108M 5s
466900K .......... .......... .......... .......... .......... 86%  106M 5s
466950K .......... .......... .......... .......... .......... 86%  103M 5s
467000K .......... .......... .......... .......... .......... 86%  131M 5s
467050K .......... .......... .......... .......... .......... 86% 47.8M 5s
467100K .......... .......... .......... .......... .......... 86% 74.3M 5s
467150K .......... .......... .......... .......... .......... 86% 31.3M 5s
467200K .......... .......... .......... .......... .......... 86%  117M 5s
467250K .......... .......... .......... .......... .......... 86% 54.5M 5s
467300K .......... .......... .......... .......... .......... 86%  125M 5s
467350K .......... .......... .......... .......... .......... 86% 47.2M 5s
467400K .......... .......... .......... .......... .......... 86%  121M 5s
467450K .......... .......... .......... .......... .......... 86% 38.8M 5s
467500K .......... .......... .......... .......... .......... 87% 45.1M 5s
467550K .......... .......... .......... .......... .......... 87%  140M 5s
467600K .......... .......... .......... .......... .......... 87% 34.5M 5s
467650K .......... .......... .......... .......... .......... 87%  113M 5s
467700K .......... .......... .......... .......... .......... 87% 42.9M 5s
467750K .......... .......... .......... .......... .......... 87%  103M 5s
467800K .......... .......... .......... .......... .......... 87% 49.0M 5s
467850K .......... .......... .......... .......... .......... 87% 85.2M 5s
467900K .......... .......... .......... .......... .......... 87% 52.5M 5s
467950K .......... .......... .......... .......... .......... 87% 41.5M 5s
468000K .......... .......... .......... .......... .......... 87% 96.1M 5s
468050K .......... .......... .......... .......... .......... 87% 43.6M 5s
468100K .......... .......... .......... .......... .......... 87% 99.0M 5s
468150K .......... .......... .......... .......... .......... 87% 57.6M 5s
468200K .......... .......... .......... .......... .......... 87%  105M 5s
468250K .......... .......... .......... .......... .......... 87% 47.0M 5s
468300K .......... .......... .......... .......... .......... 87% 70.9M 5s
468350K .......... .......... .......... .......... .......... 87% 19.0M 5s
468400K .......... .......... .......... .......... .......... 87%  127M 5s
468450K .......... .......... .......... .......... .......... 87%  101M 5s
468500K .......... .......... .......... .......... .......... 87% 92.7M 5s
468550K .......... .......... .......... .......... .......... 87% 44.1M 5s
468600K .......... .......... .......... .......... .......... 87%  102M 5s
468650K .......... .......... .......... .......... .......... 87% 46.9M 5s
468700K .......... .......... .......... .......... .......... 87%  101M 5s
468750K .......... .......... .......... .......... .......... 87% 40.1M 5s
468800K .......... .......... .......... .......... .......... 87% 50.2M 5s
468850K .......... .......... .......... .......... .......... 87% 78.6M 5s
468900K .......... .......... .......... .......... .......... 87% 36.1M 5s
468950K .......... .......... .......... .......... .......... 87% 82.8M 5s
469000K .......... .......... .......... .......... .......... 87% 42.7M 5s
469050K .......... .......... .......... .......... .......... 87% 95.4M 5s
469100K .......... .......... .......... .......... .......... 87%  122M 5s
469150K .......... .......... .......... .......... .......... 87% 43.3M 5s
469200K .......... .......... .......... .......... .......... 87%  113M 5s
469250K .......... .......... .......... .......... .......... 87% 37.7M 5s
469300K .......... .......... .......... .......... .......... 87%  187M 5s
469350K .......... .......... .......... .......... .......... 87%  162M 5s
469400K .......... .......... .......... .......... .......... 87%  126M 5s
469450K .......... .......... .......... .......... .......... 87%  104M 5s
469500K .......... .......... .......... .......... .......... 87% 79.5M 5s
469550K .......... .......... .......... .......... .......... 87% 64.9M 5s
469600K .......... .......... .......... .......... .......... 87%  136M 5s
469650K .......... .......... .......... .......... .......... 87% 67.7M 5s
469700K .......... .......... .......... .......... .......... 87%  107M 5s
469750K .......... .......... .......... .......... .......... 87%  116M 5s
469800K .......... .......... .......... .......... .......... 87% 62.6M 5s
469850K .......... .......... .......... .......... .......... 87%  118M 5s
469900K .......... .......... .......... .......... .......... 87%  136M 5s
469950K .......... .......... .......... .......... .......... 87% 58.5M 5s
470000K .......... .......... .......... .......... .......... 87%  147M 5s
470050K .......... .......... .......... .......... .......... 87%  132M 5s
470100K .......... .......... .......... .......... .......... 87% 10.5M 5s
470150K .......... .......... .......... .......... .......... 87%  134M 5s
470200K .......... .......... .......... .......... .......... 87%  102M 5s
470250K .......... .......... .......... .......... .......... 87%  185M 5s
470300K .......... .......... .......... .......... .......... 87%  107M 5s
470350K .......... .......... .......... .......... .......... 87%  131M 5s
470400K .......... .......... .......... .......... .......... 87%  167M 5s
470450K .......... .......... .......... .......... .......... 87% 86.1M 5s
470500K .......... .......... .......... .......... .......... 87%  166M 5s
470550K .......... .......... .......... .......... .......... 87%  119M 5s
470600K .......... .......... .......... .......... .......... 87%  125M 5s
470650K .......... .......... .......... .......... .......... 87%  177M 5s
470700K .......... .......... .......... .......... .......... 87%  109M 5s
470750K .......... .......... .......... .......... .......... 87%  136M 5s
470800K .......... .......... .......... .......... .......... 87%  130M 5s
470850K .......... .......... .......... .......... .......... 87%  116M 5s
470900K .......... .......... .......... .......... .......... 87%  128M 5s
470950K .......... .......... .......... .......... .......... 87%  106M 5s
471000K .......... .......... .......... .......... .......... 87%  129M 5s
471050K .......... .......... .......... .......... .......... 87%  121M 5s
471100K .......... .......... .......... .......... .......... 87% 84.5M 5s
471150K .......... .......... .......... .......... .......... 87% 96.3M 5s
471200K .......... .......... .......... .......... .......... 87% 78.6M 5s
471250K .......... .......... .......... .......... .......... 87%  120M 5s
471300K .......... .......... .......... .......... .......... 87% 91.8M 5s
471350K .......... .......... .......... .......... .......... 87% 95.9M 5s
471400K .......... .......... .......... .......... .......... 87% 93.7M 5s
471450K .......... .......... .......... .......... .......... 87% 76.3M 5s
471500K .......... .......... .......... .......... .......... 87%  125M 5s
471550K .......... .......... .......... .......... .......... 87%  111M 5s
471600K .......... .......... .......... .......... .......... 87% 52.3M 5s
471650K .......... .......... .......... .......... .......... 87%  130M 5s
471700K .......... .......... .......... .......... .......... 87% 80.4M 5s
471750K .......... .......... .......... .......... .......... 87%  107M 5s
471800K .......... .......... .......... .......... .......... 87% 53.8M 5s
471850K .......... .......... .......... .......... .......... 87% 97.1M 5s
471900K .......... .......... .......... .......... .......... 87%  100M 5s
471950K .......... .......... .......... .......... .......... 87%  106M 5s
472000K .......... .......... .......... .......... .......... 87% 85.1M 5s
472050K .......... .......... .......... .......... .......... 87% 95.2M 5s
472100K .......... .......... .......... .......... .......... 87% 92.7M 5s
472150K .......... .......... .......... .......... .......... 87%  102M 5s
472200K .......... .......... .......... .......... .......... 87% 90.8M 5s
472250K .......... .......... .......... .......... .......... 87%  126M 5s
472300K .......... .......... .......... .......... .......... 87% 67.5M 5s
472350K .......... .......... .......... .......... .......... 87% 91.3M 5s
472400K .......... .......... .......... .......... .......... 87%  119M 5s
472450K .......... .......... .......... .......... .......... 87% 57.5M 5s
472500K .......... .......... .......... .......... .......... 87% 63.2M 5s
472550K .......... .......... .......... .......... .......... 87%  108M 5s
472600K .......... .......... .......... .......... .......... 87% 95.2M 5s
472650K .......... .......... .......... .......... .......... 87% 97.1M 5s
472700K .......... .......... .......... .......... .......... 87% 76.8M 5s
472750K .......... .......... .......... .......... .......... 87% 74.8M 5s
472800K .......... .......... .......... .......... .......... 87%  101M 5s
472850K .......... .......... .......... .......... .......... 87% 80.4M 5s
472900K .......... .......... .......... .......... .......... 88% 84.2M 5s
472950K .......... .......... .......... .......... .......... 88% 99.9M 5s
473000K .......... .......... .......... .......... .......... 88% 76.7M 5s
473050K .......... .......... .......... .......... .......... 88%  101M 5s
473100K .......... .......... .......... .......... .......... 88% 88.5M 5s
473150K .......... .......... .......... .......... .......... 88%  121M 5s
473200K .......... .......... .......... .......... .......... 88% 73.1M 5s
473250K .......... .......... .......... .......... .......... 88%  111M 5s
473300K .......... .......... .......... .......... .......... 88% 48.4M 5s
473350K .......... .......... .......... .......... .......... 88% 97.3M 5s
473400K .......... .......... .......... .......... .......... 88%  138M 5s
473450K .......... .......... .......... .......... .......... 88% 51.7M 5s
473500K .......... .......... .......... .......... .......... 88% 97.9M 5s
473550K .......... .......... .......... .......... .......... 88%  100M 5s
473600K .......... .......... .......... .......... .......... 88% 98.0M 5s
473650K .......... .......... .......... .......... .......... 88% 94.1M 5s
473700K .......... .......... .......... .......... .......... 88% 71.4M 5s
473750K .......... .......... .......... .......... .......... 88%  150M 5s
473800K .......... .......... .......... .......... .......... 88% 61.7M 5s
473850K .......... .......... .......... .......... .......... 88%  107M 5s
473900K .......... .......... .......... .......... .......... 88% 86.9M 5s
473950K .......... .......... .......... .......... .......... 88% 75.2M 5s
474000K .......... .......... .......... .......... .......... 88%  110M 5s
474050K .......... .......... .......... .......... .......... 88%  105M 5s
474100K .......... .......... .......... .......... .......... 88% 57.0M 5s
474150K .......... .......... .......... .......... .......... 88%  119M 5s
474200K .......... .......... .......... .......... .......... 88% 75.7M 5s
474250K .......... .......... .......... .......... .......... 88%  128M 5s
474300K .......... .......... .......... .......... .......... 88% 93.2M 5s
474350K .......... .......... .......... .......... .......... 88% 87.2M 5s
474400K .......... .......... .......... .......... .......... 88% 99.2M 5s
474450K .......... .......... .......... .......... .......... 88% 93.2M 5s
474500K .......... .......... .......... .......... .......... 88% 96.5M 5s
474550K .......... .......... .......... .......... .......... 88%  122M 5s
474600K .......... .......... .......... .......... .......... 88% 66.3M 5s
474650K .......... .......... .......... .......... .......... 88%  102M 5s
474700K .......... .......... .......... .......... .......... 88% 95.9M 5s
474750K .......... .......... .......... .......... .......... 88% 89.8M 5s
474800K .......... .......... .......... .......... .......... 88% 97.5M 5s
474850K .......... .......... .......... .......... .......... 88% 74.4M 5s
474900K .......... .......... .......... .......... .......... 88% 94.6M 5s
474950K .......... .......... .......... .......... .......... 88% 90.4M 5s
475000K .......... .......... .......... .......... .......... 88%  142M 5s
475050K .......... .......... .......... .......... .......... 88% 82.8M 5s
475100K .......... .......... .......... .......... .......... 88% 86.6M 5s
475150K .......... .......... .......... .......... .......... 88% 98.8M 5s
475200K .......... .......... .......... .......... .......... 88% 85.4M 5s
475250K .......... .......... .......... .......... .......... 88% 91.4M 5s
475300K .......... .......... .......... .......... .......... 88%  138M 4s
475350K .......... .......... .......... .......... .......... 88% 83.2M 4s
475400K .......... .......... .......... .......... .......... 88%  122M 4s
475450K .......... .......... .......... .......... .......... 88% 84.0M 4s
475500K .......... .......... .......... .......... .......... 88% 87.3M 4s
475550K .......... .......... .......... .......... .......... 88% 96.7M 4s
475600K .......... .......... .......... .......... .......... 88% 42.1M 4s
475650K .......... .......... .......... .......... .......... 88%  121M 4s
475700K .......... .......... .......... .......... .......... 88% 94.4M 4s
475750K .......... .......... .......... .......... .......... 88%  103M 4s
475800K .......... .......... .......... .......... .......... 88% 95.4M 4s
475850K .......... .......... .......... .......... .......... 88% 87.0M 4s
475900K .......... .......... .......... .......... .......... 88% 82.2M 4s
475950K .......... .......... .......... .......... .......... 88% 90.8M 4s
476000K .......... .......... .......... .......... .......... 88% 95.9M 4s
476050K .......... .......... .......... .......... .......... 88% 89.9M 4s
476100K .......... .......... .......... .......... .......... 88%  132M 4s
476150K .......... .......... .......... .......... .......... 88%  103M 4s
476200K .......... .......... .......... .......... .......... 88% 56.7M 4s
476250K .......... .......... .......... .......... .......... 88%  109M 4s
476300K .......... .......... .......... .......... .......... 88% 93.2M 4s
476350K .......... .......... .......... .......... .......... 88% 78.1M 4s
476400K .......... .......... .......... .......... .......... 88%  138M 4s
476450K .......... .......... .......... .......... .......... 88% 47.1M 4s
476500K .......... .......... .......... .......... .......... 88%  106M 4s
476550K .......... .......... .......... .......... .......... 88%  118M 4s
476600K .......... .......... .......... .......... .......... 88% 61.2M 4s
476650K .......... .......... .......... .......... .......... 88%  101M 4s
476700K .......... .......... .......... .......... .......... 88%  111M 4s
476750K .......... .......... .......... .......... .......... 88% 61.2M 4s
476800K .......... .......... .......... .......... .......... 88%  102M 4s
476850K .......... .......... .......... .......... .......... 88% 87.2M 4s
476900K .......... .......... .......... .......... .......... 88% 98.4M 4s
476950K .......... .......... .......... .......... .......... 88% 70.9M 4s
477000K .......... .......... .......... .......... .......... 88%  141M 4s
477050K .......... .......... .......... .......... .......... 88% 93.9M 4s
477100K .......... .......... .......... .......... .......... 88% 66.4M 4s
477150K .......... .......... .......... .......... .......... 88% 91.6M 4s
477200K .......... .......... .......... .......... .......... 88% 96.9M 4s
477250K .......... .......... .......... .......... .......... 88% 56.8M 4s
477300K .......... .......... .......... .......... .......... 88%  134M 4s
477350K .......... .......... .......... .......... .......... 88% 69.5M 4s
477400K .......... .......... .......... .......... .......... 88% 92.8M 4s
477450K .......... .......... .......... .......... .......... 88% 91.1M 4s
477500K .......... .......... .......... .......... .......... 88%  145M 4s
477550K .......... .......... .......... .......... .......... 88% 80.0M 4s
477600K .......... .......... .......... .......... .......... 88% 80.2M 4s
477650K .......... .......... .......... .......... .......... 88%  126M 4s
477700K .......... .......... .......... .......... .......... 88% 70.7M 4s
477750K .......... .......... .......... .......... .......... 88% 93.5M 4s
477800K .......... .......... .......... .......... .......... 88%  127M 4s
477850K .......... .......... .......... .......... .......... 88% 58.3M 4s
477900K .......... .......... .......... .......... .......... 88%  119M 4s
477950K .......... .......... .......... .......... .......... 88% 93.9M 4s
478000K .......... .......... .......... .......... .......... 88% 87.5M 4s
478050K .......... .......... .......... .......... .......... 88%  118M 4s
478100K .......... .......... .......... .......... .......... 88% 86.3M 4s
478150K .......... .......... .......... .......... .......... 88%  101M 4s
478200K .......... .......... .......... .......... .......... 88% 74.4M 4s
478250K .......... .......... .......... .......... .......... 89%  103M 4s
478300K .......... .......... .......... .......... .......... 89% 92.8M 4s
478350K .......... .......... .......... .......... .......... 89% 65.3M 4s
478400K .......... .......... .......... .......... .......... 89% 79.0M 4s
478450K .......... .......... .......... .......... .......... 89%  100M 4s
478500K .......... .......... .......... .......... .......... 89% 96.1M 4s
478550K .......... .......... .......... .......... .......... 89%  128M 4s
478600K .......... .......... .......... .......... .......... 89% 27.2M 4s
478650K .......... .......... .......... .......... .......... 89% 90.6M 4s
478700K .......... .......... .......... .......... .......... 89%  119M 4s
478750K .......... .......... .......... .......... .......... 89%  120M 4s
478800K .......... .......... .......... .......... .......... 89% 99.2M 4s
478850K .......... .......... .......... .......... .......... 89% 90.3M 4s
478900K .......... .......... .......... .......... .......... 89%  118M 4s
478950K .......... .......... .......... .......... .......... 89%  123M 4s
479000K .......... .......... .......... .......... .......... 89%  134M 4s
479050K .......... .......... .......... .......... .......... 89% 71.1M 4s
479100K .......... .......... .......... .......... .......... 89% 45.2M 4s
479150K .......... .......... .......... .......... .......... 89% 92.5M 4s
479200K .......... .......... .......... .......... .......... 89% 49.0M 4s
479250K .......... .......... .......... .......... .......... 89%  117M 4s
479300K .......... .......... .......... .......... .......... 89% 52.9M 4s
479350K .......... .......... .......... .......... .......... 89% 90.6M 4s
479400K .......... .......... .......... .......... .......... 89% 54.4M 4s
479450K .......... .......... .......... .......... .......... 89% 39.2M 4s
479500K .......... .......... .......... .......... .......... 89% 94.1M 4s
479550K .......... .......... .......... .......... .......... 89% 70.0M 4s
479600K .......... .......... .......... .......... .......... 89% 86.9M 4s
479650K .......... .......... .......... .......... .......... 89% 46.2M 4s
479700K .......... .......... .......... .......... .......... 89% 69.6M 4s
479750K .......... .......... .......... .......... .......... 89% 49.8M 4s
479800K .......... .......... .......... .......... .......... 89% 47.1M 4s
479850K .......... .......... .......... .......... .......... 89% 81.0M 4s
479900K .......... .......... .......... .......... .......... 89% 40.4M 4s
479950K .......... .......... .......... .......... .......... 89% 59.7M 4s
480000K .......... .......... .......... .......... .......... 89% 72.3M 4s
480050K .......... .......... .......... .......... .......... 89% 32.8M 4s
480100K .......... .......... .......... .......... .......... 89% 66.6M 4s
480150K .......... .......... .......... .......... .......... 89% 48.2M 4s
480200K .......... .......... .......... .......... .......... 89% 62.0M 4s
480250K .......... .......... .......... .......... .......... 89%  132M 4s
480300K .......... .......... .......... .......... .......... 89% 46.5M 4s
480350K .......... .......... .......... .......... .......... 89%  100M 4s
480400K .......... .......... .......... .......... .......... 89% 51.9M 4s
480450K .......... .......... .......... .......... .......... 89% 60.2M 4s
480500K .......... .......... .......... .......... .......... 89% 80.6M 4s
480550K .......... .......... .......... .......... .......... 89% 66.7M 4s
480600K .......... .......... .......... .......... .......... 89% 41.6M 4s
480650K .......... .......... .......... .......... .......... 89% 85.2M 4s
480700K .......... .......... .......... .......... .......... 89% 51.0M 4s
480750K .......... .......... .......... .......... .......... 89% 84.5M 4s
480800K .......... .......... .......... .......... .......... 89% 48.8M 4s
480850K .......... .......... .......... .......... .......... 89% 85.4M 4s
480900K .......... .......... .......... .......... .......... 89% 37.6M 4s
480950K .......... .......... .......... .......... .......... 89% 80.4M 4s
481000K .......... .......... .......... .......... .......... 89% 35.4M 4s
481050K .......... .......... .......... .......... .......... 89% 51.1M 4s
481100K .......... .......... .......... .......... .......... 89% 84.2M 4s
481150K .......... .......... .......... .......... .......... 89% 52.7M 4s
481200K .......... .......... .......... .......... .......... 89% 82.2M 4s
481250K .......... .......... .......... .......... .......... 89% 87.7M 4s
481300K .......... .......... .......... .......... .......... 89% 69.8M 4s
481350K .......... .......... .......... .......... .......... 89% 86.4M 4s
481400K .......... .......... .......... .......... .......... 89%  131M 4s
481450K .......... .......... .......... .......... .......... 89% 55.9M 4s
481500K .......... .......... .......... .......... .......... 89%  114M 4s
481550K .......... .......... .......... .......... .......... 89%  105M 4s
481600K .......... .......... .......... .......... .......... 89% 73.4M 4s
481650K .......... .......... .......... .......... .......... 89% 54.4M 4s
481700K .......... .......... .......... .......... .......... 89% 84.9M 4s
481750K .......... .......... .......... .......... .......... 89%  129M 4s
481800K .......... .......... .......... .......... .......... 89%  117M 4s
481850K .......... .......... .......... .......... .......... 89% 63.2M 4s
481900K .......... .......... .......... .......... .......... 89%  102M 4s
481950K .......... .......... .......... .......... .......... 89% 56.6M 4s
482000K .......... .......... .......... .......... .......... 89%  107M 4s
482050K .......... .......... .......... .......... .......... 89% 38.3M 4s
482100K .......... .......... .......... .......... .......... 89% 75.9M 4s
482150K .......... .......... .......... .......... .......... 89%  148M 4s
482200K .......... .......... .......... .......... .......... 89%  137M 4s
482250K .......... .......... .......... .......... .......... 89%  108M 4s
482300K .......... .......... .......... .......... .......... 89%  117M 4s
482350K .......... .......... .......... .......... .......... 89% 73.2M 4s
482400K .......... .......... .......... .......... .......... 89% 76.9M 4s
482450K .......... .......... .......... .......... .......... 89% 93.2M 4s
482500K .......... .......... .......... .......... .......... 89% 74.4M 4s
482550K .......... .......... .......... .......... .......... 89% 94.4M 4s
482600K .......... .......... .......... .......... .......... 89% 48.5M 4s
482650K .......... .......... .......... .......... .......... 89%  104M 4s
482700K .......... .......... .......... .......... .......... 89% 69.8M 4s
482750K .......... .......... .......... .......... .......... 89% 80.2M 4s
482800K .......... .......... .......... .......... .......... 89% 92.0M 4s
482850K .......... .......... .......... .......... .......... 89% 49.1M 4s
482900K .......... .......... .......... .......... .......... 89% 56.1M 4s
482950K .......... .......... .......... .......... .......... 89% 97.3M 4s
483000K .......... .......... .......... .......... .......... 89% 76.2M 4s
483050K .......... .......... .......... .......... .......... 89% 75.0M 4s
483100K .......... .......... .......... .......... .......... 89% 87.7M 4s
483150K .......... .......... .......... .......... .......... 89% 55.4M 4s
483200K .......... .......... .......... .......... .......... 89% 77.6M 4s
483250K .......... .......... .......... .......... .......... 89% 65.8M 4s
483300K .......... .......... .......... .......... .......... 89% 81.0M 4s
483350K .......... .......... .......... .......... .......... 89% 20.8M 4s
483400K .......... .......... .......... .......... .......... 89%  154M 4s
483450K .......... .......... .......... .......... .......... 89%  109M 4s
483500K .......... .......... .......... .......... .......... 89%  141M 4s
483550K .......... .......... .......... .......... .......... 89%  147M 4s
483600K .......... .......... .......... .......... .......... 89% 64.2M 4s
483650K .......... .......... .......... .......... .......... 90% 94.3M 4s
483700K .......... .......... .......... .......... .......... 90% 44.5M 4s
483750K .......... .......... .......... .......... .......... 90% 85.1M 4s
483800K .......... .......... .......... .......... .......... 90%  127M 4s
483850K .......... .......... .......... .......... .......... 90% 54.9M 4s
483900K .......... .......... .......... .......... .......... 90%  110M 4s
483950K .......... .......... .......... .......... .......... 90% 42.6M 4s
484000K .......... .......... .......... .......... .......... 90%  106M 4s
484050K .......... .......... .......... .......... .......... 90% 61.3M 4s
484100K .......... .......... .......... .......... .......... 90% 74.3M 4s
484150K .......... .......... .......... .......... .......... 90% 40.0M 4s
484200K .......... .......... .......... .......... .......... 90% 69.4M 4s
484250K .......... .......... .......... .......... .......... 90% 57.6M 4s
484300K .......... .......... .......... .......... .......... 90% 90.4M 4s
484350K .......... .......... .......... .......... .......... 90% 34.7M 4s
484400K .......... .......... .......... .......... .......... 90%  118M 4s
484450K .......... .......... .......... .......... .......... 90% 65.5M 4s
484500K .......... .......... .......... .......... .......... 90% 73.0M 4s
484550K .......... .......... .......... .......... .......... 90% 91.8M 4s
484600K .......... .......... .......... .......... .......... 90% 43.9M 4s
484650K .......... .......... .......... .......... .......... 90% 82.8M 4s
484700K .......... .......... .......... .......... .......... 90% 71.9M 4s
484750K .......... .......... .......... .......... .......... 90% 92.7M 4s
484800K .......... .......... .......... .......... .......... 90%  102M 4s
484850K .......... .......... .......... .......... .......... 90% 54.9M 4s
484900K .......... .......... .......... .......... .......... 90%  122M 4s
484950K .......... .......... .......... .......... .......... 90% 82.8M 4s
485000K .......... .......... .......... .......... .......... 90% 51.5M 4s
485050K .......... .......... .......... .......... .......... 90%  109M 4s
485100K .......... .......... .......... .......... .......... 90% 24.1M 4s
485150K .......... .......... .......... .......... .......... 90%  125M 4s
485200K .......... .......... .......... .......... .......... 90%  159M 4s
485250K .......... .......... .......... .......... .......... 90%  129M 4s
485300K .......... .......... .......... .......... .......... 90%  192M 4s
485350K .......... .......... .......... .......... .......... 90%  157M 4s
485400K .......... .......... .......... .......... .......... 90% 45.4M 4s
485450K .......... .......... .......... .......... .......... 90%  174M 4s
485500K .......... .......... .......... .......... .......... 90% 52.7M 4s
485550K .......... .......... .......... .......... .......... 90%  108M 4s
485600K .......... .......... .......... .......... .......... 90% 49.5M 4s
485650K .......... .......... .......... .......... .......... 90%  115M 4s
485700K .......... .......... .......... .......... .......... 90% 43.5M 4s
485750K .......... .......... .......... .......... .......... 90%  164M 4s
485800K .......... .......... .......... .......... .......... 90% 38.6M 4s
485850K .......... .......... .......... .......... .......... 90% 79.4M 4s
485900K .......... .......... .......... .......... .......... 90% 74.4M 4s
485950K .......... .......... .......... .......... .......... 90% 94.8M 4s
486000K .......... .......... .......... .......... .......... 90% 54.4M 4s
486050K .......... .......... .......... .......... .......... 90%  133M 4s
486100K .......... .......... .......... .......... .......... 90% 41.6M 4s
486150K .......... .......... .......... .......... .......... 90% 83.9M 4s
486200K .......... .......... .......... .......... .......... 90% 53.4M 4s
486250K .......... .......... .......... .......... .......... 90%  131M 4s
486300K .......... .......... .......... .......... .......... 90% 64.7M 4s
486350K .......... .......... .......... .......... .......... 90% 61.1M 4s
486400K .......... .......... .......... .......... .......... 90% 65.8M 4s
486450K .......... .......... .......... .......... .......... 90% 85.4M 4s
486500K .......... .......... .......... .......... .......... 90% 54.2M 4s
486550K .......... .......... .......... .......... .......... 90%  114M 4s
486600K .......... .......... .......... .......... .......... 90% 49.6M 4s
486650K .......... .......... .......... .......... .......... 90% 53.6M 4s
486700K .......... .......... .......... .......... .......... 90% 72.4M 4s
486750K .......... .......... .......... .......... .......... 90% 98.6M 4s
486800K .......... .......... .......... .......... .......... 90% 72.7M 4s
486850K .......... .......... .......... .......... .......... 90% 66.0M 4s
486900K .......... .......... .......... .......... .......... 90% 44.6M 4s
486950K .......... .......... .......... .......... .......... 90% 87.7M 4s
487000K .......... .......... .......... .......... .......... 90% 33.2M 4s
487050K .......... .......... .......... .......... .......... 90% 94.1M 4s
487100K .......... .......... .......... .......... .......... 90% 44.4M 4s
487150K .......... .......... .......... .......... .......... 90% 88.5M 4s
487200K .......... .......... .......... .......... .......... 90% 68.4M 4s
487250K .......... .......... .......... .......... .......... 90% 58.8M 4s
487300K .......... .......... .......... .......... .......... 90%  136M 4s
487350K .......... .......... .......... .......... .......... 90% 36.4M 4s
487400K .......... .......... .......... .......... .......... 90%  103M 4s
487450K .......... .......... .......... .......... .......... 90% 40.8M 4s
487500K .......... .......... .......... .......... .......... 90%  106M 4s
487550K .......... .......... .......... .......... .......... 90%  102M 4s
487600K .......... .......... .......... .......... .......... 90% 67.3M 4s
487650K .......... .......... .......... .......... .......... 90%  100M 4s
487700K .......... .......... .......... .......... .......... 90% 88.3M 4s
487750K .......... .......... .......... .......... .......... 90% 43.9M 4s
487800K .......... .......... .......... .......... .......... 90%  123M 4s
487850K .......... .......... .......... .......... .......... 90% 28.3M 4s
487900K .......... .......... .......... .......... .......... 90%  101M 4s
487950K .......... .......... .......... .......... .......... 90%  105M 4s
488000K .......... .......... .......... .......... .......... 90%  138M 4s
488050K .......... .......... .......... .......... .......... 90%  124M 3s
488100K .......... .......... .......... .......... .......... 90%  103M 3s
488150K .......... .......... .......... .......... .......... 90%  125M 3s
488200K .......... .......... .......... .......... .......... 90% 80.6M 3s
488250K .......... .......... .......... .......... .......... 90% 66.3M 3s
488300K .......... .......... .......... .......... .......... 90% 87.3M 3s
488350K .......... .......... .......... .......... .......... 90% 78.6M 3s
488400K .......... .......... .......... .......... .......... 90% 65.9M 3s
488450K .......... .......... .......... .......... .......... 90% 60.1M 3s
488500K .......... .......... .......... .......... .......... 90% 78.1M 3s
488550K .......... .......... .......... .......... .......... 90%  104M 3s
488600K .......... .......... .......... .......... .......... 90% 66.9M 3s
488650K .......... .......... .......... .......... .......... 90% 89.4M 3s
488700K .......... .......... .......... .......... .......... 90% 95.2M 3s
488750K .......... .......... .......... .......... .......... 90% 44.2M 3s
488800K .......... .......... .......... .......... .......... 90% 83.8M 3s
488850K .......... .......... .......... .......... .......... 90% 41.1M 3s
488900K .......... .......... .......... .......... .......... 90%  137M 3s
488950K .......... .......... .......... .......... .......... 90% 49.0M 3s
489000K .......... .......... .......... .......... .......... 91%  130M 3s
489050K .......... .......... .......... .......... .......... 91% 42.5M 3s
489100K .......... .......... .......... .......... .......... 91%  101M 3s
489150K .......... .......... .......... .......... .......... 91% 87.5M 3s
489200K .......... .......... .......... .......... .......... 91% 74.4M 3s
489250K .......... .......... .......... .......... .......... 91% 58.8M 3s
489300K .......... .......... .......... .......... .......... 91% 74.2M 3s
489350K .......... .......... .......... .......... .......... 91% 43.4M 3s
489400K .......... .......... .......... .......... .......... 91%  111M 3s
489450K .......... .......... .......... .......... .......... 91% 81.5M 3s
489500K .......... .......... .......... .......... .......... 91% 75.9M 3s
489550K .......... .......... .......... .......... .......... 91% 98.2M 3s
489600K .......... .......... .......... .......... .......... 91% 85.4M 3s
489650K .......... .......... .......... .......... .......... 91% 50.0M 3s
489700K .......... .......... .......... .......... .......... 91% 87.8M 3s
489750K .......... .......... .......... .......... .......... 91% 47.0M 3s
489800K .......... .......... .......... .......... .......... 91% 78.6M 3s
489850K .......... .......... .......... .......... .......... 91% 91.3M 3s
489900K .......... .......... .......... .......... .......... 91% 77.8M 3s
489950K .......... .......... .......... .......... .......... 91% 98.2M 3s
490000K .......... .......... .......... .......... .......... 91% 62.6M 3s
490050K .......... .......... .......... .......... .......... 91% 92.1M 3s
490100K .......... .......... .......... .......... .......... 91% 39.6M 3s
490150K .......... .......... .......... .......... .......... 91% 90.6M 3s
490200K .......... .......... .......... .......... .......... 91% 91.8M 3s
490250K .......... .......... .......... .......... .......... 91% 51.1M 3s
490300K .......... .......... .......... .......... .......... 91%  101M 3s
490350K .......... .......... .......... .......... .......... 91% 58.6M 3s
490400K .......... .......... .......... .......... .......... 91%  101M 3s
490450K .......... .......... .......... .......... .......... 91% 46.5M 3s
490500K .......... .......... .......... .......... .......... 91% 84.3M 3s
490550K .......... .......... .......... .......... .......... 91% 95.2M 3s
490600K .......... .......... .......... .......... .......... 91% 89.8M 3s
490650K .......... .......... .......... .......... .......... 91%  109M 3s
490700K .......... .......... .......... .......... .......... 91% 88.5M 3s
490750K .......... .......... .......... .......... .......... 91% 52.7M 3s
490800K .......... .......... .......... .......... .......... 91% 92.7M 3s
490850K .......... .......... .......... .......... .......... 91% 82.9M 3s
490900K .......... .......... .......... .......... .......... 91%  104M 3s
490950K .......... .......... .......... .......... .......... 91% 26.2M 3s
491000K .......... .......... .......... .......... .......... 91%  121M 3s
491050K .......... .......... .......... .......... .......... 91%  128M 3s
491100K .......... .......... .......... .......... .......... 91% 99.6M 3s
491150K .......... .......... .......... .......... .......... 91%  139M 3s
491200K .......... .......... .......... .......... .......... 91% 65.6M 3s
491250K .......... .......... .......... .......... .......... 91%  105M 3s
491300K .......... .......... .......... .......... .......... 91%  218M 3s
491350K .......... .......... .......... .......... .......... 91% 83.6M 3s
491400K .......... .......... .......... .......... .......... 91% 70.7M 3s
491450K .......... .......... .......... .......... .......... 91% 36.4M 3s
491500K .......... .......... .......... .......... .......... 91% 87.2M 3s
491550K .......... .......... .......... .......... .......... 91% 71.8M 3s
491600K .......... .......... .......... .......... .......... 91% 48.8M 3s
491650K .......... .......... .......... .......... .......... 91% 47.5M 3s
491700K .......... .......... .......... .......... .......... 91% 82.2M 3s
491750K .......... .......... .......... .......... .......... 91% 39.4M 3s
491800K .......... .......... .......... .......... .......... 91% 48.3M 3s
491850K .......... .......... .......... .......... .......... 91% 62.1M 3s
491900K .......... .......... .......... .......... .......... 91% 38.0M 3s
491950K .......... .......... .......... .......... .......... 91% 39.7M 3s
492000K .......... .......... .......... .......... .......... 91% 86.4M 3s
492050K .......... .......... .......... .......... .......... 91% 40.6M 3s
492100K .......... .......... .......... .......... .......... 91% 98.2M 3s
492150K .......... .......... .......... .......... .......... 91% 51.0M 3s
492200K .......... .......... .......... .......... .......... 91% 63.7M 3s
492250K .......... .......... .......... .......... .......... 91% 66.7M 3s
492300K .......... .......... .......... .......... .......... 91% 52.8M 3s
492350K .......... .......... .......... .......... .......... 91% 53.8M 3s
492400K .......... .......... .......... .......... .......... 91% 75.8M 3s
492450K .......... .......... .......... .......... .......... 91% 55.3M 3s
492500K .......... .......... .......... .......... .......... 91% 57.6M 3s
492550K .......... .......... .......... .......... .......... 91% 82.2M 3s
492600K .......... .......... .......... .......... .......... 91% 36.7M 3s
492650K .......... .......... .......... .......... .......... 91%  110M 3s
492700K .......... .......... .......... .......... .......... 91% 50.8M 3s
492750K .......... .......... .......... .......... .......... 91% 61.1M 3s
492800K .......... .......... .......... .......... .......... 91% 91.4M 3s
492850K .......... .......... .......... .......... .......... 91% 57.0M 3s
492900K .......... .......... .......... .......... .......... 91% 69.7M 3s
492950K .......... .......... .......... .......... .......... 91% 48.1M 3s
493000K .......... .......... .......... .......... .......... 91% 63.3M 3s
493050K .......... .......... .......... .......... .......... 91% 77.8M 3s
493100K .......... .......... .......... .......... .......... 91% 41.6M 3s
493150K .......... .......... .......... .......... .......... 91% 96.9M 3s
493200K .......... .......... .......... .......... .......... 91% 61.7M 3s
493250K .......... .......... .......... .......... .......... 91% 54.0M 3s
493300K .......... .......... .......... .......... .......... 91%  119M 3s
493350K .......... .......... .......... .......... .......... 91% 46.5M 3s
493400K .......... .......... .......... .......... .......... 91%  125M 3s
493450K .......... .......... .......... .......... .......... 91% 94.3M 3s
493500K .......... .......... .......... .......... .......... 91% 47.5M 3s
493550K .......... .......... .......... .......... .......... 91%  129M 3s
493600K .......... .......... .......... .......... .......... 91%  105M 3s
493650K .......... .......... .......... .......... .......... 91% 72.4M 3s
493700K .......... .......... .......... .......... .......... 91%  101M 3s
493750K .......... .......... .......... .......... .......... 91% 97.1M 3s
493800K .......... .......... .......... .......... .......... 91% 91.3M 3s
493850K .......... .......... .......... .......... .......... 91%  105M 3s
493900K .......... .......... .......... .......... .......... 91% 79.7M 3s
493950K .......... .......... .......... .......... .......... 91%  106M 3s
494000K .......... .......... .......... .......... .......... 91% 97.9M 3s
494050K .......... .......... .......... .......... .......... 91% 62.4M 3s
494100K .......... .......... .......... .......... .......... 91%  121M 3s
494150K .......... .......... .......... .......... .......... 91%  131M 3s
494200K .......... .......... .......... .......... .......... 91% 77.6M 3s
494250K .......... .......... .......... .......... .......... 91% 80.7M 3s
494300K .......... .......... .......... .......... .......... 91%  105M 3s
494350K .......... .......... .......... .......... .......... 91% 89.9M 3s
494400K .......... .......... .......... .......... .......... 92%  103M 3s
494450K .......... .......... .......... .......... .......... 92% 80.0M 3s
494500K .......... .......... .......... .......... .......... 92%  108M 3s
494550K .......... .......... .......... .......... .......... 92%  114M 3s
494600K .......... .......... .......... .......... .......... 92% 93.7M 3s
494650K .......... .......... .......... .......... .......... 92% 93.5M 3s
494700K .......... .......... .......... .......... .......... 92% 90.3M 3s
494750K .......... .......... .......... .......... .......... 92%  110M 3s
494800K .......... .......... .......... .......... .......... 92% 80.7M 3s
494850K .......... .......... .......... .......... .......... 92% 57.6M 3s
494900K .......... .......... .......... .......... .......... 92%  121M 3s
494950K .......... .......... .......... .......... .......... 92% 94.1M 3s
495000K .......... .......... .......... .......... .......... 92% 54.4M 3s
495050K .......... .......... .......... .......... .......... 92%  104M 3s
495100K .......... .......... .......... .......... .......... 92%  105M 3s
495150K .......... .......... .......... .......... .......... 92%  128M 3s
495200K .......... .......... .......... .......... .......... 92% 81.1M 3s
495250K .......... .......... .......... .......... .......... 92% 79.1M 3s
495300K .......... .......... .......... .......... .......... 92%  120M 3s
495350K .......... .......... .......... .......... .......... 92% 62.7M 3s
495400K .......... .......... .......... .......... .......... 92%  101M 3s
495450K .......... .......... .......... .......... .......... 92%  106M 3s
495500K .......... .......... .......... .......... .......... 92%  101M 3s
495550K .......... .......... .......... .......... .......... 92% 91.8M 3s
495600K .......... .......... .......... .......... .......... 92% 81.1M 3s
495650K .......... .......... .......... .......... .......... 92%  118M 3s
495700K .......... .......... .......... .......... .......... 92% 82.8M 3s
495750K .......... .......... .......... .......... .......... 92%  119M 3s
495800K .......... .......... .......... .......... .......... 92% 64.1M 3s
495850K .......... .......... .......... .......... .......... 92%  107M 3s
495900K .......... .......... .......... .......... .......... 92%  127M 3s
495950K .......... .......... .......... .......... .......... 92% 59.6M 3s
496000K .......... .......... .......... .......... .......... 92%  109M 3s
496050K .......... .......... .......... .......... .......... 92%  118M 3s
496100K .......... .......... .......... .......... .......... 92% 81.9M 3s
496150K .......... .......... .......... .......... .......... 92%  124M 3s
496200K .......... .......... .......... .......... .......... 92% 47.9M 3s
496250K .......... .......... .......... .......... .......... 92%  105M 3s
496300K .......... .......... .......... .......... .......... 92%  122M 3s
496350K .......... .......... .......... .......... .......... 92% 84.3M 3s
496400K .......... .......... .......... .......... .......... 92% 96.7M 3s
496450K .......... .......... .......... .......... .......... 92%  114M 3s
496500K .......... .......... .......... .......... .......... 92% 64.2M 3s
496550K .......... .......... .......... .......... .......... 92% 87.8M 3s
496600K .......... .......... .......... .......... .......... 92%  104M 3s
496650K .......... .......... .......... .......... .......... 92% 51.3M 3s
496700K .......... .......... .......... .......... .......... 92% 95.9M 3s
496750K .......... .......... .......... .......... .......... 92%  105M 3s
496800K .......... .......... .......... .......... .......... 92% 91.3M 3s
496850K .......... .......... .......... .......... .......... 92% 54.5M 3s
496900K .......... .......... .......... .......... .......... 92%  105M 3s
496950K .......... .......... .......... .......... .......... 92% 61.8M 3s
497000K .......... .......... .......... .......... .......... 92%  100M 3s
497050K .......... .......... .......... .......... .......... 92%  101M 3s
497100K .......... .......... .......... .......... .......... 92% 83.3M 3s
497150K .......... .......... .......... .......... .......... 92%  105M 3s
497200K .......... .......... .......... .......... .......... 92% 70.4M 3s
497250K .......... .......... .......... .......... .......... 92% 98.0M 3s
497300K .......... .......... .......... .......... .......... 92% 78.4M 3s
497350K .......... .......... .......... .......... .......... 92% 81.4M 3s
497400K .......... .......... .......... .......... .......... 92% 97.3M 3s
497450K .......... .......... .......... .......... .......... 92% 23.5M 3s
497500K .......... .......... .......... .......... .......... 92%  154M 3s
497550K .......... .......... .......... .......... .......... 92%  103M 3s
497600K .......... .......... .......... .......... .......... 92% 98.6M 3s
497650K .......... .......... .......... .......... .......... 92%  105M 3s
497700K .......... .......... .......... .......... .......... 92%  115M 3s
497750K .......... .......... .......... .......... .......... 92%  125M 3s
497800K .......... .......... .......... .......... .......... 92%  136M 3s
497850K .......... .......... .......... .......... .......... 92% 88.6M 3s
497900K .......... .......... .......... .......... .......... 92% 64.2M 3s
497950K .......... .......... .......... .......... .......... 92% 56.2M 3s
498000K .......... .......... .......... .......... .......... 92% 89.6M 3s
498050K .......... .......... .......... .......... .......... 92% 71.9M 3s
498100K .......... .......... .......... .......... .......... 92% 91.1M 3s
498150K .......... .......... .......... .......... .......... 92% 68.1M 3s
498200K .......... .......... .......... .......... .......... 92% 95.6M 3s
498250K .......... .......... .......... .......... .......... 92% 41.9M 3s
498300K .......... .......... .......... .......... .......... 92%  118M 3s
498350K .......... .......... .......... .......... .......... 92% 55.1M 3s
498400K .......... .......... .......... .......... .......... 92%  127M 3s
498450K .......... .......... .......... .......... .......... 92% 48.0M 3s
498500K .......... .......... .......... .......... .......... 92% 91.8M 3s
498550K .......... .......... .......... .......... .......... 92%  130M 3s
498600K .......... .......... .......... .......... .......... 92% 38.0M 3s
498650K .......... .......... .......... .......... .......... 92%  107M 3s
498700K .......... .......... .......... .......... .......... 92% 68.0M 3s
498750K .......... .......... .......... .......... .......... 92% 68.7M 3s
498800K .......... .......... .......... .......... .......... 92% 96.3M 3s
498850K .......... .......... .......... .......... .......... 92% 46.3M 3s
498900K .......... .......... .......... .......... .......... 92% 93.2M 3s
498950K .......... .......... .......... .......... .......... 92% 99.4M 3s
499000K .......... .......... .......... .......... .......... 92% 53.7M 3s
499050K .......... .......... .......... .......... .......... 92% 86.3M 3s
499100K .......... .......... .......... .......... .......... 92% 95.2M 3s
499150K .......... .......... .......... .......... .......... 92% 49.5M 3s
499200K .......... .......... .......... .......... .......... 92% 82.1M 3s
499250K .......... .......... .......... .......... .......... 92% 54.4M 3s
499300K .......... .......... .......... .......... .......... 92% 92.7M 3s
499350K .......... .......... .......... .......... .......... 92% 93.4M 3s
499400K .......... .......... .......... .......... .......... 92% 62.7M 3s
499450K .......... .......... .......... .......... .......... 92% 93.0M 3s
499500K .......... .......... .......... .......... .......... 92% 42.9M 3s
499550K .......... .......... .......... .......... .......... 92%  134M 3s
499600K .......... .......... .......... .......... .......... 92% 42.3M 3s
499650K .......... .......... .......... .......... .......... 92%  114M 3s
499700K .......... .......... .......... .......... .......... 92% 57.4M 3s
499750K .......... .......... .......... .......... .......... 93% 89.1M 3s
499800K .......... .......... .......... .......... .......... 93% 24.4M 3s
499850K .......... .......... .......... .......... .......... 93% 99.4M 3s
499900K .......... .......... .......... .......... .......... 93%  119M 3s
499950K .......... .......... .......... .......... .......... 93% 87.2M 3s
500000K .......... .......... .......... .......... .......... 93% 83.6M 3s
500050K .......... .......... .......... .......... .......... 93%  125M 3s
500100K .......... .......... .......... .......... .......... 93% 41.8M 3s
500150K .......... .......... .......... .......... .......... 93% 49.1M 3s
500200K .......... .......... .......... .......... .......... 93% 51.3M 3s
500250K .......... .......... .......... .......... .......... 93% 85.1M 3s
500300K .......... .......... .......... .......... .......... 93% 67.3M 3s
500350K .......... .......... .......... .......... .......... 93% 65.4M 3s
500400K .......... .......... .......... .......... .......... 93% 46.4M 3s
500450K .......... .......... .......... .......... .......... 93% 68.9M 3s
500500K .......... .......... .......... .......... .......... 93% 65.5M 3s
500550K .......... .......... .......... .......... .......... 93% 47.3M 3s
500600K .......... .......... .......... .......... .......... 93% 79.7M 3s
500650K .......... .......... .......... .......... .......... 93% 42.5M 3s
500700K .......... .......... .......... .......... .......... 93% 63.7M 3s
500750K .......... .......... .......... .......... .......... 93%  124M 3s
500800K .......... .......... .......... .......... .......... 93% 50.6M 3s
500850K .......... .......... .......... .......... .......... 93% 43.5M 3s
500900K .......... .......... .......... .......... .......... 93% 73.5M 3s
500950K .......... .......... .......... .......... .......... 93% 57.2M 3s
501000K .......... .......... .......... .......... .......... 93% 65.0M 3s
501050K .......... .......... .......... .......... .......... 93% 96.3M 3s
501100K .......... .......... .......... .......... .......... 93% 47.9M 3s
501150K .......... .......... .......... .......... .......... 93% 46.4M 3s
501200K .......... .......... .......... .......... .......... 93% 98.6M 3s
501250K .......... .......... .......... .......... .......... 93% 42.3M 3s
501300K .......... .......... .......... .......... .......... 93% 52.3M 3s
501350K .......... .......... .......... .......... .......... 93% 67.3M 2s
501400K .......... .......... .......... .......... .......... 93% 46.3M 2s
501450K .......... .......... .......... .......... .......... 93% 36.8M 2s
501500K .......... .......... .......... .......... .......... 93% 93.2M 2s
501550K .......... .......... .......... .......... .......... 93% 40.3M 2s
501600K .......... .......... .......... .......... .......... 93% 35.0M 2s
501650K .......... .......... .......... .......... .......... 93%  114M 2s
501700K .......... .......... .......... .......... .......... 93% 37.7M 2s
501750K .......... .......... .......... .......... .......... 93%  108M 2s
501800K .......... .......... .......... .......... .......... 93% 37.1M 2s
501850K .......... .......... .......... .......... .......... 93% 38.0M 2s
501900K .......... .......... .......... .......... .......... 93%  103M 2s
501950K .......... .......... .......... .......... .......... 93% 47.0M 2s
502000K .......... .......... .......... .......... .......... 93% 73.6M 2s
502050K .......... .......... .......... .......... .......... 93% 99.6M 2s
502100K .......... .......... .......... .......... .......... 93% 89.9M 2s
502150K .......... .......... .......... .......... .......... 93% 43.8M 2s
502200K .......... .......... .......... .......... .......... 93% 99.4M 2s
502250K .......... .......... .......... .......... .......... 93% 69.3M 2s
502300K .......... .......... .......... .......... .......... 93%  111M 2s
502350K .......... .......... .......... .......... .......... 93% 85.8M 2s
502400K .......... .......... .......... .......... .......... 93% 25.7M 2s
502450K .......... .......... .......... .......... .......... 93% 72.7M 2s
502500K .......... .......... .......... .......... .......... 93%  130M 2s
502550K .......... .......... .......... .......... .......... 93%  140M 2s
502600K .......... .......... .......... .......... .......... 93%  101M 2s
502650K .......... .......... .......... .......... .......... 93%  158M 2s
502700K .......... .......... .......... .......... .......... 93% 86.9M 2s
502750K .......... .......... .......... .......... .......... 93% 57.6M 2s
502800K .......... .......... .......... .......... .......... 93%  174M 2s
502850K .......... .......... .......... .......... .......... 93%  164M 2s
502900K .......... .......... .......... .......... .......... 93% 40.2M 2s
502950K .......... .......... .......... .......... .......... 93%  126M 2s
503000K .......... .......... .......... .......... .......... 93%  138M 2s
503050K .......... .......... .......... .......... .......... 93% 74.3M 2s
503100K .......... .......... .......... .......... .......... 93% 29.6M 2s
503150K .......... .......... .......... .......... .......... 93%  117M 2s
503200K .......... .......... .......... .......... .......... 93% 73.0M 2s
503250K .......... .......... .......... .......... .......... 93%  123M 2s
503300K .......... .......... .......... .......... .......... 93%  123M 2s
503350K .......... .......... .......... .......... .......... 93% 65.9M 2s
503400K .......... .......... .......... .......... .......... 93% 92.8M 2s
503450K .......... .......... .......... .......... .......... 93% 71.9M 2s
503500K .......... .......... .......... .......... .......... 93% 96.3M 2s
503550K .......... .......... .......... .......... .......... 93% 74.4M 2s
503600K .......... .......... .......... .......... .......... 93% 49.1M 2s
503650K .......... .......... .......... .......... .......... 93% 75.5M 2s
503700K .......... .......... .......... .......... .......... 93% 72.7M 2s
503750K .......... .......... .......... .......... .......... 93%  105M 2s
503800K .......... .......... .......... .......... .......... 93% 52.6M 2s
503850K .......... .......... .......... .......... .......... 93%  101M 2s
503900K .......... .......... .......... .......... .......... 93% 52.3M 2s
503950K .......... .......... .......... .......... .......... 93% 76.9M 2s
504000K .......... .......... .......... .......... .......... 93% 95.4M 2s
504050K .......... .......... .......... .......... .......... 93% 79.0M 2s
504100K .......... .......... .......... .......... .......... 93%  100M 2s
504150K .......... .......... .......... .......... .......... 93%  142M 2s
504200K .......... .......... .......... .......... .......... 93% 41.1M 2s
504250K .......... .......... .......... .......... .......... 93%  109M 2s
504300K .......... .......... .......... .......... .......... 93%  150M 2s
504350K .......... .......... .......... .......... .......... 93% 88.1M 2s
504400K .......... .......... .......... .......... .......... 93%  104M 2s
504450K .......... .......... .......... .......... .......... 93%  126M 2s
504500K .......... .......... .......... .......... .......... 93% 34.6M 2s
504550K .......... .......... .......... .......... .......... 93%  130M 2s
504600K .......... .......... .......... .......... .......... 93% 92.0M 2s
504650K .......... .......... .......... .......... .......... 93%  101M 2s
504700K .......... .......... .......... .......... .......... 93% 96.7M 2s
504750K .......... .......... .......... .......... .......... 93% 12.2M 2s
504800K .......... .......... .......... .......... .......... 93%  112M 2s
504850K .......... .......... .......... .......... .......... 93% 94.4M 2s
504900K .......... .......... .......... .......... .......... 93% 86.9M 2s
504950K .......... .......... .......... .......... .......... 93% 88.6M 2s
505000K .......... .......... .......... .......... .......... 93%  166M 2s
505050K .......... .......... .......... .......... .......... 93%  158M 2s
505100K .......... .......... .......... .......... .......... 93%  140M 2s
505150K .......... .......... .......... .......... .......... 94%  184M 2s
505200K .......... .......... .......... .......... .......... 94% 83.5M 2s
505250K .......... .......... .......... .......... .......... 94%  130M 2s
505300K .......... .......... .......... .......... .......... 94%  164M 2s
505350K .......... .......... .......... .......... .......... 94% 73.4M 2s
505400K .......... .......... .......... .......... .......... 94%  142M 2s
505450K .......... .......... .......... .......... .......... 94% 85.5M 2s
505500K .......... .......... .......... .......... .......... 94%  115M 2s
505550K .......... .......... .......... .......... .......... 94%  128M 2s
505600K .......... .......... .......... .......... .......... 94%  146M 2s
505650K .......... .......... .......... .......... .......... 94%  118M 2s
505700K .......... .......... .......... .......... .......... 94% 87.0M 2s
505750K .......... .......... .......... .......... .......... 94% 57.7M 2s
505800K .......... .......... .......... .......... .......... 94% 94.6M 2s
505850K .......... .......... .......... .......... .......... 94% 43.6M 2s
505900K .......... .......... .......... .......... .......... 94% 98.6M 2s
505950K .......... .......... .......... .......... .......... 94% 99.9M 2s
506000K .......... .......... .......... .......... .......... 94% 64.1M 2s
506050K .......... .......... .......... .......... .......... 94% 91.8M 2s
506100K .......... .......... .......... .......... .......... 94% 42.4M 2s
506150K .......... .......... .......... .......... .......... 94%  104M 2s
506200K .......... .......... .......... .......... .......... 94%  101M 2s
506250K .......... .......... .......... .......... .......... 94% 56.1M 2s
506300K .......... .......... .......... .......... .......... 94% 93.5M 2s
506350K .......... .......... .......... .......... .......... 94% 98.4M 2s
506400K .......... .......... .......... .......... .......... 94% 88.1M 2s
506450K .......... .......... .......... .......... .......... 94% 80.4M 2s
506500K .......... .......... .......... .......... .......... 94% 71.2M 2s
506550K .......... .......... .......... .......... .......... 94%  111M 2s
506600K .......... .......... .......... .......... .......... 94% 83.2M 2s
506650K .......... .......... .......... .......... .......... 94% 39.6M 2s
506700K .......... .......... .......... .......... .......... 94%  102M 2s
506750K .......... .......... .......... .......... .......... 94%  121M 2s
506800K .......... .......... .......... .......... .......... 94% 75.9M 2s
506850K .......... .......... .......... .......... .......... 94%  103M 2s
506900K .......... .......... .......... .......... .......... 94% 69.8M 2s
506950K .......... .......... .......... .......... .......... 94%  105M 2s
507000K .......... .......... .......... .......... .......... 94% 42.2M 2s
507050K .......... .......... .......... .......... .......... 94% 97.5M 2s
507100K .......... .......... .......... .......... .......... 94%  103M 2s
507150K .......... .......... .......... .......... .......... 94% 65.0M 2s
507200K .......... .......... .......... .......... .......... 94%  101M 2s
507250K .......... .......... .......... .......... .......... 94%  114M 2s
507300K .......... .......... .......... .......... .......... 94% 75.2M 2s
507350K .......... .......... .......... .......... .......... 94% 94.3M 2s
507400K .......... .......... .......... .......... .......... 94% 73.2M 2s
507450K .......... .......... .......... .......... .......... 94% 68.3M 2s
507500K .......... .......... .......... .......... .......... 94% 93.4M 2s
507550K .......... .......... .......... .......... .......... 94%  132M 2s
507600K .......... .......... .......... .......... .......... 94% 63.6M 2s
507650K .......... .......... .......... .......... .......... 94%  111M 2s
507700K .......... .......... .......... .......... .......... 94% 40.2M 2s
507750K .......... .......... .......... .......... .......... 94%  128M 2s
507800K .......... .......... .......... .......... .......... 94% 86.0M 2s
507850K .......... .......... .......... .......... .......... 94% 30.0M 2s
507900K .......... .......... .......... .......... .......... 94%  144M 2s
507950K .......... .......... .......... .......... .......... 94% 92.1M 2s
508000K .......... .......... .......... .......... .......... 94%  110M 2s
508050K .......... .......... .......... .......... .......... 94%  108M 2s
508100K .......... .......... .......... .......... .......... 94% 93.7M 2s
508150K .......... .......... .......... .......... .......... 94% 97.7M 2s
508200K .......... .......... .......... .......... .......... 94% 54.7M 2s
508250K .......... .......... .......... .......... .......... 94% 81.8M 2s
508300K .......... .......... .......... .......... .......... 94% 47.9M 2s
508350K .......... .......... .......... .......... .......... 94% 88.5M 2s
508400K .......... .......... .......... .......... .......... 94% 60.1M 2s
508450K .......... .......... .......... .......... .......... 94% 77.9M 2s
508500K .......... .......... .......... .......... .......... 94% 43.1M 2s
508550K .......... .......... .......... .......... .......... 94% 99.4M 2s
508600K .......... .......... .......... .......... .......... 94% 48.4M 2s
508650K .......... .......... .......... .......... .......... 94% 91.8M 2s
508700K .......... .......... .......... .......... .......... 94% 48.1M 2s
508750K .......... .......... .......... .......... .......... 94% 82.6M 2s
508800K .......... .......... .......... .......... .......... 94% 68.5M 2s
508850K .......... .......... .......... .......... .......... 94% 41.4M 2s
508900K .......... .......... .......... .......... .......... 94% 70.0M 2s
508950K .......... .......... .......... .......... .......... 94% 80.8M 2s
509000K .......... .......... .......... .......... .......... 94% 95.9M 2s
509050K .......... .......... .......... .......... .......... 94% 58.1M 2s
509100K .......... .......... .......... .......... .......... 94% 83.5M 2s
509150K .......... .......... .......... .......... .......... 94% 62.3M 2s
509200K .......... .......... .......... .......... .......... 94% 45.8M 2s
509250K .......... .......... .......... .......... .......... 94% 93.5M 2s
509300K .......... .......... .......... .......... .......... 94% 50.3M 2s
509350K .......... .......... .......... .......... .......... 94% 94.8M 2s
509400K .......... .......... .......... .......... .......... 94% 39.1M 2s
509450K .......... .......... .......... .......... .......... 94% 83.6M 2s
509500K .......... .......... .......... .......... .......... 94% 28.1M 2s
509550K .......... .......... .......... .......... .......... 94%  104M 2s
509600K .......... .......... .......... .......... .......... 94% 50.2M 2s
509650K .......... .......... .......... .......... .......... 94%  106M 2s
509700K .......... .......... .......... .......... .......... 94% 49.5M 2s
509750K .......... .......... .......... .......... .......... 94% 83.8M 2s
509800K .......... .......... .......... .......... .......... 94% 57.3M 2s
509850K .......... .......... .......... .......... .......... 94% 40.5M 2s
509900K .......... .......... .......... .......... .......... 94%  113M 2s
509950K .......... .......... .......... .......... .......... 94% 51.4M 2s
510000K .......... .......... .......... .......... .......... 94% 84.5M 2s
510050K .......... .......... .......... .......... .......... 94% 49.4M 2s
510100K .......... .......... .......... .......... .......... 94% 82.2M 2s
510150K .......... .......... .......... .......... .......... 94% 29.3M 2s
510200K .......... .......... .......... .......... .......... 94%  100M 2s
510250K .......... .......... .......... .......... .......... 94% 66.0M 2s
510300K .......... .......... .......... .......... .......... 94% 73.4M 2s
510350K .......... .......... .......... .......... .......... 94%  116M 2s
510400K .......... .......... .......... .......... .......... 94% 59.8M 2s
510450K .......... .......... .......... .......... .......... 94% 89.6M 2s
510500K .......... .......... .......... .......... .......... 95% 70.1M 2s
510550K .......... .......... .......... .......... .......... 95% 58.9M 2s
510600K .......... .......... .......... .......... .......... 95% 78.4M 2s
510650K .......... .......... .......... .......... .......... 95% 97.1M 2s
510700K .......... .......... .......... .......... .......... 95% 71.1M 2s
510750K .......... .......... .......... .......... .......... 95% 98.0M 2s
510800K .......... .......... .......... .......... .......... 95%  161M 2s
510850K .......... .......... .......... .......... .......... 95% 39.9M 2s
510900K .......... .......... .......... .......... .......... 95%  112M 2s
510950K .......... .......... .......... .......... .......... 95% 70.3M 2s
511000K .......... .......... .......... .......... .......... 95% 79.3M 2s
511050K .......... .......... .......... .......... .......... 95% 96.9M 2s
511100K .......... .......... .......... .......... .......... 95% 75.6M 2s
511150K .......... .......... .......... .......... .......... 95% 89.3M 2s
511200K .......... .......... .......... .......... .......... 95% 47.7M 2s
511250K .......... .......... .......... .......... .......... 95%  117M 2s
511300K .......... .......... .......... .......... .......... 95%  130M 2s
511350K .......... .......... .......... .......... .......... 95% 99.0M 2s
511400K .......... .......... .......... .......... .......... 95% 61.6M 2s
511450K .......... .......... .......... .......... .......... 95%  104M 2s
511500K .......... .......... .......... .......... .......... 95% 85.4M 2s
511550K .......... .......... .......... .......... .......... 95% 94.1M 2s
511600K .......... .......... .......... .......... .......... 95% 81.4M 2s
511650K .......... .......... .......... .......... .......... 95% 47.1M 2s
511700K .......... .......... .......... .......... .......... 95% 78.9M 2s
511750K .......... .......... .......... .......... .......... 95%  123M 2s
511800K .......... .......... .......... .......... .......... 95% 87.5M 2s
511850K .......... .......... .......... .......... .......... 95% 58.8M 2s
511900K .......... .......... .......... .......... .......... 95%  108M 2s
511950K .......... .......... .......... .......... .......... 95% 69.0M 2s
512000K .......... .......... .......... .......... .......... 95% 52.3M 2s
512050K .......... .......... .......... .......... .......... 95% 93.4M 2s
512100K .......... .......... .......... .......... .......... 95% 52.3M 2s
512150K .......... .......... .......... .......... .......... 95% 88.5M 2s
512200K .......... .......... .......... .......... .......... 95% 78.1M 2s
512250K .......... .......... .......... .......... .......... 95% 85.4M 2s
512300K .......... .......... .......... .......... .......... 95%  133M 2s
512350K .......... .......... .......... .......... .......... 95% 39.4M 2s
512400K .......... .......... .......... .......... .......... 95% 98.8M 2s
512450K .......... .......... .......... .......... .......... 95% 78.5M 2s
512500K .......... .......... .......... .......... .......... 95% 26.8M 2s
512550K .......... .......... .......... .......... .......... 95% 87.0M 2s
512600K .......... .......... .......... .......... .......... 95%  107M 2s
512650K .......... .......... .......... .......... .......... 95%  117M 2s
512700K .......... .......... .......... .......... .......... 95%  117M 2s
512750K .......... .......... .......... .......... .......... 95% 63.4M 2s
512800K .......... .......... .......... .......... .......... 95%  161M 2s
512850K .......... .......... .......... .......... .......... 95%  106M 2s
512900K .......... .......... .......... .......... .......... 95% 78.1M 2s
512950K .......... .......... .......... .......... .......... 95%  121M 2s
513000K .......... .......... .......... .......... .......... 95% 42.7M 2s
513050K .......... .......... .......... .......... .......... 95% 73.1M 2s
513100K .......... .......... .......... .......... .......... 95% 49.5M 2s
513150K .......... .......... .......... .......... .......... 95% 88.1M 2s
513200K .......... .......... .......... .......... .......... 95% 48.9M 2s
513250K .......... .......... .......... .......... .......... 95% 78.0M 2s
513300K .......... .......... .......... .......... .......... 95% 73.1M 2s
513350K .......... .......... .......... .......... .......... 95% 33.6M 2s
513400K .......... .......... .......... .......... .......... 95% 76.1M 2s
513450K .......... .......... .......... .......... .......... 95% 51.1M 2s
513500K .......... .......... .......... .......... .......... 95% 39.6M 2s
513550K .......... .......... .......... .......... .......... 95% 40.0M 2s
513600K .......... .......... .......... .......... .......... 95% 78.0M 2s
513650K .......... .......... .......... .......... .......... 95% 45.5M 2s
513700K .......... .......... .......... .......... .......... 95% 35.8M 2s
513750K .......... .......... .......... .......... .......... 95% 91.1M 2s
513800K .......... .......... .......... .......... .......... 95% 30.0M 2s
513850K .......... .......... .......... .......... .......... 95% 84.2M 2s
513900K .......... .......... .......... .......... .......... 95% 50.7M 2s
513950K .......... .......... .......... .......... .......... 95% 9.36M 2s
514000K .......... .......... .......... .......... .......... 95% 75.1M 2s
514050K .......... .......... .......... .......... .......... 95%  107M 2s
514100K .......... .......... .......... .......... .......... 95%  121M 2s
514150K .......... .......... .......... .......... .......... 95%  109M 2s
514200K .......... .......... .......... .......... .......... 95% 57.0M 2s
514250K .......... .......... .......... .......... .......... 95% 91.8M 2s
514300K .......... .......... .......... .......... .......... 95% 72.3M 2s
514350K .......... .......... .......... .......... .......... 95% 82.6M 2s
514400K .......... .......... .......... .......... .......... 95% 82.8M 2s
514450K .......... .......... .......... .......... .......... 95% 51.0M 2s
514500K .......... .......... .......... .......... .......... 95% 58.8M 2s
514550K .......... .......... .......... .......... .......... 95% 43.1M 2s
514600K .......... .......... .......... .......... .......... 95% 48.0M 2s
514650K .......... .......... .......... .......... .......... 95% 65.8M 2s
514700K .......... .......... .......... .......... .......... 95% 38.8M 2s
514750K .......... .......... .......... .......... .......... 95%  117M 2s
514800K .......... .......... .......... .......... .......... 95% 40.7M 2s
514850K .......... .......... .......... .......... .......... 95%  107M 2s
514900K .......... .......... .......... .......... .......... 95% 97.5M 2s
514950K .......... .......... .......... .......... .......... 95% 50.8M 2s
515000K .......... .......... .......... .......... .......... 95% 47.1M 2s
515050K .......... .......... .......... .......... .......... 95%  101M 2s
515100K .......... .......... .......... .......... .......... 95% 84.2M 2s
515150K .......... .......... .......... .......... .......... 95%  102M 2s
515200K .......... .......... .......... .......... .......... 95% 83.6M 2s
515250K .......... .......... .......... .......... .......... 95%  120M 2s
515300K .......... .......... .......... .......... .......... 95% 90.9M 1s
515350K .......... .......... .......... .......... .......... 95% 37.8M 1s
515400K .......... .......... .......... .......... .......... 95%  103M 1s
515450K .......... .......... .......... .......... .......... 95% 82.3M 1s
515500K .......... .......... .......... .......... .......... 95%  121M 1s
515550K .......... .......... .......... .......... .......... 95%  101M 1s
515600K .......... .......... .......... .......... .......... 95% 54.5M 1s
515650K .......... .......... .......... .......... .......... 95%  130M 1s
515700K .......... .......... .......... .......... .......... 95% 63.7M 1s
515750K .......... .......... .......... .......... .......... 95%  108M 1s
515800K .......... .......... .......... .......... .......... 95%  119M 1s
515850K .......... .......... .......... .......... .......... 96% 19.4M 1s
515900K .......... .......... .......... .......... .......... 96%  173M 1s
515950K .......... .......... .......... .......... .......... 96%  141M 1s
516000K .......... .......... .......... .......... .......... 96%  142M 1s
516050K .......... .......... .......... .......... .......... 96%  189M 1s
516100K .......... .......... .......... .......... .......... 96%  157M 1s
516150K .......... .......... .......... .......... .......... 96%  121M 1s
516200K .......... .......... .......... .......... .......... 96% 98.4M 1s
516250K .......... .......... .......... .......... .......... 96%  110M 1s
516300K .......... .......... .......... .......... .......... 96%  131M 1s
516350K .......... .......... .......... .......... .......... 96% 69.0M 1s
516400K .......... .......... .......... .......... .......... 96%  109M 1s
516450K .......... .......... .......... .......... .......... 96% 47.1M 1s
516500K .......... .......... .......... .......... .......... 96% 81.4M 1s
516550K .......... .......... .......... .......... .......... 96% 98.0M 1s
516600K .......... .......... .......... .......... .......... 96% 57.6M 1s
516650K .......... .......... .......... .......... .......... 96% 95.0M 1s
516700K .......... .......... .......... .......... .......... 96% 85.5M 1s
516750K .......... .......... .......... .......... .......... 96% 19.6M 1s
516800K .......... .......... .......... .......... .......... 96% 93.0M 1s
516850K .......... .......... .......... .......... .......... 96%  127M 1s
516900K .......... .......... .......... .......... .......... 96%  113M 1s
516950K .......... .......... .......... .......... .......... 96%  110M 1s
517000K .......... .......... .......... .......... .......... 96% 98.4M 1s
517050K .......... .......... .......... .......... .......... 96%  120M 1s
517100K .......... .......... .......... .......... .......... 96% 90.4M 1s
517150K .......... .......... .......... .......... .......... 96% 40.4M 1s
517200K .......... .......... .......... .......... .......... 96% 36.9M 1s
517250K .......... .......... .......... .......... .......... 96% 86.4M 1s
517300K .......... .......... .......... .......... .......... 96% 18.1M 1s
517350K .......... .......... .......... .......... .......... 96%  145M 1s
517400K .......... .......... .......... .......... .......... 96%  117M 1s
517450K .......... .......... .......... .......... .......... 96%  113M 1s
517500K .......... .......... .......... .......... .......... 96% 49.7M 1s
517550K .......... .......... .......... .......... .......... 96% 57.1M 1s
517600K .......... .......... .......... .......... .......... 96% 47.0M 1s
517650K .......... .......... .......... .......... .......... 96% 92.1M 1s
517700K .......... .......... .......... .......... .......... 96% 30.9M 1s
517750K .......... .......... .......... .......... .......... 96%  102M 1s
517800K .......... .......... .......... .......... .......... 96% 48.2M 1s
517850K .......... .......... .......... .......... .......... 96% 33.7M 1s
517900K .......... .......... .......... .......... .......... 96% 35.0M 1s
517950K .......... .......... .......... .......... .......... 96% 96.9M 1s
518000K .......... .......... .......... .......... .......... 96% 51.3M 1s
518050K .......... .......... .......... .......... .......... 96% 49.6M 1s
518100K .......... .......... .......... .......... .......... 96% 88.8M 1s
518150K .......... .......... .......... .......... .......... 96% 52.3M 1s
518200K .......... .......... .......... .......... .......... 96% 39.3M 1s
518250K .......... .......... .......... .......... .......... 96% 79.0M 1s
518300K .......... .......... .......... .......... .......... 96% 51.0M 1s
518350K .......... .......... .......... .......... .......... 96% 36.0M 1s
518400K .......... .......... .......... .......... .......... 96%  101M 1s
518450K .......... .......... .......... .......... .......... 96% 38.8M 1s
518500K .......... .......... .......... .......... .......... 96% 71.2M 1s
518550K .......... .......... .......... .......... .......... 96% 53.0M 1s
518600K .......... .......... .......... .......... .......... 96% 42.1M 1s
518650K .......... .......... .......... .......... .......... 96%  107M 1s
518700K .......... .......... .......... .......... .......... 96% 35.5M 1s
518750K .......... .......... .......... .......... .......... 96% 40.1M 1s
518800K .......... .......... .......... .......... .......... 96%  116M 1s
518850K .......... .......... .......... .......... .......... 96% 44.7M 1s
518900K .......... .......... .......... .......... .......... 96% 73.8M 1s
518950K .......... .......... .......... .......... .......... 96% 53.7M 1s
519000K .......... .......... .......... .......... .......... 96% 52.0M 1s
519050K .......... .......... .......... .......... .......... 96% 96.9M 1s
519100K .......... .......... .......... .......... .......... 96% 95.7M 1s
519150K .......... .......... .......... .......... .......... 96% 79.9M 1s
519200K .......... .......... .......... .......... .......... 96% 81.8M 1s
519250K .......... .......... .......... .......... .......... 96%  122M 1s
519300K .......... .......... .......... .......... .......... 96%  100M 1s
519350K .......... .......... .......... .......... .......... 96% 37.3M 1s
519400K .......... .......... .......... .......... .......... 96%  133M 1s
519450K .......... .......... .......... .......... .......... 96% 51.5M 1s
519500K .......... .......... .......... .......... .......... 96%  140M 1s
519550K .......... .......... .......... .......... .......... 96% 88.8M 1s
519600K .......... .......... .......... .......... .......... 96% 75.5M 1s
519650K .......... .......... .......... .......... .......... 96%  137M 1s
519700K .......... .......... .......... .......... .......... 96% 73.2M 1s
519750K .......... .......... .......... .......... .......... 96%  104M 1s
519800K .......... .......... .......... .......... .......... 96% 92.1M 1s
519850K .......... .......... .......... .......... .......... 96% 82.3M 1s
519900K .......... .......... .......... .......... .......... 96% 84.9M 1s
519950K .......... .......... .......... .......... .......... 96%  114M 1s
520000K .......... .......... .......... .......... .......... 96% 75.5M 1s
520050K .......... .......... .......... .......... .......... 96% 90.9M 1s
520100K .......... .......... .......... .......... .......... 96% 98.0M 1s
520150K .......... .......... .......... .......... .......... 96% 84.8M 1s
520200K .......... .......... .......... .......... .......... 96% 88.9M 1s
520250K .......... .......... .......... .......... .......... 96%  114M 1s
520300K .......... .......... .......... .......... .......... 96% 74.4M 1s
520350K .......... .......... .......... .......... .......... 96% 77.0M 1s
520400K .......... .......... .......... .......... .......... 96% 56.4M 1s
520450K .......... .......... .......... .......... .......... 96%  103M 1s
520500K .......... .......... .......... .......... .......... 96%  126M 1s
520550K .......... .......... .......... .......... .......... 96% 40.7M 1s
520600K .......... .......... .......... .......... .......... 96% 73.9M 1s
520650K .......... .......... .......... .......... .......... 96%  117M 1s
520700K .......... .......... .......... .......... .......... 96% 73.9M 1s
520750K .......... .......... .......... .......... .......... 96% 82.3M 1s
520800K .......... .......... .......... .......... .......... 96%  117M 1s
520850K .......... .......... .......... .......... .......... 96% 44.6M 1s
520900K .......... .......... .......... .......... .......... 96%  132M 1s
520950K .......... .......... .......... .......... .......... 96% 70.6M 1s
521000K .......... .......... .......... .......... .......... 96% 59.1M 1s
521050K .......... .......... .......... .......... .......... 96% 95.0M 1s
521100K .......... .......... .......... .......... .......... 96% 87.8M 1s
521150K .......... .......... .......... .......... .......... 96% 99.4M 1s
521200K .......... .......... .......... .......... .......... 96% 68.9M 1s
521250K .......... .......... .......... .......... .......... 97%  129M 1s
521300K .......... .......... .......... .......... .......... 97%  108M 1s
521350K .......... .......... .......... .......... .......... 97% 39.9M 1s
521400K .......... .......... .......... .......... .......... 97%  128M 1s
521450K .......... .......... .......... .......... .......... 97% 67.3M 1s
521500K .......... .......... .......... .......... .......... 97% 74.8M 1s
521550K .......... .......... .......... .......... .......... 97%  112M 1s
521600K .......... .......... .......... .......... .......... 97% 30.9M 1s
521650K .......... .......... .......... .......... .......... 97% 13.0M 1s
521700K .......... .......... .......... .......... .......... 97% 77.6M 1s
521750K .......... .......... .......... .......... .......... 97%  180M 1s
521800K .......... .......... .......... .......... .......... 97%  138M 1s
521850K .......... .......... .......... .......... .......... 97%  130M 1s
521900K .......... .......... .......... .......... .......... 97% 86.6M 1s
521950K .......... .......... .......... .......... .......... 97%  103M 1s
522000K .......... .......... .......... .......... .......... 97%  132M 1s
522050K .......... .......... .......... .......... .......... 97%  110M 1s
522100K .......... .......... .......... .......... .......... 97%  108M 1s
522150K .......... .......... .......... .......... .......... 97%  132M 1s
522200K .......... .......... .......... .......... .......... 97% 89.9M 1s
522250K .......... .......... .......... .......... .......... 97%  152M 1s
522300K .......... .......... .......... .......... .......... 97% 74.2M 1s
522350K .......... .......... .......... .......... .......... 97% 93.2M 1s
522400K .......... .......... .......... .......... .......... 97% 54.4M 1s
522450K .......... .......... .......... .......... .......... 97% 42.5M 1s
522500K .......... .......... .......... .......... .......... 97% 96.5M 1s
522550K .......... .......... .......... .......... .......... 97% 93.4M 1s
522600K .......... .......... .......... .......... .......... 97% 78.3M 1s
522650K .......... .......... .......... .......... .......... 97% 2.41M 1s
522700K .......... .......... .......... .......... .......... 97% 88.0M 1s
522750K .......... .......... .......... .......... .......... 97%  118M 1s
522800K .......... .......... .......... .......... .......... 97%  119M 1s
522850K .......... .......... .......... .......... .......... 97% 80.7M 1s
522900K .......... .......... .......... .......... .......... 97%  126M 1s
522950K .......... .......... .......... .......... .......... 97%  109M 1s
523000K .......... .......... .......... .......... .......... 97%  135M 1s
523050K .......... .......... .......... .......... .......... 97%  120M 1s
523100K .......... .......... .......... .......... .......... 97%  111M 1s
523150K .......... .......... .......... .......... .......... 97%  111M 1s
523200K .......... .......... .......... .......... .......... 97% 43.9M 1s
523250K .......... .......... .......... .......... .......... 97%  152M 1s
523300K .......... .......... .......... .......... .......... 97%  109M 1s
523350K .......... .......... .......... .......... .......... 97%  114M 1s
523400K .......... .......... .......... .......... .......... 97%  114M 1s
523450K .......... .......... .......... .......... .......... 97% 42.9M 1s
523500K .......... .......... .......... .......... .......... 97% 44.6M 1s
523550K .......... .......... .......... .......... .......... 97% 90.9M 1s
523600K .......... .......... .......... .......... .......... 97% 49.1M 1s
523650K .......... .......... .......... .......... .......... 97% 84.6M 1s
523700K .......... .......... .......... .......... .......... 97% 30.3M 1s
523750K .......... .......... .......... .......... .......... 97% 68.3M 1s
523800K .......... .......... .......... .......... .......... 97% 55.2M 1s
523850K .......... .......... .......... .......... .......... 97% 65.3M 1s
523900K .......... .......... .......... .......... .......... 97% 69.5M 1s
523950K .......... .......... .......... .......... .......... 97% 44.6M 1s
524000K .......... .......... .......... .......... .......... 97% 43.1M 1s
524050K .......... .......... .......... .......... .......... 97% 99.2M 1s
524100K .......... .......... .......... .......... .......... 97% 51.7M 1s
524150K .......... .......... .......... .......... .......... 97% 82.6M 1s
524200K .......... .......... .......... .......... .......... 97% 62.8M 1s
524250K .......... .......... .......... .......... .......... 97% 62.4M 1s
524300K .......... .......... .......... .......... .......... 97% 79.7M 1s
524350K .......... .......... .......... .......... .......... 97% 35.6M 1s
524400K .......... .......... .......... .......... .......... 97% 86.0M 1s
524450K .......... .......... .......... .......... .......... 97% 58.1M 1s
524500K .......... .......... .......... .......... .......... 97% 64.9M 1s
524550K .......... .......... .......... .......... .......... 97% 81.2M 1s
524600K .......... .......... .......... .......... .......... 97% 36.0M 1s
524650K .......... .......... .......... .......... .......... 97% 56.0M 1s
524700K .......... .......... .......... .......... .......... 97% 69.8M 1s
524750K .......... .......... .......... .......... .......... 97% 44.6M 1s
524800K .......... .......... .......... .......... .......... 97%  119M 1s
524850K .......... .......... .......... .......... .......... 97% 35.0M 1s
524900K .......... .......... .......... .......... .......... 97% 42.6M 1s
524950K .......... .......... .......... .......... .......... 97% 92.8M 1s
525000K .......... .......... .......... .......... .......... 97% 31.3M 1s
525050K .......... .......... .......... .......... .......... 97% 38.7M 1s
525100K .......... .......... .......... .......... .......... 97% 74.1M 1s
525150K .......... .......... .......... .......... .......... 97% 31.2M 1s
525200K .......... .......... .......... .......... .......... 97% 84.5M 1s
525250K .......... .......... .......... .......... .......... 97% 39.5M 1s
525300K .......... .......... .......... .......... .......... 97%  132M 1s
525350K .......... .......... .......... .......... .......... 97% 77.1M 1s
525400K .......... .......... .......... .......... .......... 97% 53.0M 1s
525450K .......... .......... .......... .......... .......... 97% 96.1M 1s
525500K .......... .......... .......... .......... .......... 97% 49.6M 1s
525550K .......... .......... .......... .......... .......... 97% 97.3M 1s
525600K .......... .......... .......... .......... .......... 97%  113M 1s
525650K .......... .......... .......... .......... .......... 97% 54.8M 1s
525700K .......... .......... .......... .......... .......... 97%  101M 1s
525750K .......... .......... .......... .......... .......... 97% 84.5M 1s
525800K .......... .......... .......... .......... .......... 97%  114M 1s
525850K .......... .......... .......... .......... .......... 97% 77.3M 1s
525900K .......... .......... .......... .......... .......... 97% 90.1M 1s
525950K .......... .......... .......... .......... .......... 97% 72.7M 1s
526000K .......... .......... .......... .......... .......... 97% 91.1M 1s
526050K .......... .......... .......... .......... .......... 97% 90.4M 1s
526100K .......... .......... .......... .......... .......... 97% 67.7M 1s
526150K .......... .......... .......... .......... .......... 97%  118M 1s
526200K .......... .......... .......... .......... .......... 97% 88.1M 1s
526250K .......... .......... .......... .......... .......... 97% 69.4M 1s
526300K .......... .......... .......... .......... .......... 97%  138M 1s
526350K .......... .......... .......... .......... .......... 97% 54.2M 1s
526400K .......... .......... .......... .......... .......... 97% 93.4M 1s
526450K .......... .......... .......... .......... .......... 97%  105M 1s
526500K .......... .......... .......... .......... .......... 97% 67.5M 1s
526550K .......... .......... .......... .......... .......... 97%  107M 1s
526600K .......... .......... .......... .......... .......... 98% 79.1M 1s
526650K .......... .......... .......... .......... .......... 98% 97.5M 1s
526700K .......... .......... .......... .......... .......... 98% 94.3M 1s
526750K .......... .......... .......... .......... .......... 98% 69.9M 1s
526800K .......... .......... .......... .......... .......... 98%  131M 1s
526850K .......... .......... .......... .......... .......... 98% 62.0M 1s
526900K .......... .......... .......... .......... .......... 98% 89.3M 1s
526950K .......... .......... .......... .......... .......... 98%  115M 1s
527000K .......... .......... .......... .......... .......... 98% 58.8M 1s
527050K .......... .......... .......... .......... .......... 98%  184M 1s
527100K .......... .......... .......... .......... .......... 98% 89.6M 1s
527150K .......... .......... .......... .......... .......... 98% 82.5M 1s
527200K .......... .......... .......... .......... .......... 98% 63.6M 1s
527250K .......... .......... .......... .......... .......... 98% 96.9M 1s
527300K .......... .......... .......... .......... .......... 98% 80.8M 1s
527350K .......... .......... .......... .......... .......... 98%  105M 1s
527400K .......... .......... .......... .......... .......... 98%  104M 1s
527450K .......... .......... .......... .......... .......... 98% 36.0M 1s
527500K .......... .......... .......... .......... .......... 98% 97.7M 1s
527550K .......... .......... .......... .......... .......... 98% 65.0M 1s
527600K .......... .......... .......... .......... .......... 98% 82.1M 1s
527650K .......... .......... .......... .......... .......... 98%  123M 1s
527700K .......... .......... .......... .......... .......... 98% 92.5M 1s
527750K .......... .......... .......... .......... .......... 98%  105M 1s
527800K .......... .......... .......... .......... .......... 98%  111M 1s
527850K .......... .......... .......... .......... .......... 98% 62.4M 1s
527900K .......... .......... .......... .......... .......... 98%  121M 1s
527950K .......... .......... .......... .......... .......... 98% 38.8M 1s
528000K .......... .......... .......... .......... .......... 98%  103M 1s
528050K .......... .......... .......... .......... .......... 98% 87.2M 1s
528100K .......... .......... .......... .......... .......... 98% 95.4M 1s
528150K .......... .......... .......... .......... .......... 98% 52.7M 1s
528200K .......... .......... .......... .......... .......... 98% 92.8M 1s
528250K .......... .......... .......... .......... .......... 98% 38.3M 1s
528300K .......... .......... .......... .......... .......... 98%  104M 1s
528350K .......... .......... .......... .......... .......... 98% 91.1M 1s
528400K .......... .......... .......... .......... .......... 98%  102M 1s
528450K .......... .......... .......... .......... .......... 98% 93.7M 1s
528500K .......... .......... .......... .......... .......... 98% 96.7M 1s
528550K .......... .......... .......... .......... .......... 98% 88.0M 1s
528600K .......... .......... .......... .......... .......... 98% 62.2M 1s
528650K .......... .......... .......... .......... .......... 98% 42.6M 1s
528700K .......... .......... .......... .......... .......... 98% 92.1M 1s
528750K .......... .......... .......... .......... .......... 98% 87.3M 1s
528800K .......... .......... .......... .......... .......... 98% 74.7M 1s
528850K .......... .......... .......... .......... .......... 98% 87.8M 1s
528900K .......... .......... .......... .......... .......... 98% 73.6M 1s
528950K .......... .......... .......... .......... .......... 98% 42.1M 1s
529000K .......... .......... .......... .......... .......... 98%  108M 1s
529050K .......... .......... .......... .......... .......... 98% 88.6M 1s
529100K .......... .......... .......... .......... .......... 98% 48.3M 1s
529150K .......... .......... .......... .......... .......... 98%  154M 1s
529200K .......... .......... .......... .......... .......... 98% 69.8M 1s
529250K .......... .......... .......... .......... .......... 98% 72.2M 1s
529300K .......... .......... .......... .......... .......... 98%  103M 1s
529350K .......... .......... .......... .......... .......... 98% 31.5M 1s
529400K .......... .......... .......... .......... .......... 98%  138M 1s
529450K .......... .......... .......... .......... .......... 98% 67.0M 1s
529500K .......... .......... .......... .......... .......... 98% 88.3M 1s
529550K .......... .......... .......... .......... .......... 98%  100M 1s
529600K .......... .......... .......... .......... .......... 98% 79.0M 1s
529650K .......... .......... .......... .......... .......... 98% 39.0M 1s
529700K .......... .......... .......... .......... .......... 98%  110M 1s
529750K .......... .......... .......... .......... .......... 98% 91.3M 1s
529800K .......... .......... .......... .......... .......... 98% 86.9M 1s
529850K .......... .......... .......... .......... .......... 98% 73.6M 0s
529900K .......... .......... .......... .......... .......... 98% 22.2M 0s
529950K .......... .......... .......... .......... .......... 98%  101M 0s
530000K .......... .......... .......... .......... .......... 98%  124M 0s
530050K .......... .......... .......... .......... .......... 98%  116M 0s
530100K .......... .......... .......... .......... .......... 98% 70.9M 0s
530150K .......... .......... .......... .......... .......... 98%  110M 0s
530200K .......... .......... .......... .......... .......... 98% 37.1M 0s
530250K .......... .......... .......... .......... .......... 98%  125M 0s
530300K .......... .......... .......... .......... .......... 98% 40.6M 0s
530350K .......... .......... .......... .......... .......... 98% 42.7M 0s
530400K .......... .......... .......... .......... .......... 98%  115M 0s
530450K .......... .......... .......... .......... .......... 98% 63.0M 0s
530500K .......... .......... .......... .......... .......... 98%  105M 0s
530550K .......... .......... .......... .......... .......... 98% 61.0M 0s
530600K .......... .......... .......... .......... .......... 98% 36.3M 0s
530650K .......... .......... .......... .......... .......... 98%  122M 0s
530700K .......... .......... .......... .......... .......... 98% 45.3M 0s
530750K .......... .......... .......... .......... .......... 98% 86.9M 0s
530800K .......... .......... .......... .......... .......... 98% 41.0M 0s
530850K .......... .......... .......... .......... .......... 98% 57.4M 0s
530900K .......... .......... .......... .......... .......... 98% 55.4M 0s
530950K .......... .......... .......... .......... .......... 98% 85.1M 0s
531000K .......... .......... .......... .......... .......... 98% 56.3M 0s
531050K .......... .......... .......... .......... .......... 98% 93.4M 0s
531100K .......... .......... .......... .......... .......... 98% 45.0M 0s
531150K .......... .......... .......... .......... .......... 98%  132M 0s
531200K .......... .......... .......... .......... .......... 98% 32.7M 0s
531250K .......... .......... .......... .......... .......... 98%  107M 0s
531300K .......... .......... .......... .......... .......... 98% 43.3M 0s
531350K .......... .......... .......... .......... .......... 98% 74.5M 0s
531400K .......... .......... .......... .......... .......... 98% 53.0M 0s
531450K .......... .......... .......... .......... .......... 98% 36.8M 0s
531500K .......... .......... .......... .......... .......... 98% 88.1M 0s
531550K .......... .......... .......... .......... .......... 98% 95.7M 0s
531600K .......... .......... .......... .......... .......... 98% 65.5M 0s
531650K .......... .......... .......... .......... .......... 98% 46.9M 0s
531700K .......... .......... .......... .......... .......... 98% 39.0M 0s
531750K .......... .......... .......... .......... .......... 98% 84.5M 0s
531800K .......... .......... .......... .......... .......... 98% 39.4M 0s
531850K .......... .......... .......... .......... .......... 98%  110M 0s
531900K .......... .......... .......... .......... .......... 98% 44.1M 0s
531950K .......... .......... .......... .......... .......... 98%  107M 0s
532000K .......... .......... .......... .......... .......... 99% 56.0M 0s
532050K .......... .......... .......... .......... .......... 99%  102M 0s
532100K .......... .......... .......... .......... .......... 99% 70.7M 0s
532150K .......... .......... .......... .......... .......... 99% 44.5M 0s
532200K .......... .......... .......... .......... .......... 99% 91.1M 0s
532250K .......... .......... .......... .......... .......... 99% 57.2M 0s
532300K .......... .......... .......... .......... .......... 99%  109M 0s
532350K .......... .......... .......... .......... .......... 99%  119M 0s
532400K .......... .......... .......... .......... .......... 99% 73.8M 0s
532450K .......... .......... .......... .......... .......... 99% 72.9M 0s
532500K .......... .......... .......... .......... .......... 99%  126M 0s
532550K .......... .......... .......... .......... .......... 99%  122M 0s
532600K .......... .......... .......... .......... .......... 99% 52.1M 0s
532650K .......... .......... .......... .......... .......... 99% 68.7M 0s
532700K .......... .......... .......... .......... .......... 99% 59.8M 0s
532750K .......... .......... .......... .......... .......... 99% 81.4M 0s
532800K .......... .......... .......... .......... .......... 99%  107M 0s
532850K .......... .......... .......... .......... .......... 99% 72.7M 0s
532900K .......... .......... .......... .......... .......... 99% 97.5M 0s
532950K .......... .......... .......... .......... .......... 99%  103M 0s
533000K .......... .......... .......... .......... .......... 99% 43.9M 0s
533050K .......... .......... .......... .......... .......... 99% 65.1M 0s
533100K .......... .......... .......... .......... .......... 99%  102M 0s
533150K .......... .......... .......... .......... .......... 99% 62.0M 0s
533200K .......... .......... .......... .......... .......... 99%  108M 0s
533250K .......... .......... .......... .......... .......... 99% 94.1M 0s
533300K .......... .......... .......... .......... .......... 99% 93.4M 0s
533350K .......... .......... .......... .......... .......... 99% 54.1M 0s
533400K .......... .......... .......... .......... .......... 99% 82.1M 0s
533450K .......... .......... .......... .......... .......... 99% 56.1M 0s
533500K .......... .......... .......... .......... .......... 99%  101M 0s
533550K .......... .......... .......... .......... .......... 99%  102M 0s
533600K .......... .......... .......... .......... .......... 99% 36.0M 0s
533650K .......... .......... .......... .......... .......... 99%  134M 0s
533700K .......... .......... .......... .......... .......... 99%  113M 0s
533750K .......... .......... .......... .......... .......... 99%  132M 0s
533800K .......... .......... .......... .......... .......... 99%  157M 0s
533850K .......... .......... .......... .......... .......... 99% 50.1M 0s
533900K .......... .......... .......... .......... .......... 99%  116M 0s
533950K .......... .......... .......... .......... .......... 99% 49.2M 0s
534000K .......... .......... .......... .......... .......... 99%  112M 0s
534050K .......... .......... .......... .......... .......... 99% 57.6M 0s
534100K .......... .......... .......... .......... .......... 99% 80.6M 0s
534150K .......... .......... .......... .......... .......... 99% 47.0M 0s
534200K .......... .......... .......... .......... .......... 99% 61.6M 0s
534250K .......... .......... .......... .......... .......... 99%  121M 0s
534300K .......... .......... .......... .......... .......... 99% 69.8M 0s
534350K .......... .......... .......... .......... .......... 99% 81.0M 0s
534400K .......... .......... .......... .......... .......... 99% 90.4M 0s
534450K .......... .......... .......... .......... .......... 99% 56.9M 0s
534500K .......... .......... .......... .......... .......... 99%  100M 0s
534550K .......... .......... .......... .......... .......... 99% 44.8M 0s
534600K .......... .......... .......... .......... .......... 99% 89.4M 0s
534650K .......... .......... .......... .......... .......... 99% 85.5M 0s
534700K .......... .......... .......... .......... .......... 99% 58.0M 0s
534750K .......... .......... .......... .......... .......... 99%  105M 0s
534800K .......... .......... .......... .......... .......... 99% 35.7M 0s
534850K .......... .......... .......... .......... .......... 99% 77.1M 0s
534900K .......... .......... .......... .......... .......... 99% 56.1M 0s
534950K .......... .......... .......... .......... .......... 99% 88.3M 0s
535000K .......... .......... .......... .......... .......... 99% 37.1M 0s
535050K .......... .......... .......... .......... .......... 99%  136M 0s
535100K .......... .......... .......... .......... .......... 99% 43.2M 0s
535150K .......... .......... .......... .......... .......... 99%  108M 0s
535200K .......... .......... .......... .......... .......... 99% 38.6M 0s
535250K .......... .......... .......... .......... .......... 99%  131M 0s
535300K .......... .......... .......... .......... .......... 99% 53.4M 0s
535350K .......... .......... .......... .......... .......... 99% 99.6M 0s
535400K .......... .......... .......... .......... .......... 99% 75.6M 0s
535450K .......... .......... .......... .......... .......... 99% 88.3M 0s
535500K .......... .......... .......... .......... .......... 99% 58.5M 0s
535550K .......... .......... .......... .......... .......... 99% 60.2M 0s
535600K .......... .......... .......... .......... .......... 99% 61.0M 0s
535650K .......... .......... .......... .......... .......... 99% 68.3M 0s
535700K .......... .......... .......... .......... .......... 99% 71.6M 0s
535750K .......... .......... .......... .......... .......... 99% 98.0M 0s
535800K .......... .......... .......... .......... .......... 99% 91.1M 0s
535850K .......... .......... .......... .......... .......... 99% 17.9M 0s
535900K .......... .......... .......... .......... .......... 99% 63.1M 0s
535950K .......... .......... .......... .......... .......... 99% 82.8M 0s
536000K .......... .......... .......... .......... .......... 99% 84.6M 0s
536050K .......... .......... .......... .......... .......... 99%  142M 0s
536100K .......... .......... .......... .......... .......... 99% 91.6M 0s
536150K .......... .......... .......... .......... .......... 99% 93.2M 0s
536200K .......... .......... .......... .......... .......... 99%  104M 0s
536250K .......... .......... .......... .......... .......... 99% 75.1M 0s
536300K .......... .......... .......... .......... .......... 99% 60.6M 0s
536350K .......... .......... .......... .......... .......... 99% 34.2M 0s
536400K .......... .......... .......... .......... .......... 99% 46.8M 0s
536450K .......... .......... .......... .......... .......... 99% 53.3M 0s
536500K .......... .......... .......... .......... .......... 99% 93.7M 0s
536550K .......... .......... .......... .......... .......... 99% 62.3M 0s
536600K .......... .......... .......... .......... .......... 99% 34.1M 0s
536650K .......... .......... .......... .......... .......... 99% 36.8M 0s
536700K .......... .......... .......... .......... .......... 99% 40.4M 0s
536750K .......... .......... .......... .......... .......... 99%  116M 0s
536800K .......... .......... .......... .......... .......... 99% 42.9M 0s
536850K .......... .......... .......... .......... .......... 99% 52.2M 0s
536900K .......... .......... .......... .......... .......... 99% 93.4M 0s
536950K .......... .......... .......... .......... .......... 99% 63.6M 0s
537000K .......... .......... .......... .......... .......... 99% 76.4M 0s
537050K .......... .......... .......... .......... .......... 99% 50.8M 0s
537100K .......... .......... .......... .......... .......... 99% 79.7M 0s
537150K .......... .......... .......... .......... .......... 99% 44.9M 0s
537200K .......... .......... .......... .......... .......... 99% 36.1M 0s
537250K .......... .......... .......... .......... .......... 99%  115M 0s
537300K .......... .......... .......... .......... .......... 99% 42.4M 0s
537350K .......... .......... .......... .......... .....     100% 52.4M=35s

2024-03-06 20:31:18 (14.8 MB/s) - ‘ESPbeta-macos-x86_64.tgz’ saved [550292565/550292565]

+ tar -xf ESPbeta-macos-x86_64.tgz
+ cd ESPbeta
+ rm -rf /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Slugs
++ uname -a
+ [[ Darwin macys.mit.edu 22.6.0 Darwin Kernel Version 22.6.0: Tue Nov  7 21:48:06 PST 2023; root:xnu-8796.141.3.702.9~2/RELEASE_X86_64 x86_64 == *\D\a\r\w\i\n* ]]
+ ./setup.command
Custom icon assigned to '/Users/jenkins/Desktop/ESP125.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/esp_logo.png'.
Custom icon assigned to '/Users/jenkins/Desktop/runESP125.command' based on '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/ESP/esp_logo.png'.
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/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/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/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/mpicc'
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/parkill'
Patching '/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/bin/mpicxx'
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/mpifort'
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/mpicc'
Patching 'bin/mpicxx'
Patching 'bin/mpifort'
Patching 'lib/pkgconfig/mpich.pc'
+ 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:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=.:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin:/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/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:/usr/local/opt/python/libexec/bin:/usr/local/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONINC=/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/Python-3.11.6/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 macys.mit.edu 22.6.0 Darwin Kernel Version 22.6.0: Tue Nov  7 21:48:06 PST 2023; root:xnu-8796.141.3.702.9~2/RELEASE_X86_64 x86_64 == *\D\a\r\w\i\n* ]]
+ sed -i '' '/.*capsExamples.*/d' /Users/jenkins/workspace/ESP_bPreBuilt/Verification.sh
+ bash -ex /Users/jenkins/workspace/ESP_bPreBuilt/Verification.sh
+ expectSuccess 01 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/verify_7.8.0/expressions.vfy", so verification is being skipped
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000152 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:169]]
        ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,0,999)"
ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set)
    --> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000158 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:176]]
        ibeg must be be between 1 and strlen(str) when evaluating "slice(e3,14,999)"
ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set)
    --> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (func_arg_out_of_bounds) in Branch Brch_000164 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:183]]
        iend must not be less than ibeg when evaluating "slice(e3,4,-1)"
ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set)
    --> catching signal -258 (func_arg_out_of_bounds)
ERROR:: (illegal_pmtr_index) in Branch Brch_000317 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:384]]
        index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000332 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:402]]
        index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000346 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:418]]
        row index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000360 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:434]]
        row index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000367 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:442]]
        row index must be between 1 and 2
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000374 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:450]]
        column index must be between 1 and 3
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (illegal_pmtr_index) in Branch Brch_000381 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:458]]
        column index must be between 1 and 3
    --> catching signal -262 (illegal_pmtr_index)
ERROR:: (UNKNOWN) in Branch Brch_001805 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:1914]]
        signal 1 thrown by user
    --> catching signal 1 (UNKNOWN)
ERROR:: (illegal_value) in Branch Brch_001813 at [[/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/basic/expressions.csm:1924]]
        vertex and base must be different
    --> catching signal -225 (illegal_value)
==> serveESP completed successfully with no verification data

real	0m4.025s
user	0m0.283s
sys	0m0.021s
+ set +x

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

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

real	0m0.432s
user	0m0.471s
sys	0m0.043s
+ 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	0m1.764s
user	0m2.933s
sys	0m0.757s
+ 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	0m0.611s
user	0m0.666s
sys	0m0.059s
+ 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	0m0.560s
user	0m0.732s
sys	0m0.073s
+ 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	0m0.611s
user	0m0.783s
sys	0m0.042s
+ set +x

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

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

real	0m2.845s
user	0m5.022s
sys	0m0.663s
+ 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	0m16.655s
user	0m32.013s
sys	0m2.303s
+ 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	0m0.604s
user	0m0.718s
sys	0m0.034s
+ 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	0m19.438s
user	1m20.618s
sys	0m25.786s
+ 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	0m0.626s
user	0m0.431s
sys	0m0.042s
+ set +x

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

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

real	0m0.568s
user	0m0.755s
sys	0m0.016s
+ 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	0m0.356s
user	0m0.383s
sys	0m0.016s
+ 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	0m0.589s
user	0m0.543s
sys	0m0.021s
+ 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 1.537s

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

real	0m4.812s
user	0m7.141s
sys	0m0.201s
++ 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 = 155
	Number of elements = 306
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 306
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 298
	Combined Number of elements = 588
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 588
	Combined Elemental Quad4 = 0

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

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

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

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

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

----------------------------------------------------------------------
Ran 100 tests in 29.099s

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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.038   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          =     0.007   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4280      6316
AFLR2 GG : Nodes, Faces      =      6142     10040
AFLR2 GG : Nodes, Faces      =      7878     13512
AFLR2 GG : Nodes, Faces      =      9457     16670
AFLR2 GG : Nodes, Faces      =     10755     19266
AFLR2 GG : Nodes, Faces      =     11958     21672
AFLR2 GG : Nodes, Faces      =     13085     23926
AFLR2 GG : Nodes, Faces      =     14138     26032
AFLR2 GG : Nodes, Faces      =     15126     28008
AFLR2 GG : Nodes, Faces      =     16046     29848
AFLR2 GG : Nodes, Faces      =     16885     31526
AFLR2 GG : Nodes, Faces      =     17661     33078
AFLR2 GG : Nodes, Faces      =     18384     34524
AFLR2 GG : Nodes, Faces      =     19043     35842
AFLR2 GG : Nodes, Faces      =     19652     37060
AFLR2 GG : Nodes, Faces      =     20219     38194
AFLR2 GG : Nodes, Faces      =     20752     39260
AFLR2 GG : Nodes, Faces      =     21255     40266
AFLR2 GG : Nodes, Faces      =     21709     41174
AFLR2 GG : Nodes, Faces      =     22137     42030
AFLR2 GG : Nodes, Faces      =     22527     42810
AFLR2 GG : Nodes, Faces      =     22881     43518
AFLR2 GG : Nodes, Faces      =     23170     44096
AFLR2 GG : Nodes, Faces      =     23413     44582
AFLR2 GG : Nodes, Faces      =     23626     45008
AFLR2 GG : Nodes, Faces      =     23816     45388
AFLR2 GG : Nodes, Faces      =     23971     45698
AFLR2 GG : Nodes, Faces      =     24067     45890
AFLR2 GG : Nodes, Faces      =     24162     46080
AFLR2 GG : Nodes, Faces      =     24254     46264
AFLR2 GG : Nodes, Faces      =     24329     46414
AFLR2 GG : Nodes, Faces      =     24383     46522
AFLR2 GG : Nodes, Faces      =     24422     46600
AFLR2 GG : Nodes, Faces      =     24441     46638
AFLR2 GG : Nodes, Faces      =     24449     46654
AFLR2 GG : Nodes, Faces      =     24450     46656
 
AFLR2    : CPU Time          =     0.055   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     24450     46656
 
AFLR2    : CPU Time          =     0.098   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 24450
Number of elements = 48900
Number of tris = 46656
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          =     0.008   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4121      6018
AFLR2 GG : Nodes, Faces      =      5676      9128
AFLR2 GG : Nodes, Faces      =      6930     11636
AFLR2 GG : Nodes, Faces      =      8008     13792
AFLR2 GG : Nodes, Faces      =      8945     15666
AFLR2 GG : Nodes, Faces      =      9742     17260
AFLR2 GG : Nodes, Faces      =     10427     18630
AFLR2 GG : Nodes, Faces      =     11007     19790
AFLR2 GG : Nodes, Faces      =     11514     20804
AFLR2 GG : Nodes, Faces      =     11940     21656
AFLR2 GG : Nodes, Faces      =     12314     22404
AFLR2 GG : Nodes, Faces      =     12630     23036
AFLR2 GG : Nodes, Faces      =     12902     23580
AFLR2 GG : Nodes, Faces      =     13117     24010
AFLR2 GG : Nodes, Faces      =     13293     24362
AFLR2 GG : Nodes, Faces      =     13417     24610
AFLR2 GG : Nodes, Faces      =     13516     24808
AFLR2 GG : Nodes, Faces      =     13581     24938
AFLR2 GG : Nodes, Faces      =     13623     25022
AFLR2 GG : Nodes, Faces      =     13649     25074
AFLR2 GG : Nodes, Faces      =     13660     25096
AFLR2 GG : Nodes, Faces      =     13664     25104
 
AFLR2    : CPU Time          =     0.029   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     13664     25104
 
AFLR2    : CPU Time          =     0.002   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 13664
Number of elements = 27328
Number of tris = 25104
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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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          =     0.007   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4280      6316
AFLR2 GG : Nodes, Faces      =      6142     10040
AFLR2 GG : Nodes, Faces      =      7878     13512
AFLR2 GG : Nodes, Faces      =      9457     16670
AFLR2 GG : Nodes, Faces      =     10755     19266
AFLR2 GG : Nodes, Faces      =     11958     21672
AFLR2 GG : Nodes, Faces      =     13085     23926
AFLR2 GG : Nodes, Faces      =     14138     26032
AFLR2 GG : Nodes, Faces      =     15126     28008
AFLR2 GG : Nodes, Faces      =     16046     29848
AFLR2 GG : Nodes, Faces      =     16885     31526
AFLR2 GG : Nodes, Faces      =     17661     33078
AFLR2 GG : Nodes, Faces      =     18384     34524
AFLR2 GG : Nodes, Faces      =     19043     35842
AFLR2 GG : Nodes, Faces      =     19652     37060
AFLR2 GG : Nodes, Faces      =     20219     38194
AFLR2 GG : Nodes, Faces      =     20752     39260
AFLR2 GG : Nodes, Faces      =     21255     40266
AFLR2 GG : Nodes, Faces      =     21709     41174
AFLR2 GG : Nodes, Faces      =     22137     42030
AFLR2 GG : Nodes, Faces      =     22527     42810
AFLR2 GG : Nodes, Faces      =     22881     43518
AFLR2 GG : Nodes, Faces      =     23170     44096
AFLR2 GG : Nodes, Faces      =     23413     44582
AFLR2 GG : Nodes, Faces      =     23626     45008
AFLR2 GG : Nodes, Faces      =     23816     45388
AFLR2 GG : Nodes, Faces      =     23971     45698
AFLR2 GG : Nodes, Faces      =     24067     45890
AFLR2 GG : Nodes, Faces      =     24162     46080
AFLR2 GG : Nodes, Faces      =     24254     46264
AFLR2 GG : Nodes, Faces      =     24329     46414
AFLR2 GG : Nodes, Faces      =     24383     46522
AFLR2 GG : Nodes, Faces      =     24422     46600
AFLR2 GG : Nodes, Faces      =     24441     46638
AFLR2 GG : Nodes, Faces      =     24449     46654
AFLR2 GG : Nodes, Faces      =     24450     46656
 
AFLR2    : CPU Time          =     0.056   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     24450     46656
 
AFLR2    : CPU Time          =     0.004   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 24450
Number of elements = 48900
Number of tris = 46656
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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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          =     0.007   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4121      6018
AFLR2 GG : Nodes, Faces      =      5676      9128
AFLR2 GG : Nodes, Faces      =      6930     11636
AFLR2 GG : Nodes, Faces      =      8008     13792
AFLR2 GG : Nodes, Faces      =      8945     15666
AFLR2 GG : Nodes, Faces      =      9742     17260
AFLR2 GG : Nodes, Faces      =     10427     18630
AFLR2 GG : Nodes, Faces      =     11007     19790
AFLR2 GG : Nodes, Faces      =     11514     20804
AFLR2 GG : Nodes, Faces      =     11940     21656
AFLR2 GG : Nodes, Faces      =     12314     22404
AFLR2 GG : Nodes, Faces      =     12630     23036
AFLR2 GG : Nodes, Faces      =     12902     23580
AFLR2 GG : Nodes, Faces      =     13117     24010
AFLR2 GG : Nodes, Faces      =     13293     24362
AFLR2 GG : Nodes, Faces      =     13417     24610
AFLR2 GG : Nodes, Faces      =     13516     24808
AFLR2 GG : Nodes, Faces      =     13581     24938
AFLR2 GG : Nodes, Faces      =     13623     25022
AFLR2 GG : Nodes, Faces      =     13649     25074
AFLR2 GG : Nodes, Faces      =     13660     25096
AFLR2 GG : Nodes, Faces      =     13664     25104
 
AFLR2    : CPU Time          =     0.029   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     13664     25104
 
AFLR2    : CPU Time          =     0.003   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 13664
Number of elements = 27328
Number of tris = 25104
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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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          =     0.007   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4280      6316
AFLR2 GG : Nodes, Faces      =      6142     10040
AFLR2 GG : Nodes, Faces      =      7878     13512
AFLR2 GG : Nodes, Faces      =      9457     16670
AFLR2 GG : Nodes, Faces      =     10755     19266
AFLR2 GG : Nodes, Faces      =     11958     21672
AFLR2 GG : Nodes, Faces      =     13085     23926
AFLR2 GG : Nodes, Faces      =     14138     26032
AFLR2 GG : Nodes, Faces      =     15126     28008
AFLR2 GG : Nodes, Faces      =     16046     29848
AFLR2 GG : Nodes, Faces      =     16885     31526
AFLR2 GG : Nodes, Faces      =     17661     33078
AFLR2 GG : Nodes, Faces      =     18384     34524
AFLR2 GG : Nodes, Faces      =     19043     35842
AFLR2 GG : Nodes, Faces      =     19652     37060
AFLR2 GG : Nodes, Faces      =     20219     38194
AFLR2 GG : Nodes, Faces      =     20752     39260
AFLR2 GG : Nodes, Faces      =     21255     40266
AFLR2 GG : Nodes, Faces      =     21709     41174
AFLR2 GG : Nodes, Faces      =     22137     42030
AFLR2 GG : Nodes, Faces      =     22527     42810
AFLR2 GG : Nodes, Faces      =     22881     43518
AFLR2 GG : Nodes, Faces      =     23170     44096
AFLR2 GG : Nodes, Faces      =     23413     44582
AFLR2 GG : Nodes, Faces      =     23626     45008
AFLR2 GG : Nodes, Faces      =     23816     45388
AFLR2 GG : Nodes, Faces      =     23971     45698
AFLR2 GG : Nodes, Faces      =     24067     45890
AFLR2 GG : Nodes, Faces      =     24162     46080
AFLR2 GG : Nodes, Faces      =     24254     46264
AFLR2 GG : Nodes, Faces      =     24329     46414
AFLR2 GG : Nodes, Faces      =     24383     46522
AFLR2 GG : Nodes, Faces      =     24422     46600
AFLR2 GG : Nodes, Faces      =     24441     46638
AFLR2 GG : Nodes, Faces      =     24449     46654
AFLR2 GG : Nodes, Faces      =     24450     46656
 
AFLR2    : CPU Time          =     0.052   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     24450     46656
 
AFLR2    : CPU Time          =     0.004   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 24450
Number of elements = 48900
Number of tris = 46656
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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       316       634
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 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          =     0.010   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      6876     13408
 
AFLR2    : CPU Time          =     0.002   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          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       681      1018
AFLR2 GGp: Nodes, Faces      =      1013      1682
AFLR2 GGp: Nodes, Faces      =      1339      2334
AFLR2 GGp: Nodes, Faces      =      1652      2960
AFLR2 GGp: Nodes, Faces      =      1957      3570
AFLR2 GGp: Nodes, Faces      =      2252      4160
AFLR2 GGp: Nodes, Faces      =      2526      4708
AFLR2 GGp: Nodes, Faces      =      2809      5274
AFLR2 GGp: Nodes, Faces      =      3083      5822
AFLR2 GGp: Nodes, Faces      =      3327      6310
AFLR2 GGp: Nodes, Faces      =      3564      6784
AFLR2 GGp: Nodes, Faces      =      3788      7232
AFLR2 GGp: Nodes, Faces      =      3995      7646
AFLR2 GGp: Nodes, Faces      =      4194      8044
AFLR2 GGp: Nodes, Faces      =      4394      8444
AFLR2 GGp: Nodes, Faces      =      4585      8826
AFLR2 GGp: Nodes, Faces      =      4772      9200
AFLR2 GGp: Nodes, Faces      =      4943      9542
AFLR2 GGp: Nodes, Faces      =      5129      9914
AFLR2 GGp: Nodes, Faces      =      5293     10242
AFLR2 GGp: Nodes, Faces      =      5447     10550
AFLR2 GGp: Nodes, Faces      =      5594     10844
AFLR2 GGp: Nodes, Faces      =      5716     11088
AFLR2 GGp: Nodes, Faces      =      5830     11316
AFLR2 GGp: Nodes, Faces      =      5909     11474
AFLR2 GGp: Nodes, Faces      =      5964     11584
AFLR2 GGp: Nodes, Faces      =      6006     11668
AFLR2 GGp: Nodes, Faces      =      6025     11706
AFLR2 GGp: Nodes, Faces      =      6034     11724
 
AFLR2    : CPU Time          =     0.015   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      6034     11724
AFLR2 QI : Nodes, Faces      =      6033       454
AFLR2 QI : Nodes, Faces      =      6033      5634
AFLR2 QI : Nodes, Faces      =      6033     11722
AFLR2 QI : Nodes, Faces      =      6032       462
AFLR2 QI : Nodes, Faces      =      6032      5629
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       456
AFLR2 QI : Nodes, Faces      =      6032      5632
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       474
AFLR2 QI : Nodes, Faces      =      6032      5623
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6031       486
AFLR2 QI : Nodes, Faces      =      6031      5616
AFLR2 QI : Nodes, Faces      =      6031       488
AFLR2 QI : Nodes, Faces      =      6031      5616
 
AFLR2    : CPU Time          =     0.007   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

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

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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       316       634
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       681      1018
AFLR2 GGp: Nodes, Faces      =      1013      1682
AFLR2 GGp: Nodes, Faces      =      1339      2334
AFLR2 GGp: Nodes, Faces      =      1652      2960
AFLR2 GGp: Nodes, Faces      =      1957      3570
AFLR2 GGp: Nodes, Faces      =      2252      4160
AFLR2 GGp: Nodes, Faces      =      2526      4708
AFLR2 GGp: Nodes, Faces      =      2809      5274
AFLR2 GGp: Nodes, Faces      =      3083      5822
AFLR2 GGp: Nodes, Faces      =      3327      6310
AFLR2 GGp: Nodes, Faces      =      3564      6784
AFLR2 GGp: Nodes, Faces      =      3788      7232
AFLR2 GGp: Nodes, Faces      =      3995      7646
AFLR2 GGp: Nodes, Faces      =      4194      8044
AFLR2 GGp: Nodes, Faces      =      4394      8444
AFLR2 GGp: Nodes, Faces      =      4585      8826
AFLR2 GGp: Nodes, Faces      =      4772      9200
AFLR2 GGp: Nodes, Faces      =      4943      9542
AFLR2 GGp: Nodes, Faces      =      5129      9914
AFLR2 GGp: Nodes, Faces      =      5293     10242
AFLR2 GGp: Nodes, Faces      =      5447     10550
AFLR2 GGp: Nodes, Faces      =      5594     10844
AFLR2 GGp: Nodes, Faces      =      5716     11088
AFLR2 GGp: Nodes, Faces      =      5830     11316
AFLR2 GGp: Nodes, Faces      =      5909     11474
AFLR2 GGp: Nodes, Faces      =      5964     11584
AFLR2 GGp: Nodes, Faces      =      6006     11668
AFLR2 GGp: Nodes, Faces      =      6025     11706
AFLR2 GGp: Nodes, Faces      =      6034     11724
 
AFLR2    : CPU Time          =     0.017   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          =     0.009   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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 7):
	Number of nodes          = 6353
	Number of elements       = 35297
	Number of triangles      = 4430
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 30867
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cone, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 7):
	Number of nodes          = 13586
	Number of elements       = 76197
	Number of triangles      = 8142
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 68055
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = torus, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 4 (of 7):
	Number of nodes          = 42291
	Number of elements       = 240392
	Number of triangles      = 19942
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 220450
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = sphere, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 7):
	Number of nodes          = 4366
	Number of elements       = 24242
	Number of triangles      = 3014
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 21228
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = boxhole, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 6 (of 7):
	Number of nodes          = 11036
	Number of elements       = 60950
	Number of triangles      = 8628
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 52322
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = bullet, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 7 (of 7):
	Number of nodes          = 10730
	Number of elements       = 60223
	Number of triangles      = 6362
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 53861
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing 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          = 89551
	Number of elements       = 503550
	Number of triangles      = 51850
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 451700
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing 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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
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          = 17731
	Number of elements       = 101026
	Number of triangles      = 8318
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 92708
	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          = 2592
	Number of elements       = 13823
	Number of triangles      = 2758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11065
	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          = 3651
	Number of elements       = 19783
	Number of triangles      = 3394
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 16389
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
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          = 5487
	Number of elements       = 30509
	Number of triangles      = 3656
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 26853
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
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          = 4694
	Number of elements       = 25935
	Number of triangles      = 3326
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 22609
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
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          = 5554
	Number of elements       = 30862
	Number of triangles      = 3756
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 27106
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
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          = 2260
	Number of elements       = 12133
	Number of triangles      = 2222
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 9911
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
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          = 3341
	Number of elements       = 18069
	Number of triangles      = 3110
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 14959
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
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          = 4414
	Number of elements       = 23974
	Number of triangles      = 3998
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 19976
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
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          = 5490
	Number of elements       = 29891
	Number of triangles      = 4886
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 25005
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
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          = 6542
	Number of elements       = 35667
	Number of triangles      = 5774
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 29893
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
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          = 7601
	Number of elements       = 41489
	Number of triangles      = 6662
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 34827
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
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          = 19800
	Number of elements       = 109798
	Number of triangles      = 15540
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 94258
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
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          = 29411
	Number of elements       = 170137
	Number of triangles      = 7670
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 162467
	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          = 22482
	Number of elements       = 130132
	Number of triangles      = 6118
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 124014
	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          = 29411
	Number of elements       = 170137
	Number of triangles      = 7670
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 162467
	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          = 22482
	Number of elements       = 130132
	Number of triangles      = 6118
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 124014
	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          = 29411
	Number of elements       = 170137
	Number of triangles      = 7670
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 162467
	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          = 22482
	Number of elements       = 130132
	Number of triangles      = 6118
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 124014
	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          = 29411
	Number of elements       = 170137
	Number of triangles      = 7670
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 162467
	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          = 22482
	Number of elements       = 130132
	Number of triangles      = 6118
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 124014
	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          = 5047
	Number of elements       = 27987
	Number of triangles      = 3464
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 24523
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
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          = 6467
	Number of elements       = 36212
	Number of triangles      = 4048
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 32164
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
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          = 40512
	Number of elements       = 233939
	Number of triangles      = 12424
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 221515
	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          = 44117
	Number of elements       = 255216
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 242810
	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          = 40512
	Number of elements       = 233921
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 221515
	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 IEEE_DENORMAL
Done running Astros!
ok
test_Plate (test_astros.TestAstros.test_Plate) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to 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 IEEE_DENORMAL
Aero_Reference value is NULL - No aero reference parameters set

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - Mach
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 3
	Objective name - C_A
	Objective name - C_N
	Objective name - C_Y
	Done getting CFD functional
 Body size = 15.356535
 Tessellating body 1 with  MaxEdge = 0.383913  Sag = 0.015357  Angle = 15.000000
 Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:35:49) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:35:51) 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
   (20:35:52) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:35:56) 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
   (20:35:57) Linearizing cut-cells
   (20:35:57) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:35:58) Computing gradients
   (20:36:06) ... 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
   (20:36:07) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:36:08) 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
   (20:36:09) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:36:10) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:36:11) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:36:14) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (20:36:14) Linearizing cut-cells
   (20:36:14) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:36:14) Computing gradients
   (20:36:22) ... 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
   (20:36:24) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:36:25) 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
   (20:36:27) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:36:29) 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
   (20:36:30) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:36:33) 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
   (20:36:34) Linearizing cut-cells
   (20:36:34) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:36:34) Computing gradients
   (20:36:38) ... 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
   (20:36:39) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:36:40) 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
   (20:36:42) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:36:43) 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
   (20:36:44) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:36:45) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (20:36:46) Linearizing cut-cells
   (20:36:46) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:36:46) Computing gradients
   (20:36:50) ... 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
   (20:36:51) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:36:53) 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
   (20:36:54) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:36:56) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:36:57) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:36:59) 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
   (20:36:59) Linearizing cut-cells
   (20:36:59) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:36:59) Computing gradients
   (20:37:03) ... 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
   (20:37:05) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:37:06) 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
   (20:37:07) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:37:08) 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
   (20:37:10) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:37:11) 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
   (20:37:11) Linearizing cut-cells
   (20:37:11) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:37:11) Computing gradients
   (20:37:15) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:37:17) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:37:18) 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
   (20:37:19) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:37:20) 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
   (20:37:22) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:37:23) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (20:37:24) Linearizing cut-cells
   (20:37:24) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:37:24) Computing gradients
   (20:37:28) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:37:29) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:37:31) 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_z
	Done getting CFD functional
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:37:33) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:37:35) 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
   (20:37:36) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:37:38) 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
   (20:37:38) Linearizing cut-cells
   (20:37:38) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:37:38) Computing gradients
   (20:37:42) ... 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
   (20:37:44) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:37:45) 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
   (20:37:47) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:37:49) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:37:50) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:37:53) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               8744
              Estimated cutter memory:  0.000874 GB / DV
              Estimated xsensit memory: 0.016614 GB / DV
              Available threads:        2
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (20:37:54) Linearizing cut-cells
   (20:37:56) ... done
   o Number of simultaneous xsensit jobs:  2
   (20:37:56) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (20:38:04) ... 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
   (20:38:05) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
   (20:38:06) 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
 7FF8487D9780 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7FF8487D9780 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 70000FF00000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 70000FF00000 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
 7FF8487D9780 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7FF8487D9780 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 70000FF00000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 70000FF00000 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    = 7819
Number of elements = 15634
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 15634
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5889
Number of elements = 11774
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 11774
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 516
Number of elements = 1028
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1028
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14224
Total number of elements = 28436
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 14224, elements - 28436
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.113647
Creating surface mesh ...
Surface mesh seconds:  0.02227
Recovering boundaries...
Boundary recovery seconds:  0.083781
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.031435
Recovering Delaunayness...
Delaunay recovery seconds:  0.042054
Refining mesh...
  18960 insertions, added 14017 points, 701008 tetrahedra in queue.
  6313 insertions, added 2494 points, 554976 tetrahedra in queue.
  8415 insertions, added 1753 points, 70 tetrahedra in queue.
Refinement seconds:  1.48204
Smoothing vertices...
Mesh smoothing seconds:  1.51284
Improving mesh...
Mesh improvement seconds:  0.039669

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

Output seconds:  0.009321
Total running seconds:  3.33756

Statistics:

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

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

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

Getting CFD design variables.......
	Number of design variables - 5
	Design Variable name - Mach
Warning: No initial value set for Mach
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
ok
test_Design_Sensitivity (test_fun3d.TestFUN3D.test_Design_Sensitivity) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 6
	Design Variable name - Alpha
	Design Variable name - Beta
Warning: No initial value set for Beta
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 2
	Objective name - Composite
	Objective name - Lift^2
	Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing rubber.data 

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data 

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)
	Overwrite_NML is set to 'True' - a new namelist will be created
	Creating namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.
Reading rubber.data 

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - Alpha
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 2
	Objective name - Composite
	Objective name - Lift^2
	Done getting CFD functional
Creating FUN3D directory tree
DesignVariable = Alpha
Writing rubber.data 

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)
	Overwrite_NML is set to 'True' - a new namelist will be created
	Creating namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.
Reading rubber.data 
ok
test_Mesh_Morph_Sensitivity (test_fun3d.TestFUN3D.test_Mesh_Morph_Sensitivity) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 6
	Design Variable name - Alpha
	Design Variable name - Beta
Warning: No initial value set for Beta
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 2
	Objective name - Composite
	Objective name - Lift^2
	Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data 
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 
Projecting tessellation 1 (of 3) on to new body
Projecting tessellation 2 (of 3) on to new body
Projecting tessellation 3 (of 3) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 
Projecting tessellation 1 (of 3) on to new body
Projecting tessellation 2 (of 3) on to new body
Projecting tessellation 3 (of 3) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 
ok
test_cythonNML (test_fun3d.TestFUN3D.test_cythonNML) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 7819
Number of elements = 15634
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 15634
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5889
Number of elements = 11774
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 11774
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 516
Number of elements = 1028
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1028
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14224
Total number of elements = 28436
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 14224, elements - 28436
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.119283
Creating surface mesh ...
Surface mesh seconds:  0.019135
Recovering boundaries...
Boundary recovery seconds:  0.086829
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.033039
Recovering Delaunayness...
Delaunay recovery seconds:  0.046152
Refining mesh...
  18960 insertions, added 14017 points, 701008 tetrahedra in queue.
  6313 insertions, added 2494 points, 554976 tetrahedra in queue.
  8415 insertions, added 1753 points, 70 tetrahedra in queue.
Refinement seconds:  1.59249
Smoothing vertices...
Mesh smoothing seconds:  1.61366
Improving mesh...
Mesh improvement seconds:  0.033111

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

Output seconds:  0.008955
Total running seconds:  3.55315

Statistics:

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

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

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

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)

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

Writing MAPBC file ....
Finished writing MAPBC file


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

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)

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

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

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 4
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

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

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 4
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 4
	Design Variable name - area
	Design Variable name - aspect
	Design Variable name - taper
	Design Variable name - twist
	Done getting CFD design variables
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
ok
test_moving_body (test_fun3d.TestFUN3D.test_moving_body) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

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

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_phase (test_fun3d.TestFUN3D.test_phase) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

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

Generating volume mesh using TetGen.....

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

Writing MAPBC file ....
Finished writing MAPBC file

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

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

Writing MAPBC file ....
Finished writing MAPBC file

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

Writing MAPBC file ....
Finished writing MAPBC file

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

Writing MAPBC file ....
Finished writing MAPBC file

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

Writing MAPBC file ....
Finished writing MAPBC file

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
ok
test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable'
test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable'
test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable'
test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable'
test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable'
test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable'
test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable'
test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable'
test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable'
test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable'
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
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          = 1015
	Number of elements       = 5450
	Number of triangles      = 918
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4532
	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          = 323
	Number of elements       = 1583
	Number of triangles      = 496
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1087
	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          = 960
	Number of elements       = 5119
	Number of triangles      = 874
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4245
	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          = 17541
	Number of elements       = 100992
	Number of triangles      = 5240
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 95752
	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          = 1015
	Number of elements       = 5450
	Number of triangles      = 918
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4532
	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          = 398
	Number of elements       = 1955
	Number of triangles      = 612
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1343
	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          = 305
	Number of elements       = 1472
	Number of triangles      = 468
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1004
	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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
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 22.5.0 x86_64
AFLR3    : Compile Date   07/26/23 @ 01:42PM
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          =     0.012   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =      6209         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =      1244      7653
AFLR3 IG : Nodes, Elements   =      2488     16237
AFLR3 IG : Nodes, Elements   =      3732     24929
AFLR3 IG : Nodes, Elements   =      4976     33940
AFLR3 IG : Nodes, Elements   =      6216     42984
AFLR3 IG : Nodes, Elements   =      6216     42932
AFLR3 IG : Nodes, Elements   =      6216     42936
AFLR3 IG : Nodes, Elements   =      6216     42931
AFLR3 IG : Nodes, Elements   =      6216     42936
AFLR3 IG : Nodes, Elements   =      6216     42928
AFLR3 IG : Nodes, Elements   =      6216     42929
AFLR3 IG : Nodes, Elements   =      6209     25549
AFLR3 IG : Nodes, Elements   =      6209     25566
AFLR3 IG : Nodes, Elements   =      6209     20457
AFLR3 IG : Nodes, Elements   =      6209     18370
 
AFLR3    : CPU Time          =     0.171   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =      6209     18370
AFLR3 GG : Nodes, Elements   =      9083     27216
AFLR3 GG : Nodes, Elements   =      9083     39129
AFLR3 GG : Nodes, Elements   =      9083     36299
AFLR3 GG : Nodes, Elements   =      9083     34787
AFLR3 GG : Nodes, Elements   =     11687     42926
AFLR3 GG : Nodes, Elements   =     11687     54107
AFLR3 GG : Nodes, Elements   =     11687     50912
AFLR3 GG : Nodes, Elements   =     11687     49950
AFLR3 GG : Nodes, Elements   =     14459     58534
AFLR3 GG : Nodes, Elements   =     14459     70598
AFLR3 GG : Nodes, Elements   =     14459     67246
AFLR3 GG : Nodes, Elements   =     14459     66445
AFLR3 GG : Nodes, Elements   =     17390     75436
AFLR3 GG : Nodes, Elements   =     17390     88100
AFLR3 GG : Nodes, Elements   =     17390     84689
AFLR3 GG : Nodes, Elements   =     17390     83831
AFLR3 GG : Nodes, Elements   =     20561     93518
AFLR3 GG : Nodes, Elements   =     20561    106956
AFLR3 GG : Nodes, Elements   =     20561    103464
AFLR3 GG : Nodes, Elements   =     20561    102605
AFLR3 GG : Nodes, Elements   =     23901    112791
AFLR3 GG : Nodes, Elements   =     23901    126928
AFLR3 GG : Nodes, Elements   =     23901    123203
AFLR3 GG : Nodes, Elements   =     23901    122366
AFLR3 GG : Nodes, Elements   =     27314    132747
AFLR3 GG : Nodes, Elements   =     27314    147193
AFLR3 GG : Nodes, Elements   =     27314    143350
AFLR3 GG : Nodes, Elements   =     27314    142550
AFLR3 GG : Nodes, Elements   =     30859    153312
AFLR3 GG : Nodes, Elements   =     30859    168311
AFLR3 GG : Nodes, Elements   =     30859    164409
AFLR3 GG : Nodes, Elements   =     30859    163606
AFLR3 GG : Nodes, Elements   =     34446    174469
AFLR3 GG : Nodes, Elements   =     34446    189518
AFLR3 GG : Nodes, Elements   =     34446    185603
AFLR3 GG : Nodes, Elements   =     34446    184796
AFLR3 GG : Nodes, Elements   =     38030    195632
AFLR3 GG : Nodes, Elements   =     38030    210636
AFLR3 GG : Nodes, Elements   =     38030    206840
AFLR3 GG : Nodes, Elements   =     38030    206098
AFLR3 GG : Nodes, Elements   =     41514    216606
AFLR3 GG : Nodes, Elements   =     41514    231337
AFLR3 GG : Nodes, Elements   =     41514    227569
AFLR3 GG : Nodes, Elements   =     41514    226816
AFLR3 GG : Nodes, Elements   =     44978    237248
AFLR3 GG : Nodes, Elements   =     44978    251924
AFLR3 GG : Nodes, Elements   =     44978    248091
AFLR3 GG : Nodes, Elements   =     44978    247412
AFLR3 GG : Nodes, Elements   =     48303    257424
AFLR3 GG : Nodes, Elements   =     48303    271465
AFLR3 GG : Nodes, Elements   =     48303    267845
AFLR3 GG : Nodes, Elements   =     48303    267239
AFLR3 GG : Nodes, Elements   =     51495    276839
AFLR3 GG : Nodes, Elements   =     51495    290288
AFLR3 GG : Nodes, Elements   =     51495    286801
AFLR3 GG : Nodes, Elements   =     51495    286238
AFLR3 GG : Nodes, Elements   =     54566    295468
AFLR3 GG : Nodes, Elements   =     54566    308318
AFLR3 GG : Nodes, Elements   =     54566    305103
AFLR3 GG : Nodes, Elements   =     54566    304607
AFLR3 GG : Nodes, Elements   =     57407    313138
AFLR3 GG : Nodes, Elements   =     57407    325082
AFLR3 GG : Nodes, Elements   =     57407    322052
AFLR3 GG : Nodes, Elements   =     57407    321624
AFLR3 GG : Nodes, Elements   =     60033    329508
AFLR3 GG : Nodes, Elements   =     60033    340522
AFLR3 GG : Nodes, Elements   =     60033    337740
AFLR3 GG : Nodes, Elements   =     60033    337327
AFLR3 GG : Nodes, Elements   =     62385    344387
AFLR3 GG : Nodes, Elements   =     62385    354178
AFLR3 GG : Nodes, Elements   =     62385    351770
AFLR3 GG : Nodes, Elements   =     62385    351406
AFLR3 GG : Nodes, Elements   =     64423    357521
AFLR3 GG : Nodes, Elements   =     64423    366066
AFLR3 GG : Nodes, Elements   =     64423    363902
AFLR3 GG : Nodes, Elements   =     64423    363640
AFLR3 GG : Nodes, Elements   =     66152    368828
AFLR3 GG : Nodes, Elements   =     66152    376096
AFLR3 GG : Nodes, Elements   =     66152    374169
AFLR3 GG : Nodes, Elements   =     66152    373954
AFLR3 GG : Nodes, Elements   =     67502    378007
AFLR3 GG : Nodes, Elements   =     67502    383819
AFLR3 GG : Nodes, Elements   =     67502    382205
AFLR3 GG : Nodes, Elements   =     67502    382037
AFLR3 GG : Nodes, Elements   =     68453    384892
AFLR3 GG : Nodes, Elements   =     68453    388938
AFLR3 GG : Nodes, Elements   =     68453    387786
AFLR3 GG : Nodes, Elements   =     68453    387696
AFLR3 GG : Nodes, Elements   =     69095    389624
AFLR3 GG : Nodes, Elements   =     69095    392359
AFLR3 GG : Nodes, Elements   =     69095    391593
AFLR3 GG : Nodes, Elements   =     69095    391521
AFLR3 GG : Nodes, Elements   =     69433    392535
AFLR3 GG : Nodes, Elements   =     69433    393990
AFLR3 GG : Nodes, Elements   =     69433    393564
AFLR3 GG : Nodes, Elements   =     69433    393530
AFLR3 GG : Nodes, Elements   =     69586    393989
AFLR3 GG : Nodes, Elements   =     69586    394640
AFLR3 GG : Nodes, Elements   =     69586    394434
AFLR3 GG : Nodes, Elements   =     69586    394423
AFLR3 GG : Nodes, Elements   =     69642    394591
AFLR3 GG : Nodes, Elements   =     69642    394832
AFLR3 GG : Nodes, Elements   =     69642    394746
AFLR3 GG : Nodes, Elements   =     69642    394743
AFLR3 GG : Nodes, Elements   =     69655    394782
AFLR3 GG : Nodes, Elements   =     69655    394832
AFLR3 GG : Nodes, Elements   =     69655    394819
AFLR3 GG : Nodes, Elements   =     69655    394818
AFLR3 GG : Nodes, Elements   =     69657    394824
AFLR3 GG : Nodes, Elements   =     69657    394829
AFLR3 GG : Nodes, Elements   =     69657    394828
AFLR3 GG : Nodes, Elements   =     69657    394829
AFLR3 GG : Nodes, Elements   =     69677    394889
AFLR3 GG : Nodes, Elements   =     69677    394955
AFLR3 GG : Nodes, Elements   =     69677    394942
AFLR3 GG : Nodes, Elements   =     69677    394943
AFLR3 GG : Nodes, Elements   =     69687    394973
AFLR3 GG : Nodes, Elements   =     69687    395009
AFLR3 GG : Nodes, Elements   =     69687    395000
AFLR3 GG : Nodes, Elements   =     69687    395002
AFLR3 GG : Nodes, Elements   =     69691    395014
AFLR3 GG : Nodes, Elements   =     69691    395030
AFLR3 GG : Nodes, Elements   =     69691    395025
AFLR3 GG : Nodes, Elements   =     69691    395026
AFLR3 GG : Nodes, Elements   =     69692    395029
AFLR3 GG : Nodes, Elements   =     69692    395034
AFLR3 GG : Nodes, Elements   =     69692    395032
 
AFLR3    : CPU Time          =     3.710   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =     69692    395032
AFLR3 QI : Nodes, Elements   =     68269    387028
AFLR3 QI : Nodes, Elements   =     68069    385895
AFLR3 QI : Nodes, Elements   =     68051    385787
AFLR3 QI : Nodes, Elements   =     68049    385776
AFLR3 QI : Nodes, Elements   =     68049    389538
AFLR3 QI : Nodes, Elements   =     68049    385544
AFLR3 QI : Nodes, Elements   =     68049    385168
AFLR3 QI : Nodes, Elements   =     68049    387753
AFLR3 QI : Nodes, Elements   =     68049    385223
AFLR3 QI : Nodes, Elements   =     68049    385141
AFLR3 QI : Nodes, Elements   =     68049    385767
AFLR3 QI : Nodes, Elements   =     68049    384976
AFLR3 QI : Nodes, Elements   =     68049    384826
AFLR3 QI : Nodes, Elements   =     68049    385189
AFLR3 QI : Nodes, Elements   =     68049    384786
AFLR3 QI : Nodes, Elements   =     68049    384692
AFLR3 QI : Nodes, Elements   =     68049    384987
AFLR3 QI : Nodes, Elements   =     68049    384685
AFLR3 QI : Nodes, Elements   =     68049    384630
AFLR3 QI : Nodes, Elements   =     68053    384648
AFLR3 QI : Nodes, Elements   =     68053    384951
AFLR3 QI : Nodes, Elements   =     68053    384661
AFLR3 QI : Nodes, Elements   =     68053    384646
AFLR3 QI : Nodes, Elements   =     68053    384908
AFLR3 QI : Nodes, Elements   =     68053    384645
AFLR3 QI : Nodes, Elements   =     68053    384606
 
AFLR3    : CPU Time          =     1.403   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =     68053    384606
AFLR3 QRG: Nodes, Elements   =     68057    384626
AFLR3 QRG: Nodes, Elements   =     68063    384656
 
AFLR3    : CPU Time          =     0.039   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    384656
UG3      : Min, Max Ang      =    0.7661     175.6
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        48
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.11e+06

UG3      : No. Tet Elems     =    384656
UG3      : Min Vol           =  6.55e-10
UG3      : Average Vol       =      5.48
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     =    384656
UG3      : Min, Max Q        =    0.0537         1
UG3      : Average Q         =     0.891
UG3      : No. Q<       0.1  =        22
UG3      : No. Q<      0.01  =         0

OVERALL  : CPU Time          =     5.663   seconds

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    384656
UG3      : Min, Max Ang      =    0.7661     175.6
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        48
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.11e+06

UG3      : No. Tet Elems     =    384656
UG3      : Min Vol           =  6.55e-10
UG3      : Average Vol       =      5.48
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     =    384656
UG3      : Min, Max Q        =      0.12         1
UG3      : Average Q         =     0.852
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          = 68063
	Number of elements       = 397062
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 384656
	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          = 68063
	Number of elements       = 397062
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 384656
	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          = 68063
	Number of elements       = 397062
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 384656
	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          = 68063
	Number of elements       = 397062
	Number of triangles      = 12406
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 384656
	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)
 7FF8487D9780 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 70000FF00000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7FF8487D9780 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 70000FF00000 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    = 297
Number of elements = 590
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 590
Number of quadrilateral elements = 0
Body 3 (of 7)
Number of nodes    = 487
Number of elements = 970
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 970
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    = 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
----------------------------
Total number of nodes    = 4194
Total number of elements = 8368
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 297, elements - 590
Body 3 number of surface: nodes - 487, elements - 970
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.002382
Creating surface mesh ...
Surface mesh seconds:  9.3e-05
Recovering boundaries...
Boundary recovery seconds:  0.001294
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  6.5e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.000761
Refining mesh...
Refinement seconds:  0.000827
Smoothing vertices...
Mesh smoothing seconds:  0.003678
Improving mesh...
Mesh improvement seconds:  0.0001

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

Output seconds:  5.2e-05
Total running seconds:  0.0093

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:  0.012244
Creating surface mesh ...
Surface mesh seconds:  0.000281
Recovering boundaries...
Boundary recovery seconds:  0.002081
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000282
Recovering Delaunayness...
Delaunay recovery seconds:  0.003178
Refining mesh...
Refinement seconds:  0.017482
Smoothing vertices...
Mesh smoothing seconds:  0.016802
Improving mesh...
Mesh improvement seconds:  0.000392

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

Output seconds:  0.00012
Total running seconds:  0.052923

Statistics:

  Input points: 297
  Input facets: 590
  Input segments: 885
  Input holes: 0
  Input regions: 0

  Mesh points: 347
  Mesh tetrahedra: 1044
  Mesh faces: 2383
  Mesh faces on exterior boundary: 590
  Mesh faces on input facets: 590
  Mesh edges on input segments: 885
  Steiner points inside domain: 50

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:  0.050467
Creating surface mesh ...
Surface mesh seconds:  0.000531
Recovering boundaries...
Boundary recovery seconds:  0.005149
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000782
Recovering Delaunayness...
Delaunay recovery seconds:  0.012211
Refining mesh...
  649 insertions, added 165 points, 7218 tetrahedra in queue.
  216 insertions, added 8 points, 5722 tetrahedra in queue.
  288 insertions, added 12 points, 3275 tetrahedra in queue.
  383 insertions, added 10 points, 312 tetrahedra in queue.
  511 insertions, added 11 points, 94 tetrahedra in queue.
Refinement seconds:  0.136033
Smoothing vertices...
Mesh smoothing seconds:  0.053877
Improving mesh...
Mesh improvement seconds:  0.001329

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

Output seconds:  0.000229
Total running seconds:  0.260698

Statistics:

  Input points: 487
  Input facets: 970
  Input segments: 1455
  Input holes: 0
  Input regions: 0

  Mesh points: 695
  Mesh tetrahedra: 2810
  Mesh faces: 6105
  Mesh faces on exterior boundary: 970
  Mesh faces on input facets: 970
  Mesh edges on input segments: 1455
  Steiner points inside domain: 208

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:  0.421535
Creating surface mesh ...
Surface mesh seconds:  0.004758
Recovering boundaries...
Boundary recovery seconds:  0.010021
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.002896
Recovering Delaunayness...
Delaunay recovery seconds:  0.114636
Refining mesh...
Refinement seconds:  0.28654
Smoothing vertices...
Mesh smoothing seconds:  0.224827
Improving mesh...
Mesh improvement seconds:  0.004148

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

Output seconds:  0.001013
Total running seconds:  1.07049

Statistics:

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

  Mesh points: 2895
  Mesh tetrahedra: 11267
  Mesh faces: 24582
  Mesh faces on exterior boundary: 4096
  Mesh faces on input facets: 4096
  Mesh edges on input segments: 6144
  Steiner points inside domain: 847

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:  0.00028
Creating surface mesh ...
Surface mesh seconds:  0.00018
Recovering boundaries...
Boundary recovery seconds:  0.000272
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  8.2e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.000396
Refining mesh...
  202 insertions, added 46 points, 0 tetrahedra in queue.
Refinement seconds:  0.008853
Smoothing vertices...
Mesh smoothing seconds:  0.002613
Improving mesh...
Mesh improvement seconds:  0.000194

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

Output seconds:  6.6e-05
Total running seconds:  0.012987

Statistics:

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

  Mesh points: 198
  Mesh tetrahedra: 672
  Mesh faces: 1494
  Mesh faces on exterior boundary: 300
  Mesh faces on input facets: 300
  Mesh edges on input segments: 450
  Steiner points inside domain: 46

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:  0.050771
Creating surface mesh ...
Surface mesh seconds:  0.001526
Recovering boundaries...
Boundary recovery seconds:  0.004433
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000869
Recovering Delaunayness...
Delaunay recovery seconds:  0.007319
Refining mesh...
  831 insertions, added 225 points, 6035 tetrahedra in queue.
Refinement seconds:  0.074782
Smoothing vertices...
Mesh smoothing seconds:  0.053165
Improving mesh...
Mesh improvement seconds:  0.001235

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

Output seconds:  0.000266
Total running seconds:  0.194462

Statistics:

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

  Mesh points: 856
  Mesh tetrahedra: 3198
  Mesh faces: 7020
  Mesh faces on exterior boundary: 1248
  Mesh faces on input facets: 1248
  Mesh edges on input segments: 1872
  Steiner points inside domain: 232

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:  0.043944
Creating surface mesh ...
Surface mesh seconds:  0.000489
Recovering boundaries...
Boundary recovery seconds:  0.003381
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.000404
Recovering Delaunayness...
Delaunay recovery seconds:  0.029748
Refining mesh...
Refinement seconds:  0.039284
Smoothing vertices...
Mesh smoothing seconds:  0.023748
Improving mesh...
Mesh improvement seconds:  0.002234

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

Output seconds:  0.000201
Total running seconds:  0.143503

Statistics:

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

  Mesh points: 676
  Mesh tetrahedra: 2529
  Mesh faces: 5544
  Mesh faces on exterior boundary: 972
  Mesh faces on input facets: 972
  Mesh edges on input segments: 1458
  Steiner points inside domain: 188

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 - 297, elements - 590
Body 3 number of surface: nodes - 487, elements - 970
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.00203
Creating surface mesh ...
Surface mesh seconds:  9.7e-05
Recovering boundaries...
Boundary recovery seconds:  0.000726
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  5.9e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.000705
Refining mesh...
Refinement seconds:  0.003879
Smoothing vertices...
Mesh smoothing seconds:  0.00216
Improving mesh...
Mesh improvement seconds:  7e-05

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

Output seconds:  3.9e-05
Total running seconds:  0.009812

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:  0.010199
Creating surface mesh ...
Surface mesh seconds:  0.000231
Recovering boundaries...
Boundary recovery seconds:  0.001636
Removing exterior tetrahedra ...
Warning:  The 1-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds:  0.00028
Recovering Delaunayness...
Delaunay recovery seconds:  0.003429
Refining mesh...
Refinement seconds:  0.012535
Smoothing vertices...
Mesh smoothing seconds:  0.014029
Improving mesh...
Mesh improvement seconds:  0.002994

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

Output seconds:  8.3e-05
Total running seconds:  0.045473

Statistics:

  Input points: 297
  Input facets: 590
  Input segments: 885
  Input holes: 0
  Input regions: 2

  Mesh points: 347
  Mesh tetrahedra: 1044
  Mesh faces: 2383
  Mesh faces on exterior boundary: 590
  Mesh faces on input facets: 590
  Mesh edges on input segments: 885
  Steiner points inside domain: 50


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.043302
Creating surface mesh ...
Surface mesh seconds:  0.001903
Recovering boundaries...
Boundary recovery seconds:  0.004565
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:  0.000578
Recovering Delaunayness...
Delaunay recovery seconds:  0.01121
Refining mesh...
  649 insertions, added 164 points, 7317 tetrahedra in queue.
  216 insertions, added 10 points, 6108 tetrahedra in queue.
  288 insertions, added 9 points, 3288 tetrahedra in queue.
  383 insertions, added 12 points, 283 tetrahedra in queue.
  511 insertions, added 12 points, 75 tetrahedra in queue.
Refinement seconds:  0.107082
Smoothing vertices...
Mesh smoothing seconds:  0.038463
Improving mesh...
Mesh improvement seconds:  0.00356

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

Output seconds:  0.000148
Total running seconds:  0.210875

Statistics:

  Input points: 487
  Input facets: 970
  Input segments: 1455
  Input holes: 0
  Input regions: 3

  Mesh points: 695
  Mesh tetrahedra: 2796
  Mesh faces: 6077
  Mesh faces on exterior boundary: 970
  Mesh faces on input facets: 970
  Mesh edges on input segments: 1455
  Steiner points inside domain: 208


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.329168
Creating surface mesh ...
Surface mesh seconds:  0.002001
Recovering boundaries...
Boundary recovery seconds:  0.007547
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:  0.002507
Recovering Delaunayness...
Delaunay recovery seconds:  0.096394
Refining mesh...
Refinement seconds:  0.241362
Smoothing vertices...
Mesh smoothing seconds:  0.177665
Improving mesh...
Mesh improvement seconds:  0.003577

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

Output seconds:  0.000813
Total running seconds:  0.86114

Statistics:

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

  Mesh points: 2905
  Mesh tetrahedra: 11306
  Mesh faces: 24660
  Mesh faces on exterior boundary: 4096
  Mesh faces on input facets: 4096
  Mesh edges on input segments: 6144
  Steiner points inside domain: 857


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.000276
Creating surface mesh ...
Surface mesh seconds:  0.000136
Recovering boundaries...
Boundary recovery seconds:  0.000248
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:  8.9e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.00045
Refining mesh...
  202 insertions, added 46 points, 0 tetrahedra in queue.
Refinement seconds:  0.003826
Smoothing vertices...
Mesh smoothing seconds:  0.002388
Improving mesh...
Mesh improvement seconds:  0.003199

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

Output seconds:  6.2e-05
Total running seconds:  0.010717

Statistics:

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

  Mesh points: 198
  Mesh tetrahedra: 672
  Mesh faces: 1494
  Mesh faces on exterior boundary: 300
  Mesh faces on input facets: 300
  Mesh edges on input segments: 450
  Steiner points inside domain: 46


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.039936
Creating surface mesh ...
Surface mesh seconds:  0.000784
Recovering boundaries...
Boundary recovery seconds:  0.004085
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:  0.000648
Recovering Delaunayness...
Delaunay recovery seconds:  0.006021
Refining mesh...
  831 insertions, added 225 points, 6035 tetrahedra in queue.
Refinement seconds:  0.059818
Smoothing vertices...
Mesh smoothing seconds:  0.045506
Improving mesh...
Mesh improvement seconds:  0.000957

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

Output seconds:  0.000249
Total running seconds:  0.158073

Statistics:

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

  Mesh points: 856
  Mesh tetrahedra: 3198
  Mesh faces: 7020
  Mesh faces on exterior boundary: 1248
  Mesh faces on input facets: 1248
  Mesh edges on input segments: 1872
  Steiner points inside domain: 232


Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.034802
Creating surface mesh ...
Surface mesh seconds:  0.000497
Recovering boundaries...
Boundary recovery seconds:  0.003653
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:  0.000463
Recovering Delaunayness...
Delaunay recovery seconds:  0.027217
Refining mesh...
Refinement seconds:  0.039024
Smoothing vertices...
Mesh smoothing seconds:  0.023805
Improving mesh...
Mesh improvement seconds:  0.000617

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

Output seconds:  0.000155
Total running seconds:  0.130298

Statistics:

  Input points: 488
  Input facets: 972
  Input segments: 1458
  Input holes: 0
  Input regions: 7

  Mesh points: 676
  Mesh tetrahedra: 2544
  Mesh faces: 5574
  Mesh faces on exterior boundary: 972
  Mesh faces on input facets: 972
  Mesh edges on input segments: 1458
  Steiner points inside domain: 188

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 - 9605, elements - 19202
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9605, elements - 19202
Getting volume mesh

Generating volume mesh using TetGen.....

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

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9605, elements - 19202
Getting volume mesh

Generating volume mesh using TetGen.....

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

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

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

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9605, elements - 19202
Getting volume mesh

Generating volume mesh using TetGen.....

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

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

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9605, elements - 19202
Getting volume mesh

Generating volume mesh using TetGen.....

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

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 - 7161, elements - 14314
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    = 9605
Number of elements = 19202
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 19202
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9605
Total number of elements = 19202

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 - 9605, elements - 19202
Getting volume mesh

Generating volume mesh using TetGen.....

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

Writing 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 - 9605, elements - 19202
Getting volume mesh

Generating volume mesh using TetGen.....

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

Writing 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 580.250s

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

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


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


Running AVL!


Value of Cltot = 0.619913

StripForces

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

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


real	0m0.908s
user	0m0.530s
sys	0m0.164s
+ 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	0m1.686s
user	0m1.453s
sys	0m0.112s
+ 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	0m0.736s
user	0m0.369s
sys	0m0.059s
+ 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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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          =     0.005   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          =     0.055   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     18615     36389
AFLR2 QI : Nodes, Faces      =     18608      1893
AFLR2 QI : Nodes, Faces      =     18608     17241
AFLR2 QI : Nodes, Faces      =     18608     36375
AFLR2 QI : Nodes, Faces      =     18606      1789
AFLR2 QI : Nodes, Faces      =     18606     17291
AFLR2 QI : Nodes, Faces      =     18606     36371
AFLR2 QI : Nodes, Faces      =     18604      1971
AFLR2 QI : Nodes, Faces      =     18604     17198
AFLR2 QI : Nodes, Faces      =     18604     36367
AFLR2 QI : Nodes, Faces      =     18604      2161
AFLR2 QI : Nodes, Faces      =     18604     17103
AFLR2 QI : Nodes, Faces      =     18604     36367
AFLR2 QI : Nodes, Faces      =     18604      2149
AFLR2 QI : Nodes, Faces      =     18604     17109
AFLR2 QI : Nodes, Faces      =     18604      2149
AFLR2 QI : Nodes, Faces      =     18604     17109
 
AFLR2    : CPU Time          =     0.028   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

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

Writing TECPLOT file: 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 =  2149
	Number of Hexahedral =  17109

Writing AFLR3 file ....
Finished writing AFLR3 file


Writing MAPBC file ....
Finished writing MAPBC file

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

real	0m1.915s
user	0m1.243s
sys	0m0.434s
+ status=0
+ set +x

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


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


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

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.14165
Creating surface mesh ...
Surface mesh seconds:  0.025591
Recovering boundaries...
Boundary recovery seconds:  0.109559
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.037632
Recovering Delaunayness...
Delaunay recovery seconds:  0.056644
Refining mesh...
  21350 insertions, added 16804 points, 756241 tetrahedra in queue.
  7109 insertions, added 2842 points, 312650 tetrahedra in queue.
Refinement seconds:  1.24802
Smoothing vertices...
Mesh smoothing seconds:  1.79309
Improving mesh...
Mesh improvement seconds:  0.04484

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

Output seconds:  0.011966
Total running seconds:  3.46943

Statistics:

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

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

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

Writing MAPBC file ....
Finished writing MAPBC file

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

real	0m6.498s
user	0m7.033s
sys	0m0.338s
+ status=0
+ set +x

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

Running.... STRUCTURE c-Tests

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


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

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

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

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


real	0m3.017s
user	0m5.244s
sys	0m0.105s
+ status=0
+ set +x

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


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


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

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

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

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

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

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

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

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

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

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

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

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

real	0m0.680s
user	0m0.512s
sys	0m0.060s
+ status=0
+ set +x

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


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


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

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

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

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

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

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

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

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

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

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

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

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

real	0m1.057s
user	0m0.945s
sys	0m0.053s
+ status=0
+ set +x

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


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


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

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

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

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

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

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

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

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

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

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

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

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

real	0m0.616s
user	0m0.471s
sys	0m0.062s
+ 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   0.0006119078685747781
CYtot   -6.297054052850572e-15
CZtot   -0.301286139488597
Cltot   -4.785942150399569e-14
Cmtot   -0.1945055953450375
Cntot   -2.337286621027519e-15
Cl'tot  -4.789292355835892e-14
Cn'tot  -1.501668565013235e-15
CLtot   0.3012509314150652
CDtot   0.004646353488232536
CDvis   0.0
CLff    0.3009503023520406
CYff    -7.725269974775701e-15
CDind   0.004646353488232536
CDff    0.004968969500907968
e       0.9669902146157809
StripForces 
Wing  cl =  [0.02994790451347, 0.08555545178933, 0.1329003532587, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.310122128419, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805664, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996427, 0.2453427152623, 0.2100182422922, 0.17330251928, 0.1329003532723, 0.08555545180787, 0.0299479045408]
Wing  cd =  [-0.004234137763162, -0.004494543653191, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946408, 0.0005114598078391, 0.0021191472861, 0.004145189908974, 0.006609094404181, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.006609094404439, 0.00414518990926, 0.002119147286384, 0.0005114598080994, -0.0007386538944075, -0.001762021024096, -0.002739626801367, -0.003752887372445, -0.004494543653161, -0.004234137764544]

real	0m1.121s
user	0m0.722s
sys	0m0.489s
+ status=0
+ set +x

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


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

real	0m11.022s
user	0m13.837s
sys	0m6.789s
+ status=0
+ set +x

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


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

real	0m38.609s
user	0m17.848s
sys	0m19.898s
+ status=0
+ set +x

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


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

real	0m1.307s
user	0m0.910s
sys	0m0.508s
+ 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	0m0.972s
user	0m0.682s
sys	0m0.410s
+ status=0
+ set +x

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


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

           * * *

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

At X0         0 variables are exactly at the bounds

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

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

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

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

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

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

           * * *

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

           * * *

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

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

real	0m25.106s
user	0m4.439s
sys	0m1.669s
+ status=0
+ set +x

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

friction: /Users/jenkins/workspace/ESP_bPreBuilt/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	0m0.699s
user	0m0.600s
sys	0m0.216s
+ status=0
+ set +x

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

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

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

real	0m0.971s
user	0m0.621s
sys	0m0.180s
+ status=0
+ set +x

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

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

=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  0.3783793240300122
Cd =  0.007775858044231098
Cm =  0.005262576090314894

real	0m2.608s
user	0m2.451s
sys	0m0.281s
+ status=0
+ set +x

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


=================================================
+ echo 'mses_OpenMDAO_3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_OpenMDAO_3_PyTest.py test;
+ python -u mses_OpenMDAO_3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - camber
	Done getting CFD design variables
camber [0.1] CD [0.01326534]
camber [0.1] CD [0.01326534]
CD_camber [[0.17647556]]
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            1     M =           10

At X0         1 variables are exactly at the bounds

At iterate    0    f=  1.32653D-02    |proj g|=  1.76476D-01
camber [-0.07647556] CD [0.01022329]
CD_camber [[-0.08760106]]

At iterate    1    f=  1.02233D-02    |proj g|=  8.76011D-02
camber [-0.01793405] CD [0.00770371]
CD_camber [[-0.01328824]]

At iterate    2    f=  7.70371D-03    |proj g|=  1.32882D-02
camber [-0.00746595] CD [0.0076024]
CD_camber [[-0.0054235]]

At iterate    3    f=  7.60240D-03    |proj g|=  5.42350D-03
camber [-0.00024719] CD [0.00758207]
CD_camber [[-0.00011803]]

At iterate    4    f=  7.58207D-03    |proj g|=  1.18033D-04
camber [-8.65897362e-05] CD [0.00758208]
CD_camber [[-3.7300459e-06]]
camber [-0.0002103] CD [0.00758207]
CD_camber [[-9.42615953e-05]]

At iterate    5    f=  7.58207D-03    |proj g|=  9.42616D-05

           * * *

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

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    1      5      7      5     0     0   9.426D-05   7.582D-03
  F =   7.5820708300072251E-003

CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-0.0002103]

real	0m18.443s
user	0m17.264s
sys	0m1.077s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case mses_OpenMDAO_3_PyTest.py passed (as expected)
=================================================

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

=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  [1.05475230552582, 1.36488869373661, 1.5660721427212, 2.03059709333553, 1.9727108312101, 1.87307153172578, 1.7605047576016]
Cd =  [0.0131991208675814, 0.0166540240605919, 0.0200551482562995, 0.0458671342053759, 0.0754256009396578, 0.0994469174476091, 0.12747943098905]
Alpha =  [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location =  [0.496044114417512, 0.46137773204127, 0.442376568201482, 0.361251636517606, 0.27610414085319, 0.214381239319572, 0.132988264746184]

real	0m3.335s
user	0m3.143s
sys	0m0.225s
+ 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	0m5.669s
user	0m17.143s
sys	0m5.678s
+ 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	0m3.792s
user	0m4.211s
sys	0m0.172s
+ status=0
+ set +x

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


=================================================
+ echo 'egadsTess_Spheres_Quad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_Spheres_Quad_PyTest.py test;
+ python -u egadsTess_Spheres_Quad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Spheres, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 4 has a degenerate edge - no TFI quading
	Face 5 has a degenerate edge - no TFI quading
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 6792
Number of elements = 6790
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 6790
----------------------------
Total number of nodes    = 6792
Total number of elements = 6790

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


real	0m6.654s
user	0m9.100s
sys	0m0.287s
+ status=0
+ set +x

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


=================================================
+ echo 'egadsTess_Nose_Quad_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_Nose_Quad_PyTest.py test;
+ python -u egadsTess_Nose_Quad_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = nose, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 2 has a degenerate edge - no TFI quading
Getting surface mesh for body 1 (of 1)
 EG_getSidepoint: LineSearch Failed (0.000000 0.973785)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.013232 0.966690)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.004202 0.966536)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.046939 0.962477)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.035376 0.957497)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (1.015407 0.966058)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (0.856445 0.971910)!
 EG_getSidepoint: LineSearch Failed (2.750998 0.986828)!
 EG_getSidepoint: LineSearch Failed (0.813517 0.972994)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
 EG_getSidepoint: LineSearch Failed (0.719835 0.974156)!
Body 1 (of 1)
Number of nodes    = 1498
Number of elements = 1496
Number of 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	0m2.823s
user	0m3.088s
sys	0m0.228s
+ 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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       316       634
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       681      1018
AFLR2 GGp: Nodes, Faces      =      1013      1682
AFLR2 GGp: Nodes, Faces      =      1339      2334
AFLR2 GGp: Nodes, Faces      =      1652      2960
AFLR2 GGp: Nodes, Faces      =      1957      3570
AFLR2 GGp: Nodes, Faces      =      2252      4160
AFLR2 GGp: Nodes, Faces      =      2526      4708
AFLR2 GGp: Nodes, Faces      =      2809      5274
AFLR2 GGp: Nodes, Faces      =      3083      5822
AFLR2 GGp: Nodes, Faces      =      3327      6310
AFLR2 GGp: Nodes, Faces      =      3564      6784
AFLR2 GGp: Nodes, Faces      =      3788      7232
AFLR2 GGp: Nodes, Faces      =      3995      7646
AFLR2 GGp: Nodes, Faces      =      4194      8044
AFLR2 GGp: Nodes, Faces      =      4394      8444
AFLR2 GGp: Nodes, Faces      =      4585      8826
AFLR2 GGp: Nodes, Faces      =      4772      9200
AFLR2 GGp: Nodes, Faces      =      4943      9542
AFLR2 GGp: Nodes, Faces      =      5129      9914
AFLR2 GGp: Nodes, Faces      =      5293     10242
AFLR2 GGp: Nodes, Faces      =      5447     10550
AFLR2 GGp: Nodes, Faces      =      5594     10844
AFLR2 GGp: Nodes, Faces      =      5716     11088
AFLR2 GGp: Nodes, Faces      =      5830     11316
AFLR2 GGp: Nodes, Faces      =      5909     11474
AFLR2 GGp: Nodes, Faces      =      5964     11584
AFLR2 GGp: Nodes, Faces      =      6006     11668
AFLR2 GGp: Nodes, Faces      =      6025     11706
AFLR2 GGp: Nodes, Faces      =      6034     11724
 
AFLR2    : CPU Time          =     0.015   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      6034     11724
AFLR2 QI : Nodes, Faces      =      6033       454
AFLR2 QI : Nodes, Faces      =      6033      5634
AFLR2 QI : Nodes, Faces      =      6033     11722
AFLR2 QI : Nodes, Faces      =      6032       462
AFLR2 QI : Nodes, Faces      =      6032      5629
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       456
AFLR2 QI : Nodes, Faces      =      6032      5632
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6032       474
AFLR2 QI : Nodes, Faces      =      6032      5623
AFLR2 QI : Nodes, Faces      =      6032     11720
AFLR2 QI : Nodes, Faces      =      6031       486
AFLR2 QI : Nodes, Faces      =      6031      5616
AFLR2 QI : Nodes, Faces      =      6031       488
AFLR2 QI : Nodes, Faces      =      6031      5616
 
AFLR2    : CPU Time          =     0.007   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

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

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	0m0.900s
user	0m0.979s
sys	0m0.487s
+ 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	0m2.349s
user	0m1.877s
sys	0m0.316s
+ 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	0m2.350s
user	0m2.271s
sys	0m0.586s
+ 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	0m5.295s
user	0m9.275s
sys	0m0.702s
+ 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	0m6.949s
user	0m6.516s
sys	0m0.465s
+ 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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 151209
	Number of elements       = 455692
	Number of triangles      = 14380
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 220260
	Number of pyramids       = 425
	Number of prisms         = 220627
	Number of hexahedrals    = 0

Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_VolMesh.dat ....
Finished writing TECPLOT file


real	0m10.625s
user	0m9.974s
sys	0m0.514s
+ 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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 333411
	Number of elements       = 1070785
	Number of triangles      = 44340
	Number of quadrilatarals = 1613
	Number of tetrahedrals   = 575437
	Number of pyramids       = 327
	Number of prisms         = 449068
	Number of hexahedrals    = 0

Writing TECPLOT file: pyCAPS_AFLR3_VolMesh.dat ....
Finished writing TECPLOT file


real	0m24.819s
user	0m24.024s
sys	0m1.015s
+ 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	0m6.214s
user	0m17.250s
sys	0m5.415s
+ 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 - 30087, elements - 60162
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	0m9.876s
user	0m9.296s
sys	0m0.626s
+ 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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
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=       134       226         0
AFLR4    : Nodes, Trias,Quads=       132       222         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       135       228         0
AFLR4    : Nodes, Trias,Quads=       131       220         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=       184       318         0
AFLR4    : Nodes, Trias,Quads=       178       306         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      1231      2504       464

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      1231      2504

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=       140       234         0
AFLR4    : Nodes, Trias,Quads=       134       222         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       140       234         0
AFLR4    : Nodes, Trias,Quads=       133       220         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=        76       120         0
AFLR4    : Nodes, Trias,Quads=        72       112         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       140       234         0
AFLR4    : Nodes, Trias,Quads=       133       220         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       141       236         0
AFLR4    : Nodes, Trias,Quads=       133       220         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       207       362         0
AFLR4    : Nodes, Trias,Quads=       193       334         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=       203       354         0
AFLR4    : Nodes, Trias,Quads=       193       334         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=        76       120         0
AFLR4    : Nodes, Trias,Quads=        72       112         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=       136       230         0
AFLR4    : Nodes, Trias,Quads=       132       222         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=       137       232         0
AFLR4    : Nodes, Trias,Quads=       132       222         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=       193       336         0
AFLR4    : Nodes, Trias,Quads=       183       316         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      1246      2534       464

OVERALL  : CPU Time          =     0.083   seconds
Body 1 (of 1)
Number of nodes    = 1246
Number of elements = 2534
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 2534
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1246
Total number of elements = 2534
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = cut, index = 2
Number of surface: nodes - 1246, elements - 2534
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.01068
Creating surface mesh ...
Surface mesh seconds:  0.00203
Recovering boundaries...
Boundary recovery seconds:  0.005861
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.001129
Recovering Delaunayness...
Delaunay recovery seconds:  0.002447
Refining mesh...
Refinement seconds:  0.011582
Smoothing vertices...
Mesh smoothing seconds:  0.012829
Improving mesh...
Mesh improvement seconds:  0.00108

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

Output seconds:  0.000375
Total running seconds:  0.048132

Statistics:

  Input points: 1246
  Input facets: 2534
  Input segments: 3777
  Input holes: 0
  Input regions: 2

  Mesh points: 1455
  Mesh tetrahedra: 5105
  Mesh faces: 11319
  Mesh faces on exterior boundary: 2218
  Mesh faces on input facets: 2534
  Mesh edges on input segments: 3777
  Steiner points inside domain: 209

Done meshing using TetGen!

Writing VTK file: volume.vtk....
Finished writing VTK file


real	0m0.874s
user	0m0.718s
sys	0m0.237s
+ 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    = 265
Number of elements = 526
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 526
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 3137
Total number of elements = 6262

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 - 3137, elements - 6262
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.024446
Creating surface mesh ...
Surface mesh seconds:  0.005518
Recovering boundaries...
Boundary recovery seconds:  0.049933
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.005908
Suppressing Steiner points ...
Steiner suppression seconds:  1.4e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.010058
Refining mesh...
  4188 insertions, added 2185 points, 134452 tetrahedra in queue.
  1394 insertions, added 466 points, 139158 tetrahedra in queue.
  1858 insertions, added 424 points, 135152 tetrahedra in queue.
  2477 insertions, added 444 points, 115259 tetrahedra in queue.
  3302 insertions, added 499 points, 69620 tetrahedra in queue.
  4401 insertions, added 357 points, 954 tetrahedra in queue.
Refinement seconds:  0.548055
Smoothing vertices...
Mesh smoothing seconds:  0.365319
Improving mesh...
Mesh improvement seconds:  0.011962
Jettisoning redundant points.

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

Output seconds:  0.002497
Total running seconds:  1.02387

Statistics:

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

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

Done meshing using TetGen!

Writing TECPLOT file: pyCAPS_Tetgen_Test.dat ....
	Binary output is not currently supported for Tecplot output
	..... switching to ASCII!
Finished writing TECPLOT file


real	0m2.503s
user	0m2.346s
sys	0m0.369s
+ 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:  0.15349
Creating surface mesh ...
Surface mesh seconds:  0.009737
Recovering boundaries...
Boundary recovery seconds:  0.064622
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.008579
Recovering Delaunayness...
Delaunay recovery seconds:  0.036576
Refining mesh...
Refinement seconds:  0.174862
Smoothing vertices...
Mesh smoothing seconds:  0.204688
Improving mesh...
Mesh improvement seconds:  0.00744
Jettisoning redundant points.

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

Output seconds:  0.002962
Total running seconds:  0.663256

Statistics:

  Input points: 8995
  Input facets: 18112
  Input segments: 27104
  Input holes: 1
  Input regions: 0

  Mesh points: 7140
  Mesh tetrahedra: 27881
  Mesh faces: 60802
  Mesh faces on exterior boundary: 10080
  Mesh faces on input facets: 10080
  Mesh edges on input segments: 15120
  Steiner points inside domain: 2098

Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.

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


real	0m1.744s
user	0m1.647s
sys	0m0.237s
+ 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:  0.155212
Creating surface mesh ...
Surface mesh seconds:  0.014632
Recovering boundaries...
Boundary recovery seconds:  0.078967
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.007058
Recovering Delaunayness...
Delaunay recovery seconds:  0.070987
Refining mesh...
Refinement seconds:  0.365748
Smoothing vertices...
Mesh smoothing seconds:  0.474958
Improving mesh...
Mesh improvement seconds:  0.013299

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

Output seconds:  0.00424
Total running seconds:  1.18555

Statistics:

  Input points: 8995
  Input facets: 18112
  Input segments: 27104
  Input holes: 0
  Input regions: 2

  Mesh points: 13181
  Mesh tetrahedra: 55765
  Mesh faces: 119562
  Mesh faces on exterior boundary: 16064
  Mesh faces on input facets: 18112
  Mesh edges on input segments: 27104
  Steiner points inside domain: 4186

Done meshing using TetGen!

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


real	0m2.293s
user	0m2.180s
sys	0m0.245s
+ 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	0m0.915s
user	0m0.877s
sys	0m0.482s
+ 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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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          =     0.007   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      3715      7206
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 3715
Number of elements = 7430
Number of tris = 7206
Number of quad = 0

Writing SU2 file ....
SU2 expects 2D meshes 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|  2.8272e-02|   -0.385358|    2.453598|    1.625650|    5.369499|    0.360138|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.7920e-02|   -0.512634|    2.087781|    1.374671|    4.973554|    1.183036|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.7338e-02|   -0.792582|    1.733529|    1.142729|    4.657622|    3.896320|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  2.6868e-02|   -0.880738|    1.486539|    1.023158|    4.334759|   14.592265|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  2.6649e-02|   -0.987528|    1.351478|    0.932491|    4.191092|  111.166022|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  2.6424e-02|   -1.104038|    1.188715|    0.874764|    3.951825| -483.924340|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  2.6258e-02|   -1.178622|    1.124587|    0.844310|    3.820426|  127.331200|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  2.6132e-02|   -1.243517|    1.097463|    0.824869|    3.768858|   40.162273|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  2.6049e-02|   -1.287932|    1.075843|    0.810639|    3.733440|   25.154653|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  2.5983e-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	0m2.014s
user	0m1.310s
sys	0m0.731s
+ 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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       545         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       545       545
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       110       222
AFLR2 IG : Nodes, Faces      =       220       442
AFLR2 IG : Nodes, Faces      =       330       662
AFLR2 IG : Nodes, Faces      =       440       882
AFLR2 IG : Nodes, Faces      =       517      1036
AFLR2 IG : Nodes, Faces      =       545      1092
AFLR2 IG : Nodes, Faces      =       549      1092
AFLR2 IG : Nodes, Faces      =       545       545
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       545       545
AFLR2 GGp: Nodes, Faces      =      1083      1621
AFLR2 GGp: Nodes, Faces      =      1616      2687
AFLR2 GGp: Nodes, Faces      =      2144      3743
AFLR2 GGp: Nodes, Faces      =      2661      4777
AFLR2 GGp: Nodes, Faces      =      3171      5797
AFLR2 GGp: Nodes, Faces      =      3672      6799
AFLR2 GGp: Nodes, Faces      =      4158      7771
AFLR2 GGp: Nodes, Faces      =      4653      8761
AFLR2 GGp: Nodes, Faces      =      5142      9739
AFLR2 GGp: Nodes, Faces      =      5608     10671
AFLR2 GGp: Nodes, Faces      =      6055     11565
AFLR2 GGp: Nodes, Faces      =      6482     12419
AFLR2 GGp: Nodes, Faces      =      6880     13215
AFLR2 GGp: Nodes, Faces      =      7257     13969
AFLR2 GGp: Nodes, Faces      =      7614     14683
AFLR2 GGp: Nodes, Faces      =      7947     15349
AFLR2 GGp: Nodes, Faces      =      8276     16007
AFLR2 GGp: Nodes, Faces      =      8575     16605
AFLR2 GGp: Nodes, Faces      =      8869     17193
AFLR2 GGp: Nodes, Faces      =      9140     17735
AFLR2 GGp: Nodes, Faces      =      9401     18257
AFLR2 GGp: Nodes, Faces      =      9654     18763
AFLR2 GGp: Nodes, Faces      =      9887     19229
AFLR2 GGp: Nodes, Faces      =     10110     19675
AFLR2 GGp: Nodes, Faces      =     10315     20085
AFLR2 GGp: Nodes, Faces      =     10497     20449
AFLR2 GGp: Nodes, Faces      =     10656     20767
AFLR2 GGp: Nodes, Faces      =     10791     21037
AFLR2 GGp: Nodes, Faces      =     10919     21293
AFLR2 GGp: Nodes, Faces      =     11022     21499
AFLR2 GGp: Nodes, Faces      =     11092     21639
AFLR2 GGp: Nodes, Faces      =     11145     21745
AFLR2 GGp: Nodes, Faces      =     11156     21767
 
AFLR2    : CPU Time          =     0.032   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     11156     21767
AFLR2 QI : Nodes, Faces      =     11155       819
AFLR2 QI : Nodes, Faces      =     11155     10473
AFLR2 QI : Nodes, Faces      =     11155     21765
AFLR2 QI : Nodes, Faces      =     11154       811
AFLR2 QI : Nodes, Faces      =     11154     10476
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11154       805
AFLR2 QI : Nodes, Faces      =     11154     10479
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11154       911
AFLR2 QI : Nodes, Faces      =     11154     10426
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11153       915
AFLR2 QI : Nodes, Faces      =     11153     10423
AFLR2 QI : Nodes, Faces      =     11153       917
AFLR2 QI : Nodes, Faces      =     11153     10423
 
AFLR2    : CPU Time          =     0.012   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|  7.3799e-02|    0.071067|    2.739763|    1.616077|    5.599701|    0.055267|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  7.1669e-02|   -0.447576|    2.193837|    1.571349|    5.070382|    0.046028|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  6.9908e-02|   -0.561159|    2.074597|    1.490746|    4.953698|    0.033910|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  6.9604e-02|   -0.723326|    1.921155|    1.390756|    4.790278|    0.049695|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  6.8823e-02|   -0.876572|    1.825653|    1.275093|    4.637161|    0.133976|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  6.8611e-02|   -1.029177|    1.759196|    1.156078|    4.482282|    0.368542|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  6.8103e-02|   -1.215334|    1.704909|    1.114966|    4.286060|    0.974759|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  6.7791e-02|   -1.329970|    1.644937|    1.145030|    4.116982|    2.716332|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  6.7424e-02|   -1.270672|    1.570739|    1.155400|    4.139480|   16.569216|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  6.7103e-02|   -1.221243|    1.499646|    1.130319|    4.189559|   -6.277653|

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

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

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

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

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

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

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

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

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

real	0m2.266s
user	0m2.112s
sys	0m0.953s
+ 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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 39312
	Number of elements       = 226864
	Number of triangles      = 12446
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 214418
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: 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.
39312 grid points.
214418 volume elements.
4 surface markers.
6594 boundary elements in index 0 (Marker = BC_1).
5358 boundary elements in index 1 (Marker = BC_2).
74 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
214418 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08667e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 4873.1. Mean K: 61.8682. Standard deviation K: 266.942.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        17.1608|         84.739|
|     CV Face Area Aspect Ratio|        1.11815|        37015.5|
|           CV Sub-Volume Ratio|        1.04044|         455686|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     39312|    1/1.00|        10|
|         1|      6485|    1/6.06|   8.22658|
|         2|      1015|    1/6.39|   6.65012|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 118.038 m^2.
Area projection in the x-plane = 11.1419 m^2, y-plane = 4.96714 m^2, z-plane = 55.4182 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.582636 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  8.9762e-01|   -0.064586|    2.297676|    2.033300|    5.426310|    1.967108|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  8.7519e-01|   -0.028142|    2.443813|    2.177084|    5.469820|    2.669025|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  8.6332e-01|    0.006388|    2.521945|    2.416533|    5.497519|    4.072698|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  8.6526e-01|   -0.032771|    2.543134|    2.541766|    5.444377|    5.959388|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  8.5885e-01|   -0.059484|    2.561671|    2.593774|    5.414288|    7.593451|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  8.5474e-01|   -0.076814|    2.565225|    2.615896|    5.407625|    8.782803|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  8.5659e-01|   -0.111978|    2.544207|    2.636258|    5.381265|    9.653546|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  8.5728e-01|   -0.156369|    2.495539|    2.651467|    5.333878|   10.185394|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  8.5799e-01|   -0.203072|    2.428150|    2.650114|    5.275471|   10.322264|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  8.5873e-01|   -0.251896|    2.375012|    2.624886|    5.221589|   10.161308|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|     -0.251896|          < -8|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_su2AFLRTest.dat       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|CSV file                           |surface_flow_su2AFLRTest.csv       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview                           |flow_su2AFLRTest.vtu               |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview surface                   |surface_flow_su2AFLRTest.vtu       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
+-----------------------------------------------------------------------+

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

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

Total Force - Pressure + Viscous
Cl =  0.796713 Cd =  0.078407
Cmx =  0.000211 Cmy =  -0.204659 Cmz =  0.000288
Cx =  0.06449 Cy =  0.000454 Cz =  0.79796
Pressure Contribution
Cl_p =  0.796713 Cd_p =  0.078407
Cmx_p =  0.000211 Cmy_p =  -0.204659 Cmz_p =  0.000288
Cx_p =  0.06449 Cy_p =  0.000454 Cz_p =  0.79796
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmx_v =  0.0 Cmy_v =  0.0 Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0 Cz_v =  0.0

real	0m30.387s
user	0m29.303s
sys	0m0.994s
+ 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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 56062
	Number of elements       = 324627
	Number of triangles      = 15872
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 308755
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: 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.
56062 grid points.
308755 volume elements.
4 surface markers.
9958 boundary elements in index 0 (Marker = BC_1).
5414 boundary elements in index 1 (Marker = BC_2).
80 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
308755 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08667e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 5523.74. Mean K: 58.8177. Standard deviation K: 282.533.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        25.8353|        86.1799|
|     CV Face Area Aspect Ratio|        1.02126|        47603.8|
|           CV Sub-Volume Ratio|        1.04989|         165826|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     56062|    1/1.00|        10|
|         1|      9228|    1/6.08|   8.22061|
|         2|      1406|    1/6.56|     6.586|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.07107 m.
Wetted area = 96.2324 m^2.
Area projection in the x-plane = 7.65774 m^2, y-plane = 4.21853 m^2, z-plane = 45.5887 m^2.
Max. coordinate in the x-direction = 12.3872 m, y-direction = 7.07107 m, z-direction = 0.521791 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.0650201 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.4424e+00|   -0.457870|    1.873279|    1.656710|    5.033025|    0.755651|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.3753e+00|   -0.472284|    2.010746|    1.748231|    5.024932|    1.425370|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.3291e+00|   -0.414217|    2.107665|    1.963200|    5.074925|    3.245288|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.3121e+00|   -0.400337|    2.167522|    2.099318|    5.078948|    7.034217|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.3010e+00|   -0.401529|    2.203755|    2.175567|    5.071313|   12.883621|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.2970e+00|   -0.407291|    2.221380|    2.217144|    5.067540|   20.159074|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.2922e+00|   -0.411436|    2.211548|    2.246056|    5.067163|   27.796880|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.2871e+00|   -0.418757|    2.160924|    2.267618|    5.055632|   32.034412|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.2823e+00|   -0.438528|    2.092229|    2.272883|    5.027335|   30.335774|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.2794e+00|   -0.487870|    2.016953|    2.255847|    4.971131|   25.705102|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -0.48787|          < -8|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_su2AFLRTest.dat       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|CSV file                           |surface_flow_su2AFLRTest.csv       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview                           |flow_su2AFLRTest.vtu               |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview surface                   |surface_flow_su2AFLRTest.vtu       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
+-----------------------------------------------------------------------+

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

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

Total Force - Pressure + Viscous
Cl =  0.52174 Cd =  0.020297
Projecting tessellation 1 (of 4) on to new body
Projecting tessellation 2 (of 4) on to new body
Projecting tessellation 3 (of 4) on to new body
Projecting tessellation 4 (of 4) on to new body
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wake
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing SU2 surface file
Writing SU2 Motion File - su2AFLRTest_motion.dat
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 15
 - bcProps.surfaceProp[2].surfaceType = 1
 - bcProps.surfaceProp[3].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.0) "


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.
56062 grid points.
308755 volume elements.
4 surface markers.
9958 boundary elements in index 0 (Marker = BC_1).
5414 boundary elements in index 1 (Marker = BC_2).
80 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
308755 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 2.08667e+06.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Ignoring Convergence Field(s): RMS_DENSITY 
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 10.928994 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.
56062 grid points.
308755 volume elements.
4 surface markers.
9958 boundary elements in index 0 (Marker = BC_1).
5414 boundary elements in index 1 (Marker = BC_2).
80 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
308755 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08667e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 5523.56. Mean K: 58.7619. Standard deviation K: 282.437.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        17.0659|        85.7425|
|     CV Face Area Aspect Ratio|        1.02723|        55937.4|
|           CV Sub-Volume Ratio|        1.05439|         215979|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     56062|    1/1.00|        10|
|         1|      9228|    1/6.08|   8.22061|
|         2|      1406|    1/6.56|     6.586|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.07107 m.
Wetted area = 95.6308 m^2.
Area projection in the x-plane = 9.17945 m^2, y-plane = 4.04295 m^2, z-plane = 44.962 m^2.
Max. coordinate in the x-direction = 12.3585 m, y-direction = 7.07107 m, z-direction = 0.521791 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.400127 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.2854e+00|   -0.397349|    1.978876|    1.645486|    5.093547|    1.917484|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.2731e+00|   -0.252045|    2.234760|    1.970250|    5.252026|    2.558863|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.2687e+00|   -0.196042|    2.339633|    2.224120|    5.301659|    3.948869|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.2647e+00|   -0.220076|    2.386540|    2.365409|    5.264943|    5.948479|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.2625e+00|   -0.253573|    2.408600|    2.430554|    5.223815|    7.864579|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.2621e+00|   -0.270783|    2.418936|    2.458803|    5.218653|    9.389224|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.2616e+00|   -0.286712|    2.403031|    2.476999|    5.213229|   10.603736|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.2591e+00|   -0.315381|    2.351751|    2.489815|    5.182543|   11.481006|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.2572e+00|   -0.352500|    2.274582|    2.487389|    5.133384|   11.951691|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.2560e+00|   -0.405104|    2.187417|    2.462671|    5.069866|   12.022914|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|     -0.405104|          < -8|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_su2AFLRTest.dat       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|CSV file                           |surface_flow_su2AFLRTest.csv       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview                           |flow_su2AFLRTest.vtu               |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview surface                   |surface_flow_su2AFLRTest.vtu       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
+-----------------------------------------------------------------------+

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

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

Total Force - Pressure + Viscous
Cl =  0.883374 Cd =  0.073474

real	1m1.858s
user	0m55.458s
sys	0m3.775s
+ 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.
6320 grid points.
12346 volume elements.
5 surface markers.
24 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_2).
24 boundary elements in index 3 (Marker = BC_4).
198 boundary elements in index 4 (Marker = BC_5).
12346 triangles.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
There has been a re-orientation of 294 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.917.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 1792.95. Mean K: 10.8142. Standard deviation K: 104.33.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        45.3524|        89.3051|
|     CV Face Area Aspect Ratio|         1.0235|        15.7138|
|           CV Sub-Volume Ratio|              1|        7.93643|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      6320|    1/1.00|        10|
|         1|      1790|    1/3.53|   7.98287|
|         2|       504|    1/3.55|   6.35388|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.07206 m.
Area projection in the x-plane = 0.179342 m, y-plane = 1.00053 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.138492 m.
Min. coordinate in the x-direction = -0.00104578 m, y-direction = -0.0151891 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is a single straight.
Computing wall distances.

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

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

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  5.4259e-02|   -1.163171|    1.073770|    1.341444|    4.312165|    0.062120|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  5.2233e-02|   -1.561828|    0.808636|    0.967487|    3.922716|    0.139775|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  5.1630e-02|   -1.601698|    0.943793|    1.009036|    3.876382|    0.373708|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  5.1259e-02|   -1.659374|    1.008221|    1.015635|    3.799753|    0.952935|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  5.0952e-02|   -1.663585|    1.011627|    0.956487|    3.788246|    2.344781|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  5.1037e-02|   -1.633451|    0.991734|    0.872954|    3.829708|    6.259549|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  5.0977e-02|   -1.626398|    0.990123|    0.847075|    3.843511|   26.349556|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  5.1460e-02|   -1.643439|    1.009125|    0.895796|    3.825758|  -56.104876|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  5.1019e-02|   -1.659565|    1.020774|    0.939260|    3.804303|  -24.431167|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  5.0619e-02|   -1.676757|    1.012633|    0.938320|    3.783310|  -21.456835|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.67676|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_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 =  0.805231 Cd =  -0.037528
Cmz =  0.414714
Cx =  -0.037528 Cy =  0.805231
Pressure Contribution
Cl_p =  0.805231 Cd_p =  -0.037528
Cmz_p =  0.414714
Cx_p =  -0.037528 Cy_p =  0.805231
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0

real	0m2.337s
user	0m1.647s
sys	0m0.776s
+ 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    = 265
Number of elements = 526
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 526
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 3137
Total number of elements = 6262

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 - 3137, elements - 6262
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.022406
Creating surface mesh ...
Surface mesh seconds:  0.006076
Recovering boundaries...
Boundary recovery seconds:  0.069179
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.00679
Suppressing Steiner points ...
Steiner suppression seconds:  1.2e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.009832
Refining mesh...
  4186 insertions, added 2132 points, 130189 tetrahedra in queue.
  1393 insertions, added 396 points, 133609 tetrahedra in queue.
  1857 insertions, added 413 points, 131356 tetrahedra in queue.
  2476 insertions, added 454 points, 112928 tetrahedra in queue.
  3300 insertions, added 466 points, 67068 tetrahedra in queue.
  4399 insertions, added 435 points, 292 tetrahedra in queue.
  5864 insertions, added 590 points, 479 tetrahedra in queue.
Refinement seconds:  0.548763
Smoothing vertices...
Mesh smoothing seconds:  0.301195
Improving mesh...
Mesh improvement seconds:  0.009095
Jettisoning redundant points.

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

Output seconds:  0.001597
Total running seconds:  0.975204

Statistics:

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

  Mesh points: 8091
  Mesh tetrahedra: 39789
  Mesh faces: 82710
  Mesh faces on exterior boundary: 6264
  Mesh faces on input facets: 6264
  Mesh edges on input segments: 9394
  Steiner points on input segments:  1
  Steiner points inside domain: 4953

Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.0) "


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.
8091 grid points.
39789 volume elements.
3 surface markers.
4468 boundary elements in index 0 (Marker = BC_1).
1270 boundary elements in index 1 (Marker = BC_2).
526 boundary elements in index 2 (Marker = BC_3).
39789 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08926e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 414.134. Mean K: 30.5804. Standard deviation K: 37.5377.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        1.66644|        84.3027|
|     CV Face Area Aspect Ratio|        1.51408|         6441.7|
|           CV Sub-Volume Ratio|        1.03202|        58553.9|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      8091|    1/1.00|        10|
|         1|      1351|    1/5.99|   8.25992|
|         2|       223|    1/6.06|   6.79647|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 120.046 m^2.
Area projection in the x-plane = 10.7914 m^2, y-plane = 4.58502 m^2, z-plane = 57.287 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.557773 m.
Min. coordinate in the x-direction = -0.00409054 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.5643e-01|    0.617984|    3.049944|    2.093190|    6.108879|    1.810742|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.5588e-01|    0.748911|    3.251769|    2.987153|    6.248586|    2.155825|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.5499e-01|    0.688623|    3.311837|    3.249508|    6.186781|    3.173369|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.5427e-01|    0.587426|    3.265724|    3.310895|    6.060983|    4.532123|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.5477e-01|    0.563655|    3.196458|    3.256149|    6.028232|    5.638253|

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

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      0.563655|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_SU2_Tetgen.dat |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|CSV file                           |surface_flow_pyCAPS_SU2_Tetgen.csv |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview                           |flow_pyCAPS_SU2_Tetgen.vtu         |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview surface                   |surface_flow_pyCAPS_SU2_Tetgen.vtu |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
+-----------------------------------------------------------------------+

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

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

Total Force - Pressure + Viscous
Cl =  0.751804 Cd =  0.13334
Cmx =  -0.004647 Cmy =  -0.210652 Cmz =  0.001238
Cx =  0.120199 Cy =  0.000192 Cz =  0.754017

real	0m11.698s
user	0m11.158s
sys	0m0.634s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_Tetgen_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_X43a_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_X43a_PyTest.py test;
+ python -u su2_X43a_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = x43A, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 3808
Number of elements = 7616
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 7616
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 5654
Number of elements = 11304
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 11304
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9462
Total number of elements = 18920

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 - 9462, elements - 18920
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.051991
Creating surface mesh ...
Surface mesh seconds:  0.014365
Recovering boundaries...
Warning:  6 segments are not recovered.
Boundary recovery seconds:  0.15364
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.011105
Suppressing Steiner points ...
Steiner suppression seconds:  1.7e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.020054
Refining mesh...
  12618 insertions, added 5274 points, 8959 tetrahedra in queue.
Refinement seconds:  0.499741
Smoothing vertices...
Mesh smoothing seconds:  0.412237
Improving mesh...
Mesh improvement seconds:  0.014566
Jettisoning redundant points.

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

Output seconds:  0.004489
Total running seconds:  1.18628

Statistics:

  Input points: 9462
  Input facets: 18920
  Input segments: 28380
  Input holes: 1
  Input regions: 0

  Mesh points: 14879
  Mesh tetrahedra: 61475
  Mesh faces: 132413
  Mesh faces on exterior boundary: 18926
  Mesh faces on input facets: 18926
  Mesh edges on input segments: 28383
  Steiner points on input segments:  3
  Steiner points inside domain: 5414

Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - x43A
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.0) "


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.
14879 grid points.
61475 volume elements.
2 surface markers.
7622 boundary elements in index 0 (Marker = BC_1).
11304 boundary elements in index 1 (Marker = BC_2).
61475 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.67744e+08.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 95.6599. Mean K: 0.525129. Standard deviation K: 2.57985.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        1.97178|        85.1584|
|     CV Face Area Aspect Ratio|        1.89387|        2232.84|
|           CV Sub-Volume Ratio|              1|         662807|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     14879|    1/1.00|        10|
|         1|      2664|    1/5.59|   8.45431|
|         2|       482|    1/5.53|   7.17255|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30 m.
Wetted area = 13596.7 m^2.
Area projection in the x-plane = 761.676 m^2, y-plane = 2062.48 m^2, z-plane = 5463.61 m^2.
Max. coordinate in the x-direction = 150 m, y-direction = 30 m, z-direction = 19 m.
Min. coordinate in the x-direction = 0 m, y-direction = -30 m, z-direction = -10.3 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        916077|             1|   m^2/s^2|        916077|
|            Velocity-X|       1189.41|             1|       m/s|       1189.41|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       62.3342|             1|       m/s|       62.3342|
|    Velocity Magnitude|       1191.04|             1|       m/s|       1191.04|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           3.5|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.9794e-01|    2.730957|    5.664998|    4.728682|    8.730433|   -0.398804|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.8996e-01|    3.137446|    6.177776|    5.665282|    9.126833|   -0.137986|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.8611e-01|    3.221739|    6.293564|    5.717532|    9.173826|   -0.037061|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  2.8331e-01|    3.189146|    6.230574|    5.640455|    9.149183|   -0.012053|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  2.8200e-01|    3.223156|    6.256981|    5.536034|    9.185450|   -0.028725|

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

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       3.22316|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_x43a_Test.dat         |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|CSV file                           |surface_flow_x43a_Test.csv         |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|Paraview                           |flow_x43a_Test.vtu                 |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|Paraview surface                   |surface_flow_x43a_Test.vtu         |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
+-----------------------------------------------------------------------+
Warning: there are 124 non-physical points in the solution.
Warning: 85 reconstructed states for upwinding are non-physical.

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

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

Total Force - Pressure + Viscous
Cl =  -3.497481 Cd =  121.75903
Cmx =  -17.512377 Cmy =  9356.955958 Cmz =  278.947628
Cx =  121.775208 Cy =  2.435697 Cz =  2.879687

real	0m7.607s
user	0m9.748s
sys	0m1.224s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_X43a_PyTest.py passed (as expected)
=================================================

./execute_PyTestRegression.sh: line 413: ulimit: stack size: cannot modify limit: Operation not permitted
flowCart: /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC//flowCart

=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ python -u cart3d_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.796888
 Tessellating body 1 with  MaxEdge = 0.094922  Sag = 0.003797  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 6 -maxR 9  > autoInputs.out
 Executing: ./aero.csh > aero.out
C_A  0.023693377
C_Y  -0.0012129281
C_N  0.065395002
C_D  0.025961197
C_S  -0.0012129281
C_L  0.064528278
C_l  0.0510971
C_m  0.000248187
C_n  -0.017525
C_M_x  0.0504544
C_M_y  0.000248187
C_M_z  -0.0192976

real	0m14.181s
user	0m25.247s
sys	0m0.750s
+ 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
   (20:48:56) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (20:48:59) 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
   (20:49:00) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (20:49:02) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (20:49:02) Linearizing cut-cells
   (20:49:02) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:49:03) Computing gradients
   (20:49:07) ... 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
   (20:49:08) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1
   (20:49:10) 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
   (20:49:11) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1
   (20:49:13) 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
   (20:49:14) Linearizing cut-cells
   (20:49:14) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:49:14) Computing gradients
   (20:49:18) ... 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
   (20:49:19) Running aero.csh on 2 core(s) in M0.5901A-0.0109918B0_DP1
   (20:49:21) aero.csh done
 o case M0.5901A-0.0109918B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [6.05653687e-06]  CL 0.00246101
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:49:22) Running aero.csh on 2 core(s) in M0.5901A-0.0109918B0_DP1
   (20:49:24) 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
   (20:49:25) Linearizing cut-cells
   (20:49:25) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:49:25) Computing gradients
   (20:49:29) ... done
 o case M0.5901A-0.0109918B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[0.00031042]]
========================================

At iterate    2    f=  6.05654D-06    |proj g|=  3.10424D-04
----------------------------------------
>>> alpha [-0.05149286]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:49:30) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1
   (20:49:32) aero.csh done
 o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [2.59817201e-10]  CL 1.612e-05
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:49:33) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1
   (20:49:35) 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
   (20:49:36) Linearizing cut-cells
   (20:49:36) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:49:36) Computing gradients
   (20:49:40) ... done
 o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[2.03612486e-06]]
========================================

At iterate    3    f=  2.59817D-10    |proj g|=  2.03612D-06
----------------------------------------
>>> alpha [-0.05176027]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:49:41) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1
   (20:49:43) aero.csh done
 o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [9.26120217e-15]  CL 1e-07
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:49:44) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1
   (20:49:46) 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
   (20:49:47) Linearizing cut-cells
   (20:49:47) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:49:47) Computing gradients
   (20:49:51) ... done
 o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[1.21394333e-08]]
========================================

At iterate    4    f=  9.26120D-15    |proj g|=  1.21394D-08

           * * *

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

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    1      4      5      4     0     0   1.214D-08   9.261D-15
  F =   9.2612021713000013E-015

CONVERGENCE: NORM_OF_PROJECTED_GRADIENT_<=_PGTOL            
Optimization Complete
-----------------------------------
Optimized value: [-0.05176027]

real	1m1.164s
user	0m41.882s
sys	0m9.082s
+ 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
   (20:49:54) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:50:06) 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
   (20:50:07) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:50:25) 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
   (20:50:26) Linearizing cut-cells
   (20:50:28) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:50:28) Computing gradients
   (20:50:32) ... 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
   (20:50:34) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:50:48) 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
   (20:50:49) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:51:07) 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
   (20:51:07) Linearizing cut-cells
   (20:51:09) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:51:09) Computing gradients
   (20:51:13) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[0.00210014]]
========================================

At iterate    1    f=  4.11230D-03    |proj g|=  2.10014D-03
----------------------------------------
>>> twist [-6.47168788]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.635635
 Tessellating body 1 with  MaxEdge = 0.018178  Sag = 0.000909  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:51:15) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:51:27) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.00980712]  CL -0.0990178
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:51:29) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:51:47) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               37091
              Estimated cutter memory:  0.003709 GB / DV
              Estimated xsensit memory: 0.070473 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (20:51:48) Linearizing cut-cells
   (20:51:50) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:51:50) Computing gradients
   (20:51:54) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[-0.00318447]]
========================================
----------------------------------------
>>> twist [-0.15773834]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.625777
 Tessellating body 1 with  MaxEdge = 0.018129  Sag = 0.000906  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:51:56) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:52:08) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [2.57285894e-07]  CL -0.00057627
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:52:09) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:52:26) 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
   (20:52:26) Linearizing cut-cells
   (20:52:28) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:52:28) Computing gradients
   (20:52:32) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[-1.67855749e-05]]
========================================

At iterate    2    f=  2.57286D-07    |proj g|=  1.67856D-05
----------------------------------------
>>> twist [-0.12478737]
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.625742
 Tessellating body 1 with  MaxEdge = 0.018129  Sag = 0.000906  Angle = 10.000000
 Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7  -symmY -halfBody > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:52:34) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:52:46) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [1.79305104e-08]  CL 0.00016606
----------------------------------------
========================================
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (20:52:48) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (20:53:05) 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
   (20:53:05) Linearizing cut-cells
   (20:53:07) ... done
   o Number of simultaneous xsensit jobs:  1
   (20:53:07) Computing gradients
   (20:53:11) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[4.43473007e-06]]
========================================

At iterate    3    f=  1.79305D-08    |proj g|=  4.43473D-06

           * * *

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

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    1      3      5      3     0     0   4.435D-06   1.793D-08
  F =   1.7930510393000000E-008

CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-0.12478737]

real	3m20.566s
user	5m0.426s
sys	0m10.445s
+ 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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 79623
	Number of elements       = 464233
	Number of triangles      = 15680
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 448553
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing TECPLOT file: 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	0m8.998s
user	0m8.157s
sys	0m0.813s
+ 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      3.428666259747
Mass      5383.006027803
Centroid  [1.222256036874, 0.1634981473778, -4.234377369776e-11]
CG        [1.222256036874, 0.1634981473778, -4.234490614246e-11]
Ixx       22133.97306033
Iyy       23448.30046709
Izz       1389.213122582
Ixy       164.2055275657
Ixz       -7.454850140458e-06
Iyz       1.707682988152e-06
I         [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.454850140458e-06, 1.707682988152e-06]
II        [[22133.97306033, -164.2055275657, 7.454850140458e-06], [-164.2055275657, 23448.30046709, -1.707682988152e-06], [7.454850140458e-06, -1.707682988152e-06, 1389.213122582]]

real	0m4.888s
user	0m11.513s
sys	0m10.437s
+ 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	0m0.594s
user	0m0.528s
sys	0m0.198s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case masstran_AGARD445_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

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

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

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

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

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

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

real	0m0.974s
user	0m0.910s
sys	0m0.154s
+ status=0
+ set +x

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


=================================================
+ echo 'hsm_CantileverPlate_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_CantileverPlate_PyTest.py test;
+ python -u hsm_CantileverPlate_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = plate, index = 1

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

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

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

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

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

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

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

 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.314E+01  0.628E+01  0.000E+00    0.080  ddx @ (   1.00   0.00   0.00)
   1*   0.341E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   1*   0.326E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.03   0.00)
   1*   0.438E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   2    0.274E+01  0.521E+01  0.106E-07    0.096  ddx @ (   1.00   0.03   0.00)
   2*   0.321E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   2*   0.373E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   2*   0.777E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3    0.202E+01  0.439E+01  0.928E-07    0.114  ddz @ (   1.00   0.03   0.00)
   3*   0.442E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.623E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.163E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.07   0.00)
   3*   0.167E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4    0.192E+01  0.476E+01  0.126E-07    0.105  ddz @ (   1.00   0.03   0.00)
   4*   0.335E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.332E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   4*   0.451E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
   5    0.187E+01  0.394E+01  0.254E-07    0.127  ddz @ (   1.00   0.07   0.00)
   5*   0.353E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   5*   0.379E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   5*   0.638E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   6    0.156E+01  0.300E+01  0.112E-06    0.166  ddx @ (   1.00   0.03   0.00)
   6*   0.326E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   6*   0.575E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   6*   0.193E-03  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   6*   0.272E-06  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   7    0.103E+01  0.323E+01  0.345E-07    0.155  ddx @ (   1.00   0.03   0.00)
   7*   0.259E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7*   0.297E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   7*   0.435E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.10   0.00)
   8    0.756E+00  0.259E+01  0.139E-07    0.193  ddx @ (   1.00   0.07   0.00)
   8*   0.295E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   8*   0.350E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   8*   0.587E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9    0.678E+00  0.179E+01  0.639E-07    0.279  ddx @ (   0.89   0.10   0.00)
   9*   0.330E-01  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9*   0.457E-02  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
   9*   0.167E-03  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
   9*   0.264E-06  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  10    0.452E+00  0.171E+01  0.499E-07    0.292  ddz @ (   1.00   0.00   0.00)
  10*   0.166E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10*   0.239E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  10*   0.393E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.10   0.00)
  iter     dr         dd         dp         rlx   max
  11    0.257E+00  0.120E+01  0.614E-08    0.417  ddz @ (   1.00   0.10   0.00)
  11*   0.206E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  11*   0.283E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  11*   0.488E-04  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12    0.131E+00  0.647E+00  0.288E-08    0.772  ddz @ (   0.89   0.10   0.00)
  12*   0.238E-01  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.357E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  12*   0.849E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
  13    0.393E-01  0.238E+00  0.325E-07    1.000  ddx @ (   1.00   0.03   0.00)
  13*   0.336E-02  0.000E+00  0.000E+00    1.000  drz @ (   1.00   0.00   0.00)
  13*   0.936E-04  0.000E+00  0.000E+00    1.000  drx @ (   1.00   0.00   0.00)
  14    0.475E-03  0.514E-02  0.635E-07    1.000  ddx @ (   1.00   0.00   0.00)
  15    0.893E-06  0.651E-06  0.135E-08    1.000  drx @ (   1.00   0.10   0.00)
  16    0.574E-10  0.216E-09  0.140E-11    1.000  ddx @ (   0.44   0.10   0.00)
  17    0.558E-15  0.304E-14  0.603E-15    1.000  ddx @ (   1.00   0.00   0.00)

 Converging n vectors ...
 it =  1    dn =  0.193E+01   rlx = 1.000  (  12 )
 it =  2    dn =  0.435E-15   rlx = 1.000  (  28 )

 Converging e1,e2 vectors ...
 it =  1    de =  0.285E+01   rlx = 0.351  (  24 )
 it =  2    de =  0.292E+01   rlx = 0.342  (  34 )
 it =  3    de =  0.226E+01   rlx = 0.442  (  34 )
 it =  4    de =  0.151E+01   rlx = 0.660  (  34 )
 it =  5    de =  0.665E+00   rlx = 1.000  (  34 )
 it =  6    de =  0.609E-01   rlx = 1.000  (  34 )
 it =  7    de =  0.573E-04   rlx = 1.000  (  34 )
 it =  8    de =  0.478E-13   rlx = 1.000  (  34 )

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

real	0m0.753s
user	0m0.744s
sys	0m0.154s
+ status=0
+ set +x

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

ASTROS_ROOT: /Users/jenkins/util/astros/Astros/Darwin-64bit

=================================================
+ echo 'astros_Aeroelastic_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Aeroelastic_PyTest.py test;
+ python -u astros_Aeroelastic_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
	Name = Wing, index = 7
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 366
	Number of elements = 523
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 190
	Elemental Quad4 = 333
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 367
	Combined Number of elements = 524
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 190
	Combined Elemental Quad4 = 333
Getting vortex lattice surface data
	VLM surface name - Skin_Top
	Done getting vortex lattice surface data
Getting vortex lattice control surface data
	VLM control surface name - CntrlLE
	VLM control surface name - CntrlTE
	Done getting vortex lattice control surface data

Getting FEA vortex lattice mesh
	Surface 1: Number of points found for aero-spline = 48
	(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or  'Fin' single surfaces !

Getting Aero Reference Parameters.......

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

Getting FEA properties.......
	Number of properties - 5
	Property name - Rib_Root
	No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
	Property name - Ribs
	No "material" specified for Property tuple Ribs, defaulting to an index of 1
	Property name - Skin
	No "material" specified for Property tuple Skin, defaulting to an index of 1
	Property name - Spar1
	No "material" specified for Property tuple Spar1, defaulting to an index of 1
	Property name - Spar2
	No "material" specified for Property tuple Spar2, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input

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

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

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Rib_Root
	No "groupName" specified for Connection tuple Rib_Root!
	Looking for automatic connections from the use of capsConnectLink for Rib_Root
	42 automatic connections were made for capsConnect Rib_Root (node id 367)
	Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

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

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

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

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

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

real	0m8.865s
user	0m19.714s
sys	0m7.253s
+ 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	0m0.790s
user	0m0.629s
sys	0m0.261s
+ 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	0m0.876s
user	0m0.710s
sys	0m0.287s
+ status=0
+ set +x

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


=================================================
+ echo 'astros_CompositeWingFreq_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_CompositeWingFreq_PyTest.py test;
+ python -u astros_CompositeWingFreq_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results for natural frequencies.....
Mapping Csys attributes ................
	Number of unique Csys attributes = 1
	Name = wing, index = 1

Getting FEA coordinate systems.......
	Number of coordinate systems - 1
	Coordinate system name - wing
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = wing, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = wing, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 429
	Number of elements = 817
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 817
	Elemental Quad4 = 0
Aero_Reference value is NULL - No aero reference parameters set

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

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - root
	No "constraintType" specified for Constraint tuple root, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
	Writing coordinate system cards
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 10
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
	Loading Eigen-Value = 4
	Loading Eigen-Value = 5
	Loading Eigen-Value = 6
	Loading Eigen-Value = 7
	Loading Eigen-Value = 8
	Loading Eigen-Value = 9
	Loading Eigen-Value = 10
Natural freq (Mode 1) = 5.91949 (Hz)
Natural freq (Mode 2) = 29.79990 (Hz)
Natural freq (Mode 3) = 39.10550 (Hz)
Natural freq (Mode 4) = 77.71580 (Hz)
Natural freq (Mode 5) = 99.79550 (Hz)
Natural freq (Mode 6) = 146.97500 (Hz)
Natural freq (Mode 7) = 176.90300 (Hz)
Natural freq (Mode 8) = 235.53300 (Hz)
Natural freq (Mode 9) = 274.42600 (Hz)
Natural freq (Mode 10) = 311.35900 (Hz)
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 429 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 429 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 429 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 429 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10
Reading Astros OUT file - extracting Eigen-Vectors!
	Number of Eigen-Vectors = 10
	Number of Grid Points = 429 for each Eigen-Vector
	Loading Eigen-Vector = 1
	Loading Eigen-Vector = 2
	Loading Eigen-Vector = 3
	Loading Eigen-Vector = 4
	Loading Eigen-Vector = 5
	Loading Eigen-Vector = 6
	Loading Eigen-Vector = 7
	Loading Eigen-Vector = 8
	Loading Eigen-Vector = 9
	Loading Eigen-Vector = 10

real	0m30.946s
user	0m30.054s
sys	0m0.820s
+ status=0
+ set +x

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


=================================================
+ echo 'astros_Flutter_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Flutter_15degree.py test;
+ python -u astros_Flutter_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

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

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

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

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

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

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

real	0m1.198s
user	0m0.895s
sys	0m0.388s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected)
=================================================


=================================================
+ echo 'astros_MultipleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_MultipleLoadCase_PyTest.py test;
+ python -u astros_MultipleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 16
	Number of elements = 9
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 9
Aero_Reference value is NULL - No aero reference parameters set

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

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

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

Getting FEA loads.......
	Number of loads - 5
	Load name - load_0
	Load name - load_1
	Load name - load_2
	Load name - load_3
	Load name - load_4
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

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

Getting FEA analyses.......
	Number of analyses - 5
	Analysis name - load_0
	Analysis name - load_1
	Analysis name - load_2
	Analysis name - load_3
	Analysis name - load_4
	Done getting FEA analyses

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case load_0, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_1, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_2, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_3, assuming all constraints are applied!!!!
	Warning: No constraints specified for case load_4, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load ADD cards
	Writing constraint cards--all constraints for each subcase
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL

real	0m0.952s
user	0m0.796s
sys	0m0.289s
+ 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	0m11.709s
user	0m17.719s
sys	0m10.435s
+ status=0
+ set +x

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


=================================================
+ echo 'astros_SingleLoadCase_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_SingleLoadCase_PyTest.py test;
+ python -u astros_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 12
	Number of elements = 6
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 6
Aero_Reference value is NULL - No aero reference parameters set

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

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

real	0m0.941s
user	0m0.708s
sys	0m0.291s
+ 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	0m1.041s
user	0m0.709s
sys	0m0.290s
+ 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	0m1.184s
user	0m0.811s
sys	0m0.298s
+ 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	0m0.978s
user	0m0.731s
sys	0m0.299s
+ 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	0m0.907s
user	0m0.702s
sys	0m0.290s
+ status=0
+ set +x

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


=================================================
+ echo 'astros_Trim_15degree.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
astros_Trim_15degree.py test;
+ python -u astros_Trim_15degree.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

Getting FEA properties.......
	Number of properties - 3
	Property name - Body
	Property name - Edge
	Property name - Root
	Done getting FEA properties
Updating mesh element types based on properties input

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

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

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - Root
	No "groupName" specified for Connection tuple Root!
	Looking for automatic connections from the use of capsConnectLink for Root
	8 automatic connections were made for capsConnect Root (node id 97)
	Done getting FEA connections

Getting FEA loads.......
	Number of loads - 2
	Load name - GravityLoad
	No "groupName" specified for Load tuple GravityLoad, going to use load name
	Load name - PointLoad
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

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

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

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

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

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

real	0m1.146s
user	0m0.911s
sys	0m0.368s
+ 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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
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=      1335      2536         0
AFLR4    : Nodes, Trias,Quads=      1317      2500         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1337      2540         0
AFLR4    : Nodes, Trias,Quads=      1320      2506         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3787      7420         0
AFLR4    : Nodes, Trias,Quads=      2943      5732         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1341      2548         0
AFLR4    : Nodes, Trias,Quads=      1321      2508         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1337      2540         0
AFLR4    : Nodes, Trias,Quads=      1320      2506         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1342      2550         0
AFLR4    : Nodes, Trias,Quads=      1318      2502         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=      9478     18952       946

OVERALL  : CPU Time          =     0.223   seconds
Body 1 (of 1)
Number of nodes    = 9478
Number of elements = 18952
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 18952
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9478
Total number of elements = 18952
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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
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          = 61021
	Number of elements       = 351564
	Number of triangles      = 18952
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 332612
	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.
61021 grid points.
332612 volume elements.
3 surface markers.
12522 boundary elements in index 0 (Marker = BC_1).
5732 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
332612 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: 0.863308. Standard deviation K: 5.00657.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        52.4071|        86.6424|
|     CV Face Area Aspect Ratio|        1.04128|        21.5651|
|           CV Sub-Volume Ratio|              1|        10.4254|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     61021|    1/1.00|        10|
|         1|     10400|    1/5.87|   8.31654|
|         2|      1824|     1/5.7|   6.98282|
+-------------------------------------------+
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|  1.4344e+00|   -1.358658|    0.921673|    0.583457|    4.110448|   -0.914331|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.4357e+00|   -1.761379|    0.764232|    0.408273|    3.694369|   -0.434651|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.4282e+00|   -1.765424|    0.580434|    0.226849|    3.691843|    1.933305|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.76542|         < -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 = 3.100050e+09, tgt = 3.100049e+09, diff = 1.862177e+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 = 3.018381e+09, tgt = 3.018381e+09, diff = 1.955084e+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 = 4.368630e+07, tgt = 4.368630e+07, diff = 5.472995e-03
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 16 (total = 178)

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

Writing subElement types (if any) - appending mesh file

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

real	0m15.164s
user	0m14.485s
sys	0m1.804s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aeroelasticSimple_Pressure_SU2_and_Astros.py passed (as expected)
=================================================


=================================================
+ echo 'aeroelasticSimple_Displacement_SU2_and_Astros.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aeroelasticSimple_Displacement_SU2_and_Astros.py test;
+ python -u aeroelasticSimple_Displacement_SU2_and_Astros.py -outLevel=0 -noPlotData
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Running PreAnalysis ...... astros
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = Skin, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 3
	Name = Skin_Top, index = 1
	Name = Skin_Bottom, index = 2
	Name = Skin_Tip, index = 3
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Skin, index = 1
	Name = Rib_Root, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 180
	Number of elements = 194
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 32
	Elemental Quad4 = 162
Aero_Reference value is NULL - No aero reference parameters set

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

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

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

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

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

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

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards


Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL

Running PostAnalysis ...... astros

Running PreAnalysis ...... su2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Farfield, index = 1
	Name = SymmPlane, index = 2
	Name = Skin, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.14.7
AFLR2    : Version Date   07/16/23 @ 01:42PM
AFLR2    : Compile OS     Darwin 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
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=      1335      2536         0
AFLR4    : Nodes, Trias,Quads=      1317      2500         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1337      2540         0
AFLR4    : Nodes, Trias,Quads=      1320      2506         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3787      7420         0
AFLR4    : Nodes, Trias,Quads=      2943      5732         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1341      2548         0
AFLR4    : Nodes, Trias,Quads=      1321      2508         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1337      2540         0
AFLR4    : Nodes, Trias,Quads=      1320      2506         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1342      2550         0
AFLR4    : Nodes, Trias,Quads=      1318      2502         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=      9478     18952       946

OVERALL  : CPU Time          =     0.226   seconds
Body 1 (of 1)
Number of nodes    = 9478
Number of elements = 18952
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 18952
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9478
Total number of elements = 18952
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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
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          = 61021
	Number of elements       = 351564
	Number of triangles      = 18952
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 332612
	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.
61021 grid points.
332612 volume elements.
3 surface markers.
12522 boundary elements in index 0 (Marker = BC_1).
5732 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
332612 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 20.233371 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.
61021 grid points.
332612 volume elements.
3 surface markers.
12522 boundary elements in index 0 (Marker = BC_1).
5732 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
332612 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 1 TETRAHEDRON volume elements.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 63997.8.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 83.9101. Mean K: 0.903406. Standard deviation K: 4.47641.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        46.1587|        86.6056|
|     CV Face Area Aspect Ratio|        1.04375|        23.1726|
|           CV Sub-Volume Ratio|              1|        124.296|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     61021|    1/1.00|        10|
|         1|     10400|    1/5.87|   8.31654|
|         2|      1824|     1/5.7|   6.98282|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.89892 m.
Wetted area = 11.6151 m^2.
Area projection in the x-plane = 2.90002 m^2, y-plane = 1.28883 m^2, z-plane = 4.27937 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|  1.4634e+00|   -0.688947|    1.740396|    1.255245|    4.780159|    0.054072|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.4480e+00|   -1.147407|    1.463053|    1.107626|    4.324911|    0.052353|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.4340e+00|   -1.161658|    1.244069|    0.911458|    4.304744|    0.132783|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.16166|         < -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	0m41.940s
user	0m37.907s
sys	0m3.843s
+ 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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
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=       386       702         0
AFLR4    : Nodes, Trias,Quads=       379       688         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       383       696         0
AFLR4    : Nodes, Trias,Quads=       381       692         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      1073      2066         0
AFLR4    : Nodes, Trias,Quads=      1011      1942         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       383       696         0
AFLR4    : Nodes, Trias,Quads=       379       688         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       386       702         0
AFLR4    : Nodes, Trias,Quads=       382       694         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       382       694         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=      2821      5638       500

OVERALL  : CPU Time          =     0.106   seconds
Body 1 (of 1)
Number of nodes    = 2821
Number of elements = 5638
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 5638
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2821
Total number of elements = 5638
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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
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          = 11564
	Number of elements       = 65500
	Number of triangles      = 5638
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 59862
	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.
11564 grid points.
59862 volume elements.
3 surface markers.
3450 boundary elements in index 0 (Marker = BC_1).
1942 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
59862 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: 0.84105. Standard deviation K: 3.91738.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        51.6918|        86.3913|
|     CV Face Area Aspect Ratio|        1.04466|        19.2647|
|           CV Sub-Volume Ratio|              1|        8.65233|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11564|    1/1.00|        10|
|         1|      2057|    1/5.62|   8.43594|
|         2|       416|    1/4.94|   7.42753|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 8.34786 m^2.
Area projection in the x-plane = 0.588155 m^2, y-plane = 0.276999 m^2, z-plane = 3.94869 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|  2.6528e-01|   -0.829249|    1.482443|    1.171374|    4.639857|   -1.038196|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.6144e-01|   -1.159834|    1.372574|    1.018520|    4.293619|   -0.652554|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.5918e-01|   -1.204489|    1.232482|    0.850876|    4.247694|    0.347942|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.20449|         < -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 = 3.095428e+09, tgt = 3.095428e+09, diff = 1.351159e+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 = 3.012963e+09, tgt = 3.012962e+09, diff = 2.009594e+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 = 4.096833e+07, tgt = 4.096833e+07, diff = 3.029571e-02
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 16 (total = 178)

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.0) "


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.
11564 grid points.
59862 volume elements.
3 surface markers.
3450 boundary elements in index 0 (Marker = BC_1).
1942 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
59862 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 0.930599 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.
11564 grid points.
59862 volume elements.
3 surface markers.
3450 boundary elements in index 0 (Marker = BC_1).
1942 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
59862 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 1108 TETRAHEDRON volume elements.
There has been a re-orientation of 58 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 64433.6.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 26.0252. Mean K: 0.571286. Standard deviation K: 1.86038.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.486942|        86.4229|
|     CV Face Area Aspect Ratio|        1.17993|        127.585|
|           CV Sub-Volume Ratio|              1|        12343.3|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11564|    1/1.00|        10|
|         1|      2055|    1/5.63|    8.4332|
|         2|       416|    1/4.94|   7.42753|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 5.13991 m.
Wetted area = 175.761 m^2.
Area projection in the x-plane = 69.4357 m^2, y-plane = 38.559 m^2, z-plane = 6.53652 m^2.
Max. coordinate in the x-direction = 2.83445 m, y-direction = 5.13991 m, z-direction = 6.98757 m.
Min. coordinate in the x-direction = -0.842877 m, y-direction = -0.0111227 m, z-direction = -20.3036 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.6528e-01|    1.731397|    4.680995|    4.878777|    7.200503|   -0.000340|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.6919e-01|    2.117513|    4.727592|    4.881788|    7.577475|   -0.004852|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.7063e-01|    2.198584|    4.810440|    4.823227|    7.635895|   -2.718552|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       2.19858|         < -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 13 non-physical points in the solution.
Warning: 1 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 = 1.623035e+09, tgt = 1.623035e+09, diff = 2.153917e+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 = 1.688797e+09, tgt = 1.688797e+09, diff = 3.787474e+00
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 = 2.495697e+07, tgt = 2.495697e+07, diff = 2.015870e-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 IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.0) "


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.
11564 grid points.
59862 volume elements.
3 surface markers.
3450 boundary elements in index 0 (Marker = BC_1).
1942 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
59862 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 1108 TETRAHEDRON volume elements.
There has been a re-orientation of 58 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 64433.6.
  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 4.777030 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.
11564 grid points.
59862 volume elements.
3 surface markers.
3450 boundary elements in index 0 (Marker = BC_1).
1942 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
59862 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 38056 TETRAHEDRON volume elements.
There has been a re-orientation of 2309 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 3.3896e+07.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 26.9611. Mean K: 0.635103. Standard deviation K: 2.04023.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.981544|        79.8091|
|     CV Face Area Aspect Ratio|        1.58183|        10080.8|
|           CV Sub-Volume Ratio|              1|         242732|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11564|    1/1.00|        10|
|         1|      2055|    1/5.63|    8.4332|
|         2|       414|    1/4.96|   7.41561|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 73.4883 m.
Wetted area = 25578.6 m^2.
Area projection in the x-plane = 15007.6 m^2, y-plane = 3572.09 m^2, z-plane = 275.381 m^2.
Max. coordinate in the x-direction = 8.4614 m, y-direction = 73.4883 m, z-direction = 0.155398 m.
Min. coordinate in the x-direction = -11.6712 m, y-direction = -0.512081 m, z-direction = -930.896 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.4820e-01|    4.829393|    7.791280|    7.855095|   10.298499|   -0.060837|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.6000e-01|    5.226738|    7.835400|    7.776357|   10.619907|   -0.061413|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.6384e-01|    5.208244|    7.843447|    7.806019|   10.706394|   -0.059365|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       5.20824|         < -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 205 non-physical points in the solution.
Warning: 44 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 = 2.595889e+09, tgt = 2.595889e+09, diff = 3.758392e+01
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 = 2.655760e+09, tgt = 2.655760e+09, diff = 1.665342e+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 = 7.970910e+06, tgt = 7.970910e+06, diff = 1.747329e-02
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 81 (total = 81)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 81 (total = 162)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 16 (total = 178)

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticSimple_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.0) "


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.
11564 grid points.
59862 volume elements.
3 surface markers.
3450 boundary elements in index 0 (Marker = BC_1).
1942 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
59862 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 38056 TETRAHEDRON volume elements.
There has been a re-orientation of 2309 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 3.3896e+07.
  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 30.717005 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.
11564 grid points.
59862 volume elements.
3 surface markers.
3450 boundary elements in index 0 (Marker = BC_1).
1942 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
59862 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 35699 TETRAHEDRON volume elements.
There has been a re-orientation of 2087 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 5.43722e+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: 64.288. Mean K: 0.464342. Standard deviation K: 2.13452.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        2.00368|        81.0874|
|     CV Face Area Aspect Ratio|        1.46525|         528462|
|           CV Sub-Volume Ratio|              1|    3.66809e+07|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11564|    1/1.00|        10|
|         1|      2057|    1/5.62|   8.43594|
|         2|       415|    1/4.96|   7.42157|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 24.3915 m.
Wetted area = 2151.66 m^2.
Area projection in the x-plane = 830.863 m^2, y-plane = 916.212 m^2, z-plane = 78.5019 m^2.
Max. coordinate in the x-direction = 2.37666 m, y-direction = 24.3915 m, z-direction = 0.603659 m.
Min. coordinate in the x-direction = -19.2916 m, y-direction = -0.226076 m, z-direction = -208.488 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.5105e-01|    7.324703|   10.291558|   10.325418|   12.793809|    0.075595|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.5789e-01|    7.892694|   10.387335|   10.341545|   13.310450|    0.074677|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.5895e-01|    7.986091|   10.441704|   10.343121|   13.400119|   -0.004865|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       7.98609|         < -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 480 non-physical points in the solution.
Warning: 53 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 =  26.853765
Cd =  -5519.63933

real	0m51.926s
user	0m48.682s
sys	0m3.614s
+ 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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
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=       386       702         0
AFLR4    : Nodes, Trias,Quads=       379       688         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=       383       696         0
AFLR4    : Nodes, Trias,Quads=       381       692         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      1073      2066         0
AFLR4    : Nodes, Trias,Quads=      1011      1942         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=       383       696         0
AFLR4    : Nodes, Trias,Quads=       379       688         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=       386       702         0
AFLR4    : Nodes, Trias,Quads=       382       694         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=       382       694         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=      2821      5638       500

OVERALL  : CPU Time          =     0.107   seconds
Body 1 (of 1)
Number of nodes    = 2821
Number of elements = 5638
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 5638
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2821
Total number of elements = 5638
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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
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          = 11564
	Number of elements       = 65500
	Number of triangles      = 5638
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 59862
	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.
11564 grid points.
59862 volume elements.
3 surface markers.
3450 boundary elements in index 0 (Marker = BC_1).
1942 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
59862 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: 0.84105. Standard deviation K: 3.91738.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        51.6918|        86.3913|
|     CV Face Area Aspect Ratio|        1.04466|        19.2647|
|           CV Sub-Volume Ratio|              1|        8.65233|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11564|    1/1.00|        10|
|         1|      2057|    1/5.62|   8.43594|
|         2|       416|    1/4.94|   7.42753|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 3.87298 m.
Wetted area = 8.34786 m^2.
Area projection in the x-plane = 0.588155 m^2, y-plane = 0.276999 m^2, z-plane = 3.94869 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|  2.4829e-01|   -0.829249|    1.482443|    1.171374|    4.639857|   -1.038196|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.4568e-01|   -1.159834|    1.372574|    1.018520|    4.293619|   -0.652554|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.4414e-01|   -1.204489|    1.232482|    0.850876|    4.247694|    0.347942|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.20449|         < -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 = 3.095428e+09, tgt = 3.095428e+09, diff = 9.790715e+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 = 3.012963e+09, tgt = 3.012963e+09, diff = 7.230747e+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 = 4.096833e+07, tgt = 4.096833e+07, diff = 2.694621e+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 IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.0) "


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.
11564 grid points.
59862 volume elements.
3 surface markers.
3450 boundary elements in index 0 (Marker = BC_1).
1942 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
59862 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 63999.5.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 1.349074 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.
11564 grid points.
59862 volume elements.
3 surface markers.
3450 boundary elements in index 0 (Marker = BC_1).
1942 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
59862 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 25249 TETRAHEDRON volume elements.
There has been a re-orientation of 1510 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 591486.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 144.635. Mean K: 1.75328. Standard deviation K: 9.42104.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.691214|        82.9974|
|     CV Face Area Aspect Ratio|        1.44733|        558.924|
|           CV Sub-Volume Ratio|              1|        61528.2|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11564|    1/1.00|        10|
|         1|      2051|    1/5.64|   8.42773|
|         2|       417|    1/4.92|   7.43347|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 26.5951 m.
Wetted area = 3528.9 m^2.
Area projection in the x-plane = 621.881 m^2, y-plane = 1110.67 m^2, z-plane = 118.437 m^2.
Max. coordinate in the x-direction = 5.24083 m, y-direction = 26.5951 m, z-direction = 26.1572 m.
Min. coordinate in the x-direction = -12.7933 m, y-direction = -0.880301 m, z-direction = -281.505 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.4245e-01|    3.692580|    6.657805|    6.818225|    9.161686|   -0.358760|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.5359e-01|    4.029617|    6.547313|    6.675597|    9.360628|   -0.348575|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.5659e-01|    6.410450|    9.436545|    7.964226|   12.199090|   -0.335949|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       6.41045|         < -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 281 non-physical points in the solution.
Warning: 7 reconstructed states for upwinding are non-physical.

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

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


Running PostAnalysis ...... su2

Running PreAnalysis ...... su2
Reading SU2 AeroLoad File - surface_flow_aeroelastic_Iterative.csv
	Number of variables = 16
	Number of data points = 130
 CAPS Info: Bound 'Skin_Top' Normalized Integrated 'Pressure'
            Rank 0: src = 1.158256e+09, tgt = 1.158256e+09, diff = 4.653122e+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 = 1.233253e+09, tgt = 1.233253e+09, diff = 7.397344e+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 = 9.591058e+06, tgt = 9.591095e+06, diff = 3.674661e+01
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 330 (total = 330)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 330 (total = 660)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 30 (total = 690)

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.0) "


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.
11564 grid points.
59862 volume elements.
3 surface markers.
3450 boundary elements in index 0 (Marker = BC_1).
1942 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
59862 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 25249 TETRAHEDRON volume elements.
There has been a re-orientation of 1510 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 591486.
  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 31.135974 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.
11564 grid points.
59862 volume elements.
3 surface markers.
3450 boundary elements in index 0 (Marker = BC_1).
1942 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
59862 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 22755 TETRAHEDRON volume elements.
There has been a re-orientation of 3290 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 8.67467e+10.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 13.4523. Mean K: 0.261479. Standard deviation K: 0.882366.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|         1.6378|        79.8622|
|     CV Face Area Aspect Ratio|        1.54087|         156819|
|           CV Sub-Volume Ratio|              1|         550084|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11564|    1/1.00|        10|
|         1|      2049|    1/5.64|   8.42499|
|         2|       409|    1/5.01|   7.38563|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 315.684 m.
Wetted area = 688856 m^2.
Area projection in the x-plane = 470990 m^2, y-plane = 56246.1 m^2, z-plane = 610.97 m^2.
Max. coordinate in the x-direction = 88.9899 m, y-direction = 315.684 m, z-direction = 0.155398 m.
Min. coordinate in the x-direction = -3.43515 m, y-direction = -6.29596 m, z-direction = -4674.72 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.6631e-01|    6.914850|    9.881519|    9.824207|   12.383956|   -0.009743|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.7672e-01|    7.243348|    9.791441|    9.802642|   12.651151|   -0.007218|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.7822e-01|    7.374492|    9.862317|    9.919224|   12.747353|   -0.017063|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       7.37449|         < -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 554 non-physical points in the solution.
Warning: 29 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 = 1.198776e+09, tgt = 1.198778e+09, diff = 1.313059e+03
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 = 1.339798e+09, tgt = 1.339798e+09, diff = 7.109079e+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 = 4.218428e+07, tgt = 4.218432e+07, diff = 3.253196e+01
Extracting external pressure loads from data transfer....
	TransferName = Skin_Top
	Number of Elements = 330 (total = 330)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Bottom
	Number of Elements = 330 (total = 660)
Extracting external pressure loads from data transfer....
	TransferName = Skin_Tip
	Number of Elements = 30 (total = 690)

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

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelastic_Iterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.0) "


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.
11564 grid points.
59862 volume elements.
3 surface markers.
3450 boundary elements in index 0 (Marker = BC_1).
1942 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
59862 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
There has been a re-orientation of 22755 TETRAHEDRON volume elements.
There has been a re-orientation of 3290 TRIANGLE surface elements.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 8.67467e+10.
  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 30.704036 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.
11564 grid points.
59862 volume elements.
3 surface markers.
3450 boundary elements in index 0 (Marker = BC_1).
1942 boundary elements in index 1 (Marker = BC_2).
246 boundary elements in index 2 (Marker = BC_3).
59862 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 33680 TETRAHEDRON volume elements.
There has been a re-orientation of 1981 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 3.22423e+13.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 12.2563. Mean K: 0.188165. Standard deviation K: 0.789268.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.328021|        78.3942|
|     CV Face Area Aspect Ratio|        1.62958|    3.18055e+08|
|           CV Sub-Volume Ratio|              1|    1.61027e+07|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11564|    1/1.00|        10|
|         1|      2064|     1/5.6|    8.4455|
|         2|       423|    1/4.88|   7.46896|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 803.979 m.
Wetted area = 3.59967e+06 m^2.
Area projection in the x-plane = 339528 m^2, y-plane = 1.19488e+06 m^2, z-plane = 62073.3 m^2.
Max. coordinate in the x-direction = 95.9622 m, y-direction = 803.979 m, z-direction = 0.155398 m.
Min. coordinate in the x-direction = -32.7531 m, y-direction = -23.0913 m, z-direction = -11101 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_3 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.7321e-01|    8.520490|   11.487338|   11.558091|   13.989595|   -0.020579|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.7384e-01|    9.183430|   11.675279|   11.673413|   14.558168|   -0.020673|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.7196e-01|    9.281168|   11.764413|   11.756436|   14.636558|   -0.020791|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       9.28117|         < -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 541 non-physical points in the solution.
Warning: 101 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	1m37.546s
user	1m45.824s
sys	0m11.014s
+ 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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
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=      1335      2536         0
AFLR4    : Nodes, Trias,Quads=      1317      2500         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1337      2540         0
AFLR4    : Nodes, Trias,Quads=      1320      2506         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      3787      7420         0
AFLR4    : Nodes, Trias,Quads=      2943      5732         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1341      2548         0
AFLR4    : Nodes, Trias,Quads=      1321      2508         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=      1337      2540         0
AFLR4    : Nodes, Trias,Quads=      1320      2506         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1342      2550         0
AFLR4    : Nodes, Trias,Quads=      1318      2502         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=      9478     18952       946

OVERALL  : CPU Time          =     0.253   seconds
Body 1 (of 1)
Number of nodes    = 9478
Number of elements = 18952
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 18952
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9478
Total number of elements = 18952
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 22.5.0 x86_64
AFLR2    : Compile Date   07/25/23 @ 11:59AM
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 22.5.0 x86_64
AFLR4    : Compile Date   08/14/23 @ 01:13PM
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          = 61021
	Number of elements       = 351564
	Number of triangles      = 18952
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 332612
	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.
61021 grid points.
332612 volume elements.
3 surface markers.
12522 boundary elements in index 0 (Marker = BC_1).
5732 boundary elements in index 1 (Marker = BC_2).
698 boundary elements in index 2 (Marker = BC_3).
332612 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: 0.863308. Standard deviation K: 5.00657.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        52.4071|        86.6424|
|     CV Face Area Aspect Ratio|        1.04128|        21.5651|
|           CV Sub-Volume Ratio|              1|        10.4254|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     61021|    1/1.00|        10|
|         1|     10400|    1/5.87|   8.31654|
|         2|      1824|     1/5.7|   6.98282|
+-------------------------------------------+
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|  1.4277e+00|   -1.358658|    0.921673|    0.583457|    4.110448|   -0.914331|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.4218e+00|   -1.761379|    0.764232|    0.408273|    3.694369|   -0.434651|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.4078e+00|   -1.765424|    0.580434|    0.226849|    3.691843|    1.933305|

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

Maximum number of iterations reached (ITER = 3) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.76542|         < -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 = 1.497162e+03, tgt = 1.497162e+03, diff = 1.197986e-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 = 1.453298e+03, tgt = 1.453298e+03, diff = 2.126951e-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 = 2.097780e+01, tgt = 2.097780e+01, diff = 9.379164e-13
Extracting external thermal loads from data transfer....
	TransferName = Skin_Top
	Number of Nodes = 9 (total = 9)
Extracting external thermal loads from data transfer....
	TransferName = Skin_Bottom
	Number of Nodes = 9 (total = 18)
Extracting external thermal loads from data transfer....
	TransferName = Skin_Tip
	Number of Nodes = 4 (total = 16)

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards

Running PostAnalysis ...... tacs

real	0m14.376s
user	0m13.787s
sys	0m1.712s
+ 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	0m9.699s
user	0m1.361s
sys	0m0.312s
+ status=0
+ set +x

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


=================================================
+ echo 'qp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
qp.py test;
+ python -u qp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

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

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

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

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

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


real	0m1.518s
user	0m1.390s
sys	0m0.189s
+ status=0
+ set +x

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


=================================================
+ echo 'sp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
sp.py test;
+ python -u sp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   0.45721 dimensionless

Variables
---------
   x  :  2.56155   [-]   The X variable
   y  :  6.56155   [-]   The Y variable
   z  :  1.17116   [-]   The Z variable

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

Sensitivities
-------------
   Sensitivities not computed

Solve Report
------------
   Solve Method           :  Signomial Program--Standard 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  3 
   Termination Status     :  Converged, relative error (3.15e-04) is less than specified tolerance (1.00e-03) 


real	0m1.354s
user	0m1.360s
sys	0m0.189s
+ status=0
+ set +x

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


=================================================
+ echo 'boydBox.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
boydBox.py test;
+ python -u boydBox.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   0.00520 1 / meter ** 3

Variables
---------
   d  :  11.26658   meter   The Z variable
   h  :   2.92246   meter   The Y variable
   w  :   5.84486   meter   The X variable

Constants
---------
   Aflr   :  1000         meter ** 2   Area of floor          
   Awall  :   100         meter ** 2   Area of wall           
   alpha  :     0.50000      [-]       Aspect Ratio Constraint
   beta   :     2            [-]       Aspect Ratio Constraint
   delta  :     2            [-]       Aspect Ratio Constraint
   gamma  :     0.50000      [-]       Aspect Ratio Constraint

Sensitivities
-------------
   Sensitivities not computed

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


real	0m1.161s
user	0m1.175s
sys	0m0.183s
+ status=0
+ set +x

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


=================================================
+ echo 'hoburg_gp.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hoburg_gp.py test;
+ python -u hoburg_gp.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   5905.58568 newton

Variables
---------
   AR          :       20.36983        [-]         aspect ratio                                                            
   C_D_0       :        0.01271        [-]         Drag Coefficient, segment 0                                             
   C_D_1       :        0.01273        [-]         Drag Coefficient, segment 1                                             
   C_D_2       :        0.00778        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0   :        0.00180        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1   :        0.00180        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2   :        0.00180        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0      :        0.00542        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1      :        0.00542        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2      :        0.00023        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0      :        0.00549        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1      :        0.00551        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2      :        0.00575        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0       :        0.57420        [-]         Lift Coefficient, segment 0                                             
   C_L_1       :        0.57421        [-]         Lift Coefficient, segment 1                                             
   C_L_2       :        0.11881        [-]         Lift Coefficient, segment 2                                             
   I_cap_bar   :        0.00002        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar     :    36139.20785       newton       Root Bending unit per unit chord                                        
   P_max       :  1185884.98442        watt        Maximum Engine Power                                                    
   R           :     4999.98983     kilometer      Single Segment range                                                    
   Re_0        :  4232645.50367        [-]         Reynolds Number, segment 0                                              
   Re_1        :  4051247.93913        [-]         Reynolds Number, segment 1                                              
   Re_2        :  9305153.26607        [-]         Reynolds Number, segment 2                                              
   S           :       27.73109     meter ** 2     total wing area                                                         
   T_0         :      746.21338       newton       Thrust, segment 0                                                       
   T_1         :      684.51827       newton       Thrust, segment 1                                                       
   T_2         :     2208.51611       newton       Thrust, segment 2                                                       
   V_0         :       68.23357   meter / second   Velocity, segment 0                                                     
   V_1         :       65.30930   meter / second   Velocity, segment 1                                                     
   V_2         :      150.00638   meter / second   Velocity, segment 2                                                     
   V_stall     :       37.99896   meter / second   stall speed                                                             
   W_0         :    33698.97702       newton       Weight, segment 0                                                       
   W_1         :    30873.13301       newton       Weight, segment 1                                                       
   W_2         :    33698.96566       newton       Weight, segment 2                                                       
   W_MTO       :    36788.13387       newton       Maximum Takeoff Weight                                                  
   W_cap       :     4091.65066       newton       Weight of Wing Spar Cap                                                 
   W_eng       :     2806.10727       newton       Engine Weight                                                           
   W_fuel_out  :     3079.86524       newton       Weight of fuel, outbound                                                
   W_fuel_ret  :     2825.71897       newton       Weight of fuel, return                                                  
   W_pay       :     4905.15902       newton       Payload Weight                                                          
   W_tilde     :    22409.98513       newton       Dry Weight, no wing                                                     
   W_web       :      139.91823       newton       Weight of Wing Spar Shear Web                                           
   W_wing      :     8462.91404       newton       wing weight                                                             
   W_zfw       :    30872.92436       newton       Zero Fuel Weight                                                        
   eta_0_0     :        0.26999        [-]         Overall Efficiency, segment 0                                           
   eta_0_1     :        0.26996        [-]         Overall Efficiency, segment 1                                           
   eta_0_2     :        0.27945        [-]         Overall Efficiency, segment 2                                           
   eta_i_0     :        0.90752        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1     :        0.90742        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2     :        0.93932        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0  :        0.77139        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1  :        0.77131        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2  :        0.79842        [-]         Propeller Efficiency, segment 2                                         
   nu          :        0.78603        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p           :        1.90003        [-]         Dummy Variable (1+2*lam_w)                                              
   q           :        1.45002        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar   :        0.00456        [-]         Spar cap thickness per unit chord                                       
   t_web_bar   :        0.00069        [-]         Spar web thickness per unit chord                                       
   tau         :        0.15000        [-]         airfoil thickness to chord ratio                                        
   z_bre_0     :        0.08745        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1     :        0.08758        [-]         Breguet Range Factor, segment 1                                         

Constants
---------
   A_prop           :         0.78500           meter ** 2          Disk area of propeller                             
   CDA0             :         0.05000           meter ** 2          fuselage drag area                                 
   C_Lmax           :         1.50000              [-]              max CL with flaps down                             
   N_lift           :         6                    [-]              Ultimate Load Factor                               
   W_fixed          :     14700                   newton            fixed weight                                       
   e                :         0.95000              [-]              Oswald efficiency factor                           
   eta_eng          :         0.35000              [-]              Engine Efficiency                                  
   eta_v            :         0.85000              [-]              Propeller Viscous Efficiency                       
   f_wadd           :         2                    [-]              Added Weight Fraction                              
   g                :         9.81000      meter / second ** 2      Gravitational constant                             
   h_fuel           :  46000000              joule / kilogram       Fuel Specific energy density                       
   k_ew             :         0.03720     newton / watt ** 0.803    Constant for engine weight                         
   mu               :         0.00002   kilogram / meter / second   viscosity of air                                   
   r_h              :         0.75000              [-]              Ratio of height at rear spar to maximum wing height
   rho              :         0.90912     kilogram / meter ** 3     density of air                                     
   rho_SL           :         1.22500     kilogram / meter ** 3     density of air, sea level                          
   rho_cap          :      2700           kilogram / meter ** 3     Density of wing cap material (aluminum)            
   rho_web          :      2700           kilogram / meter ** 3     Density of wing web material (aluminum)            
   sigma_max        :       310                 megapascal          Allowable tensile stress of aluminum               
   sigma_max_shear  :       167                 megapascal          Allowable shear stress of aluminum                 
   w_bar            :         0.50000              [-]              Ratio of spar box width to chord length            

Sensitivities
-------------
   Sensitivities not computed

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


real	0m9.667s
user	0m9.535s
sys	0m0.249s
+ status=0
+ set +x

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


=================================================
+ echo 'hoburg_blackbox.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hoburg_blackbox.py test;
+ python -u hoburg_blackbox.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   5905.2294 newton

Variables
---------
   AR          :       20.3737        [-]         aspect ratio                                                            
   C_D_0       :        0.0127        [-]         Drag Coefficient, segment 0                                             
   C_D_1       :        0.0127        [-]         Drag Coefficient, segment 1                                             
   C_D_2       :        0.0078        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0   :        0.0018        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1   :        0.0018        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2   :        0.0018        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0      :        0.0054        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1      :        0.0054        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2      :        0.0002        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0      :        0.0055        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1      :        0.0055        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2      :        0.0057        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0       :        0.5743        [-]         Lift Coefficient, segment 0                                             
   C_L_1       :        0.5743        [-]         Lift Coefficient, segment 1                                             
   C_L_2       :        0.1189        [-]         Lift Coefficient, segment 2                                             
   I_cap_bar   :        0.0000        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar     :    36141.5015       newton       Root Bending unit per unit chord                                        
   P_max       :  1184357.7688        watt        Maximum Engine Power                                                    
   R           :     5000.0000     kilometer      Single Segment range                                                    
   Re_0        :  4231748.4656        [-]         Reynolds Number, segment 0                                              
   Re_1        :  4050340.4364        [-]         Reynolds Number, segment 1                                              
   Re_2        :  9301869.2065        [-]         Reynolds Number, segment 2                                              
   S           :       27.7189     meter ** 2     total wing area                                                         
   T_0         :      746.1648       newton       Thrust, segment 0                                                       
   T_1         :      684.5072       newton       Thrust, segment 1                                                       
   T_2         :     2206.5587       newton       Thrust, segment 2                                                       
   V_0         :       68.2403   meter / second   Velocity, segment 0                                                     
   V_1         :       65.3149   meter / second   Velocity, segment 1                                                     
   V_2         :      150.0000   meter / second   Velocity, segment 2                                                     
   V_stall     :       38.0000   meter / second   stall speed                                                             
   W_0         :    33694.3546       newton       Weight, segment 0                                                       
   W_1         :    30868.7209       newton       Weight, segment 1                                                       
   W_2         :    33694.3546       newton       Weight, segment 2                                                       
   W_MTO       :    36773.9503       newton       Maximum Takeoff Weight                                                  
   W_cap       :     4091.0280       newton       Weight of Wing Spar Cap                                                 
   W_eng       :     2802.5264       newton       Engine Weight                                                           
   W_fuel_out  :     3079.5957       newton       Weight of fuel, outbound                                                
   W_fuel_ret  :     2825.6337       newton       Weight of fuel, return                                                  
   W_pay       :     4905.0000       newton       Payload Weight                                                          
   W_tilde     :    22407.5264       newton       Dry Weight, no wing                                                     
   W_web       :      139.5692       newton       Weight of Wing Spar Shear Web                                           
   W_wing      :     8461.1945       newton       wing weight                                                             
   W_zfw       :    30868.7209       newton       Zero Fuel Weight                                                        
   eta_0_0     :        0.2700        [-]         Overall Efficiency, segment 0                                           
   eta_0_1     :        0.2700        [-]         Overall Efficiency, segment 1                                           
   eta_0_2     :        0.2795        [-]         Overall Efficiency, segment 2                                           
   eta_i_0     :        0.9075        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1     :        0.9074        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2     :        0.9394        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0  :        0.7714        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1  :        0.7713        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2  :        0.7985        [-]         Propeller Efficiency, segment 2                                         
   nu          :        0.7860        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p           :        1.9000        [-]         Dummy Variable (1+2*lam_w)                                              
   q           :        1.4500        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar   :        0.0046        [-]         Spar cap thickness per unit chord                                       
   t_web_bar   :        0.0007        [-]         Spar web thickness per unit chord                                       
   tau         :        0.1500        [-]         airfoil thickness to chord ratio                                        
   z_bre_0     :        0.0875        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1     :        0.0876        [-]         Breguet Range Factor, segment 1                                         

Constants
---------
   A_prop           :         0.7850           meter ** 2          Disk area of propeller                             
   CDA0             :         0.0500           meter ** 2          fuselage drag area                                 
   C_Lmax           :         1.5000              [-]              max CL with flaps down                             
   N_lift           :         6                   [-]              Ultimate Load Factor                               
   W_fixed          :     14700                  newton            fixed weight                                       
   e                :         0.9500              [-]              Oswald efficiency factor                           
   eta_eng          :         0.3500              [-]              Engine Efficiency                                  
   eta_v            :         0.8500              [-]              Propeller Viscous Efficiency                       
   f_wadd           :         2                   [-]              Added Weight Fraction                              
   g                :         9.8100      meter / second ** 2      Gravitational constant                             
   h_fuel           :  46000000             joule / kilogram       Fuel Specific energy density                       
   k_ew             :         0.0372     newton / watt ** 0.803    Constant for engine weight                         
   mu               :         0.0000   kilogram / meter / second   viscosity of air                                   
   r_h              :         0.7500              [-]              Ratio of height at rear spar to maximum wing height
   rho              :         0.9091     kilogram / meter ** 3     density of air                                     
   rho_SL           :         1.2250     kilogram / meter ** 3     density of air, sea level                          
   rho_cap          :      2700          kilogram / meter ** 3     Density of wing cap material (aluminum)            
   rho_web          :      2700          kilogram / meter ** 3     Density of wing web material (aluminum)            
   sigma_max        :       310                megapascal          Ultimate tensile stress of aluminum                
   sigma_max_shear  :       167                megapascal          Ultimate shear stress of aluminum                  
   w_bar            :         0.5000              [-]              Ratio of spar box width to chord length            

Sensitivities
-------------
   Sensitivities not currently implemented for optimization type Logspace Sequential Quadratic Program 

Solve Report
------------
   Solve Method           :  Logspace Sequential Quadratic Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  7 
   Termination Status     :  Converged, gradient of Lagrangian (9.638917e-07) within tolerance (1.000000e-06)  

Messages
--------
   1. Wolfe Condition 1 failed at iteration 5 (Step 5).  Watchdog counter is 1
   2. Wolfe Condition 1 failed at iteration 6 (Step 6).  Watchdog counter is 2


real	0m38.211s
user	0m38.063s
sys	0m0.271s
+ status=0
+ set +x

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


=================================================
+ echo 'pyCAPS/sizeWing.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/sizeWing.py test;
+ python -u pyCAPS/sizeWing.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
nrock 2

Objective
---------
   0.075 dimensionless

Variables
---------
   AR     :  10.000        [-]         Wing aspect ratio
   CD     :   0.075        [-]         Drag Coefficient 
   CL     :   0.999        [-]         Lift Coefficient 
   S      :   2.642     meter ** 2     Wing area        
   V      :   2.722   meter / second   Airspeed         
   W      :  11.979       newton       Aircraft weight  
   Wwing  :   1.598       newton       Wing weight      

Constants
---------
   ARmax     :  10                [-]            Max AR                                         
   CD0       :   0.040            [-]            Profile drag                                   
   CLmax     :   1                [-]            Max CL                                         
   E0        :  10               joule           Maximum elastic potential energy in rubber band
   Wfixed    :   0.100           newton          Weight of fixed components                     
   Wrock     :   2               newton          Weight of each rock                            
   e         :   0.900            [-]            Oswawld efficiency factor                      
   g         :   9.810    meter / second ** 2    Gravitational constant                         
   nrock     :   2                [-]            Number of rocks to carry                       
   rho       :   1.225   kilogram / meter ** 3   Density of air                                 
   rho_wing  :   1       kilogram / meter ** 3   Weight density of wing                         
   tau       :   0.120            [-]            Airfoil thickness as t/c                       

Sensitivities
-------------
   Sensitivities not computed

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

Optimized L/D: 13.267784561972134
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!

real	0m1.741s
user	0m1.652s
sys	0m0.234s
+ status=0
+ set +x

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

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

=================================================
+ echo 'pyCAPS/optTaperAvl.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/optTaperAvl.py test;
+ python -u pyCAPS/optTaperAvl.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)

Objective
---------
   1.00805 dimensionless

Variables
---------
   e    :  0.99202   [-]   Oswald efficiency factor
   lam  :  0.39881   [-]   Wing taper ratio        

Sensitivities
-------------
   Sensitivities not available for optimizations of type Sequential Log Convex Program 

Solve Report
------------
   Solve Method           :  Sequential Log Convex Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  6 
   Termination Status     :  Converged, gradient of Lagrangian (5.888882e-08) within tolerance (1.000000e-06)  

Messages
--------
   1. Wolfe Condition 1 failed at iteration 5 (Step 5).  Watchdog counter is 1


real	0m6.443s
user	0m4.085s
sys	0m2.296s
+ 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 0.3266 seconds
AR : 9.0 dimensionless
CD : 0.1 dimensionless
CL : 1.0 dimensionless
S : 1.0 meter ** 2
V : 1.0 meter / second
W : 10.0 newton
Wwing : 0.1 newton
e : 1.0 dimensionless
lam : 0.3 dimensionless
AVL run case - lam, AR: 0.3 9.0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9905504143712885 dimensionless
dydx: [<Quantity(0.06083473495512859, 'dimensionless')>, <Quantity(-0.0014769756676574763, 'dimensionless')>]
Calling cvxopt.solvers.cp at 1.4570 seconds
Got sol from cvxopt at 1.4729 seconds
status optimal
x [ 1.05e-01]
[-3.26e-01]
[-1.49e-11]
[-4.10e-01]
[ 1.28e+00]
[-6.40e-01]
[ 7.00e-01]
[-1.08e-02]
[ 5.73e-03]
[-3.20e-16]
[ 3.50e-16]
[ 1.56e-16]
[ 5.20e-16]
[ 2.70e-16]
[ 4.16e-27]
[ 3.37e-16]
[ 2.07e-23]

y [-6.40e-01]
[ 7.00e-01]
[ 3.11e-01]

znl [ 6.74e-01]
[ 4.14e-08]

zl [ 1.04e+00]
[ 5.41e-01]
[ 8.31e-12]

snl [ 8.55e-11]
[ 2.03e-01]

sl [ 1.49e-11]
[ 4.30e-10]
[ 8.74e-01]

gap 8.743959706208345e-09
relative gap 7.194197617465325e-09
primal objective -1.2154183372695615
dual objective -1.215418341683548
primal slack 1.3843122277352784e-11
dual slack 8.310943825862027e-12
primal infeasibility 1.1390345696246042e-09
dual infeasibility 2.382358051743254e-11
AVL run case - lam, AR: 0.3017253411785187 9.999999995701312
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9892210301572447 dimensionless
dydx: [<Quantity(0.06359341837318677, 'dimensionless')>, <Quantity(-0.0014812479871501028, 'dimensionless')>]
logspace stuff at 2.5950 seconds
Starting iteration 1 at 2.6282 seconds
AR : 9.999999995701312 dimensionless
CD : 0.07217671497330198 dimensionless
CL : 0.9999999999851361 dimensionless
S : 0.6639217992634344 meter ** 2
V : 3.600068783658013 meter / second
W : 5.270412635736404 newton
Wwing : 0.20138431695627712 newton
e : 0.9892553874048063 dimensionless
lam : 0.3017253411785187 dimensionless
Calling cvxopt.solvers.cp at 2.6373 seconds
Got sol from cvxopt at 2.6506 seconds
status optimal
x [ 3.90e-10]
[-5.94e-05]
[-1.96e-07]
[ 1.14e-08]
[ 7.38e-08]
[-3.68e-08]
[ 1.70e-08]
[ 1.33e-04]
[ 8.64e-03]
[ 6.35e-21]
[-6.95e-21]
[ 2.23e-16]
[ 5.42e-17]
[ 2.20e-16]
[ 1.27e-26]
[ 5.00e-16]
[ 6.63e-26]

y [ 1.27e-05]
[-1.39e-05]
[ 4.46e-01]

znl [ 1.00e+00]
[ 1.33e-10]

zl [ 1.08e-01]
[ 4.39e-01]
[ 2.53e-11]

snl [ 2.06e-11]
[ 2.03e-01]

sl [ 1.96e-07]
[ 4.02e-11]
[ 8.74e-01]

gap 2.1363031594437688e-08
relative gap 8.126967446453998e-09
primal objective -2.62865967351191
dual objective -2.628659684337801
primal slack 2.057784648174032e-11
dual slack 2.5305040679144164e-11
primal infeasibility 3.0858033491332136e-09
dual infeasibility 3.1339130723066173e-09
AVL run case - lam, AR: 0.30434464835757047 9.99999999959832
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9893844569299911 dimensionless
dydx: [<Quantity(0.06135879009172007, 'dimensionless')>, <Quantity(-0.0014697917150108264, 'dimensionless')>]
logspace stuff at 3.8003 seconds
Starting iteration 2 at 3.8430 seconds
AR : 9.99999999959832 dimensionless
CD : 0.07217242517886913 dimensionless
CL : 0.9999998041107226 dimensionless
S : 0.6639218068635588 meter ** 2
V : 3.6000690493939635 meter / second
W : 5.270412441791245 newton
Wwing : 0.20138432037500312 newton
e : 0.9893868959018433 dimensionless
lam : 0.30434464835757047 dimensionless
Calling cvxopt.solvers.cp at 3.8521 seconds
Got sol from cvxopt at 3.8656 seconds
status optimal
x [ 7.75e-13]
[-3.52e-04]
[ 4.29e-09]
[-2.11e-10]
[-1.42e-09]
[ 1.25e-09]
[-3.17e-10]
[ 7.91e-04]
[ 4.20e-02]
[ 7.26e-21]
[-7.89e-21]
[ 2.23e-16]
[ 5.45e-17]
[ 2.20e-16]
[ 1.24e-26]
[ 5.00e-16]
[ 6.65e-26]

y [ 1.45e-05]
[-1.58e-05]
[ 4.45e-01]

znl [ 1.00e+00]
[ 1.33e-10]

zl [ 1.09e-01]
[ 4.39e-01]
[ 2.49e-11]

snl [ 2.02e-11]
[ 2.03e-01]

sl [ 1.92e-07]
[ 3.94e-11]
[ 8.74e-01]

gap 2.0979541929276537e-08
relative gap 7.980432611479698e-09
primal objective -2.628872763000075
dual objective -2.628872773631924
primal slack 2.022619551948966e-11
dual slack 2.4870270233858892e-11
primal infeasibility 3.030673275142993e-09
dual infeasibility 3.076932689522998e-09
AVL run case - lam, AR: 0.31740935131467607 9.999999999606068
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9901147289476424 dimensionless
dydx: [<Quantity(0.0507308561720321, 'dimensionless')>, <Quantity(-0.0014191909882388387, 'dimensionless')>]
logspace stuff at 5.0047 seconds
Starting iteration 3 at 5.0443 seconds
AR : 9.999999999606068 dimensionless
CD : 0.07214699157333947 dimensionless
CL : 0.9999998084033913 dimensionless
S : 0.6639218067235316 meter ** 2
V : 3.6000690442960215 meter / second
W : 5.270412448377283 newton
Wwing : 0.20138432031121437 newton
e : 0.9901696737886146 dimensionless
lam : 0.31740935131467607 dimensionless
Calling cvxopt.solvers.cp at 5.0530 seconds
Got sol from cvxopt at 5.0670 seconds
status optimal
x [ 2.14e-12]
[-1.28e-03]
[ 1.17e-08]
[-5.10e-10]
[-3.51e-09]
[ 4.16e-09]
[-7.67e-10]
[ 2.88e-03]
[ 1.81e-01]
[-4.10e-21]
[ 4.49e-21]
[ 2.23e-16]
[ 5.51e-17]
[ 2.20e-16]
[ 1.18e-26]
[ 5.00e-16]
[ 6.61e-26]

y [-8.19e-06]
[ 8.98e-06]
[ 4.45e-01]

znl [ 1.00e+00]
[ 1.32e-10]

zl [ 1.10e-01]
[ 4.40e-01]
[ 2.37e-11]

snl [ 1.92e-11]
[ 2.03e-01]

sl [ 1.80e-07]
[ 3.73e-11]
[ 8.74e-01]

gap 1.9913348951306756e-08
relative gap 7.572537674951306e-09
primal objective -2.629679746219923
dual objective -2.6296797563122976
primal slack 1.9233234442651708e-11
dual slack 2.3654666053878418e-11
primal infeasibility 2.8765759272243296e-09
dual infeasibility 2.9202708384568647e-09
AVL run case - lam, AR: 0.3802990571829513 9.999999999627487
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9919295458295698 dimensionless
dydx: [<Quantity(0.009583432731846697, 'dimensionless')>, <Quantity(-0.0013533445524949173, 'dimensionless')>]
logspace stuff at 6.1913 seconds
Starting iteration 4 at 6.2327 seconds
AR : 9.999999999627487 dimensionless
CD : 0.07205440311146945 dimensionless
CL : 0.9999998201037487 dimensionless
S : 0.6639218063847039 meter ** 2
V : 3.600069031643115 meter / second
W : 5.270412470306197 newton
Wwing : 0.20138432015683608 newton
e : 0.9930297814909534 dimensionless
lam : 0.3802990571829513 dimensionless
Calling cvxopt.solvers.cp at 6.2418 seconds
Got sol from cvxopt at 6.2552 seconds
status optimal
x [-1.57e-12]
[ 4.08e-04]
[-8.59e-09]
[ 5.53e-10]
[ 3.53e-09]
[-9.72e-10]
[ 8.30e-10]
[-9.18e-04]
[ 5.19e-02]
[-2.12e-20]
[ 2.32e-20]
[ 2.24e-16]
[ 5.46e-17]
[ 2.20e-16]
[ 1.23e-26]
[ 5.00e-16]
[ 6.59e-26]

y [-4.25e-05]
[ 4.64e-05]
[ 4.47e-01]

znl [ 1.00e+00]
[ 1.32e-10]

zl [ 1.09e-01]
[ 4.39e-01]
[ 2.45e-11]

snl [ 1.99e-11]
[ 2.03e-01]

sl [ 1.88e-07]
[ 3.88e-11]
[ 8.74e-01]

gap 2.068840347932985e-08
relative gap 7.866667127620657e-09
primal objective -2.6298816441197554
dual objective -2.629881654604457
primal slack 1.9944303018506357e-11
dual slack 2.4539201182233166e-11
primal infeasibility 2.98538234782961e-09
dual infeasibility 3.036429124305033e-09
AVL run case - lam, AR: 0.40055731598206795 9.999999999611775
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9920150584836795 dimensionless
dydx: [<Quantity(-0.0008541793291738653, 'dimensionless')>, <Quantity(-0.0013850816280497336, 'dimensionless')>]
logspace stuff at 7.3700 seconds
Starting iteration 5 at 7.4093 seconds
AR : 9.999999999611775 dimensionless
CD : 0.07208383829260467 dimensionless
CL : 0.9999998115160276 dimensionless
S : 0.6639218067517706 meter ** 2
V : 3.600069044356993 meter / second
W : 5.270412465184854 newton
Wwing : 0.20138432032400533 newton
e : 0.9921187131763987 dimensionless
lam : 0.40055731598206795 dimensionless
Calling cvxopt.solvers.cp at 7.4182 seconds
Got sol from cvxopt at 7.4316 seconds
status optimal
x [ 8.00e-13]
[ 4.58e-05]
[ 4.24e-09]
[-2.43e-10]
[-1.58e-09]
[ 8.36e-10]
[-3.65e-10]
[-1.03e-04]
[-4.33e-03]
[-2.09e-21]
[ 2.29e-21]
[ 2.23e-16]
[ 5.49e-17]
[ 2.19e-16]
[ 1.20e-26]
[ 5.00e-16]
[ 6.74e-26]

y [-4.18e-06]
[ 4.57e-06]
[ 4.45e-01]

znl [ 1.00e+00]
[ 1.35e-10]

zl [ 1.10e-01]
[ 4.39e-01]
[ 2.41e-11]

snl [ 1.96e-11]
[ 2.03e-01]

sl [ 1.84e-07]
[ 3.80e-11]
[ 8.74e-01]

gap 2.03195584299249e-08
relative gap 7.726423169451732e-09
primal objective -2.629879050666439
dual objective -2.6298790609642584
primal slack 1.96170271739492e-11
dual slack 2.4096853737054615e-11
primal infeasibility 2.932364427218199e-09
dual infeasibility 2.9672633872176456e-09
AVL run case - lam, AR: 0.3988264545569237 9.999999999619773
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9920158805953644 dimensionless
dydx: [<Quantity(-6.436455185498957e-06, 'dimensionless')>, <Quantity(-0.0013814190269140214, 'dimensionless')>]
logspace stuff at 8.5480 seconds
Starting iteration 6 at 8.5887 seconds
AR : 9.999999999619773 dimensionless
CD : 0.07208714305299323 dimensionless
CL : 0.9999998157581855 dimensionless
S : 0.663921806590554 meter ** 2
V : 3.6000690386621303 meter / second
W : 5.270412469588717 newton
Wwing : 0.20138432025057312 newton
e : 0.9920165401543825 dimensionless
lam : 0.3988264545569237 dimensionless
Calling cvxopt.solvers.cp at 8.5977 seconds
Got sol from cvxopt at 8.6111 seconds
status optimal
x [ 2.35e-13]
[ 2.97e-07]
[ 1.09e-09]
[-5.55e-11]
[-3.69e-10]
[ 2.96e-10]
[-8.34e-11]
[-6.65e-07]
[-3.26e-05]
[ 1.22e-24]
[-1.28e-24]
[ 2.23e-16]
[ 5.49e-17]
[ 2.19e-16]
[ 1.20e-26]
[ 5.00e-16]
[ 6.76e-26]

y [ 2.45e-09]
[-2.57e-09]
[ 4.45e-01]

znl [ 1.00e+00]
[ 1.35e-10]

zl [ 1.10e-01]
[ 4.39e-01]
[ 2.40e-11]

snl [ 1.95e-11]
[ 2.03e-01]

sl [ 1.83e-07]
[ 3.78e-11]
[ 8.74e-01]

gap 2.0211071384152197e-08
relative gap 7.685171306919208e-09
primal objective -2.629879097939628
dual objective -2.629879108182283
primal slack 1.9527381358880008e-11
dual slack 2.3958347059782203e-11
primal infeasibility 2.915631182161227e-09
dual infeasibility 2.933788345710238e-09
AVL run case - lam, AR: 0.39881343720167217 9.999999999622123
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wing, index = 1
Getting vortex lattice surface data
	VLM surface name - wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
y: 0.9920158812322761 dimensionless
dydx: [<Quantity(-5.709554107280468e-07, 'dimensionless')>, <Quantity(-0.0013813957757918827, 'dimensionless')>]
logspace stuff at 9.7204 seconds

Objective
---------
   0.072 dimensionless

Variables
---------
   AR     :  10.000        [-]         Wing aspect ratio       
   CD     :   0.072        [-]         Drag Coefficient        
   CL     :   1.000        [-]         Lift Coefficient        
   S      :   0.664     meter ** 2     Wing area               
   V      :   3.600   meter / second   Airspeed                
   W      :   5.270       newton       Aircraft weight         
   Wwing  :   0.201       newton       Wing weight             
   e      :   0.992        [-]         Oswald efficiency factor
   lam    :   0.399        [-]         Wing taper ratio        

Sensitivities
-------------
   Sensitivities not available for optimizations of type Sequential Log Convex Program 

Solve Report
------------
   Solve Method           :  Sequential Log Convex Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  7 
   Termination Status     :  Converged, gradient of Lagrangian (1.043841e-07) within tolerance (1.000000e-06)  

Messages
--------
   1. Wolfe Condition 1 failed at iteration 3 (Step 3).  Watchdog counter is 1

13.872092548132615

real	0m11.437s
user	0m7.349s
sys	0m4.028s
+ status=0
+ set +x

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


=================================================
+ echo 'pyCAPS/GPSize.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/GPSize.py test;
+ python -u pyCAPS/GPSize.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   6339.9402476213 newton

Variables
---------
   AR          :       18.0583068591        [-]         aspect ratio                                                            
   C_D_0       :        0.0127966186        [-]         Drag Coefficient, segment 0                                             
   C_D_1       :        0.0128135534        [-]         Drag Coefficient, segment 1                                             
   C_D_2       :        0.0077622395        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0   :        0.0017626506        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1   :        0.0017626506        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2   :        0.0017626510        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0      :        0.0056016002        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1      :        0.0056028716        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2      :        0.0002594009        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0      :        0.0054327043        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1      :        0.0054483614        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2      :        0.0057382717        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0       :        0.5494535783        [-]         Lift Coefficient, segment 0                                             
   C_L_1       :        0.5495159270        [-]         Lift Coefficient, segment 1                                             
   C_L_2       :        0.1182390122        [-]         Lift Coefficient, segment 2                                             
   I_cap_bar   :        0.0000193397        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar     :    32106.9717613474       newton       Root Bending unit per unit chord                                        
   P_max       :  1211155.7559680410        watt        Maximum Engine Power                                                    
   R           :     4999.9816129528     kilometer      Single Segment range                                                    
   Re_0        :  4636790.3991634697        [-]         Reynolds Number, segment 0                                              
   Re_1        :  4427330.4209076529        [-]         Reynolds Number, segment 1                                              
   Re_2        :  9995446.9239517339        [-]         Reynolds Number, segment 2                                              
   S           :       28.3664420021     meter ** 2     total wing area                                                         
   T_0         :      799.0178645705       newton       Thrust, segment 0                                                       
   T_1         :      729.4239244544       newton       Thrust, segment 1                                                       
   T_2         :     2252.7493855701       newton       Thrust, segment 2                                                       
   V_0         :       69.5874592840   meter / second   Velocity, segment 0                                                     
   V_1         :       66.4439512429   meter / second   Velocity, segment 1                                                     
   V_2         :      150.0084591036   meter / second   Velocity, segment 2                                                     
   V_stall     :       37.9986643205   meter / second   stall speed                                                             
   W_0         :    34307.5807516552       newton       Weight, segment 0                                                       
   W_1         :    31281.5531631161       newton       Weight, segment 1                                                       
   W_2         :    34307.5610637156       newton       Weight, segment 2                                                       
   W_MTO       :    37630.4011124297       newton       Maximum Takeoff Weight                                                  
   W_cap       :     4278.1047592241       newton       Weight of Wing Spar Cap                                                 
   W_eng       :     2854.2361754189       newton       Engine Weight                                                           
   W_fuel_out  :     3314.0247993997       newton       Weight of fuel, outbound                                                
   W_fuel_ret  :     3025.9122892774       newton       Weight of fuel, return                                                  
   W_pay       :     4905.2326701420       newton       Payload Weight                                                          
   W_tilde     :    22457.8594632444       newton       Dry Weight, no wing                                                     
   W_web       :      133.6940460361       newton       Weight of Wing Spar Shear Web                                           
   W_wing      :     8823.3040844200       newton       wing weight                                                             
   W_zfw       :    31281.2018350684       newton       Zero Fuel Weight                                                        
   eta_0_0     :        0.2693167459        [-]         Overall Efficiency, segment 0                                           
   eta_0_1     :        0.2692858916        [-]         Overall Efficiency, segment 1                                           
   eta_0_2     :        0.2791280518        [-]         Overall Efficiency, segment 2                                           
   eta_i_0     :        0.9052651192        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1     :        0.9051614203        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2     :        0.9382448822        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0  :        0.7694756986        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1  :        0.7693875506        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2  :        0.7975082496        [-]         Propeller Efficiency, segment 2                                         
   nu          :        0.7860410805        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p           :        1.9000448519        [-]         Dummy Variable (1+2*lam_w)                                              
   q           :        1.4500404597        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar   :        0.0043345438        [-]         Spar cap thickness per unit chord                                       
   t_web_bar   :        0.0006000270        [-]         Spar web thickness per unit chord                                       
   tau         :        0.1499996279        [-]         airfoil thickness to chord ratio                                        
   z_bre_0     :        0.0922115805        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1     :        0.0923337617        [-]         Breguet Range Factor, segment 1                                         

Constants
---------
   A_prop           :         0.7850000000           meter ** 2          Disk area of propeller                             
   CDA0             :         0.0500000000           meter ** 2          fuselage drag area                                 
   C_Lmax           :         1.5000000000              [-]              max CL with flaps down                             
   N_lift           :         6                         [-]              Ultimate Load Factor                               
   W_fixed          :     14700                        newton            fixed weight                                       
   e                :         0.9500000000              [-]              Oswald efficiency factor                           
   eta_eng          :         0.3500000000              [-]              Engine Efficiency                                  
   eta_v            :         0.8500000000              [-]              Propeller Viscous Efficiency                       
   f_wadd           :         2                         [-]              Added Weight Fraction                              
   g                :         9.8100000000      meter / second ** 2      Gravitational constant                             
   h_fuel           :  46000000                   joule / kilogram       Fuel Specific energy density                       
   k_ew             :         0.0372000000     newton / watt ** 0.803    Constant for engine weight                         
   mu               :         0.0000171000   kilogram / meter / second   viscosity of air                                   
   r_h              :         0.7500000000              [-]              Ratio of height at rear spar to maximum wing height
   rho              :         0.9091220000     kilogram / meter ** 3     density of air                                     
   rho_SL           :         1.2250000000     kilogram / meter ** 3     density of air, sea level                          
   rho_cap          :      2700                kilogram / meter ** 3     Density of wing cap material (aluminum)            
   rho_web          :      2700                kilogram / meter ** 3     Density of wing web material (aluminum)            
   sigma_max        :       250                      megapascal          Allowable tensile stress of aluminum               
   sigma_max_shear  :       167                      megapascal          Allowable shear stress of aluminum                 
   w_bar            :         0.5000000000              [-]              Ratio of spar box width to chord length            

Sensitivities
-------------
   Sensitivities not computed

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

 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!

real	0m10.126s
user	0m9.909s
sys	0m0.411s
+ status=0
+ set +x

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

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

=================================================
+ echo 'pyCAPS/MSES.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/MSES.py test;
+ python -u pyCAPS/MSES.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Objective
---------
   6434.8686749750 newton

Variables
---------
   AR                :        17.8761256208        [-]         aspect ratio                                                            
   Alpha_p20_MSES_0  :        22.6429660188       degree       Angle of Attack + 20deg from MSES, segment 0                            
   Alpha_p20_MSES_1  :        22.6292970435       degree       Angle of Attack + 20deg from MSES, segment 1                            
   Alpha_p20_MSES_2  :        18.8664135056       degree       Angle of Attack + 20deg from MSES, segment 2                            
   C_D_0             :         0.0127145406        [-]         Drag Coefficient, segment 0                                             
   C_D_1             :         0.0126772467        [-]         Drag Coefficient, segment 1                                             
   C_D_2             :         0.0074768775        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0         :         0.0017735677        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1         :         0.0017735677        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2         :         0.0017735677        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0            :         0.0053218277        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1            :         0.0052849468        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2            :         0.0002611265        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0            :         0.0056191456        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1            :         0.0056187325        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2            :         0.0054421793        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0             :         0.5327871651        [-]         Lift Coefficient, segment 0                                             
   C_L_1             :         0.5309281670        [-]         Lift Coefficient, segment 1                                             
   C_L_2             :         0.1180315549        [-]         Lift Coefficient, segment 2                                             
   C_L_MSES_0        :         0.5327871651        [-]         Lift Coefficient from MSES, segment 0                                   
   C_L_MSES_1        :         0.5309281670        [-]         Lift Coefficient from MSES, segment 1                                   
   C_L_MSES_2        :         0.1180315549        [-]         Lift Coefficient from MSES, segment 2                                   
   I_cap_bar         :         0.0000189749        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar           :     31633.5137385074       newton       Root Bending unit per unit chord                                        
   P_max             :   1155617.0255680946        watt        Maximum Engine Power                                                    
   R                 :      5000.0000033336     kilometer      Single Segment range                                                    
   Re_0              :   4714256.8311429033        [-]         Reynolds Number, segment 0                                              
   Re_1              :   4504811.2195102284        [-]         Reynolds Number, segment 1                                              
   Re_2              :  10014801.7689142171        [-]         Reynolds Number, segment 2                                              
   S                 :        28.1917813790     meter ** 2     total wing area                                                         
   T_0               :       812.1924689899       newton       Thrust, segment 0                                                       
   T_1               :       739.4274750426       newton       Thrust, segment 1                                                       
   T_2               :      2155.8460657551       newton       Thrust, segment 2                                                       
   V_0               :        70.6090282177   meter / second   Velocity, segment 0                                                     
   V_1               :        67.4719865369   meter / second   Velocity, segment 1                                                     
   V_2               :       150.0000229949   meter / second   Velocity, segment 2                                                     
   V_stall           :        37.9999993888   meter / second   stall speed                                                             
   W_0               :     34032.6295170036       newton       Weight, segment 0                                                       
   W_1               :     30966.4603184510       newton       Weight, segment 1                                                       
   W_2               :     34032.6295170036       newton       Weight, segment 2                                                       
   W_MTO             :     37401.3303577012       newton       Maximum Takeoff Weight                                                  
   W_cap             :      4175.0307826594       newton       Weight of Wing Spar Cap                                                 
   W_eng             :      2747.7840319609       newton       Engine Weight                                                           
   W_fuel_out        :      3368.6997598764       newton       Weight of fuel, outbound                                                
   W_fuel_ret        :      3066.1689150985       newton       Weight of fuel, return                                                  
   W_pay             :      4905.0001650177       newton       Payload Weight                                                          
   W_tilde           :     22352.7841009881       newton       Dry Weight, no wing                                                     
   W_web             :       131.8074022566       newton       Weight of Wing Spar Shear Web                                           
   W_wing            :      8613.6764251259       newton       wing weight                                                             
   W_zfw             :     30966.4602788176       newton       Zero Fuel Weight                                                        
   eta_0_0           :         0.2696090441        [-]         Overall Efficiency, segment 0                                           
   eta_0_1           :         0.2696770159        [-]         Overall Efficiency, segment 1                                           
   eta_0_2           :         0.2798306963        [-]         Overall Efficiency, segment 2                                           
   eta_i_0           :         0.9062488877        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1           :         0.9064773642        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2           :         0.9406073826        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0        :         0.7703115546        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1        :         0.7705057596        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2        :         0.7995162752        [-]         Propeller Efficiency, segment 2                                         
   nu                :         0.7859964418        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p                 :         1.9000000050        [-]         Dummy Variable (1+2*lam_w)                                              
   q                 :         1.4500000078        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar         :         0.0042483467        [-]         Spar cap thickness per unit chord                                       
   t_web_bar         :         0.0005949059        [-]         Spar web thickness per unit chord                                       
   tau               :         0.1499765271        [-]         airfoil thickness to chord ratio                                        
   z_bre_0           :         0.0943866350        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1           :         0.0944151528        [-]         Breguet Range Factor, segment 1                                         

Sensitivities
-------------
   Sensitivities not available for optimizations of type Sequential Log Convex Program 

Solve Report
------------
   Solve Method           :  Sequential Log Convex Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  23 
   Termination Status     :  Converged, relative change in the objective function (5.56e-06) is witin specified tolerance (1.00e-05) 

Messages
--------
    1. Attempted step of size 1.00e+00 at iteration 2 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    2. Attempted step of size 9.00e-01 at iteration 2 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    3. Wolfe Condition 1 failed at iteration 4 (Step 4).  Watchdog counter is 1
    4. Wolfe Condition 1 failed at iteration 7 (Step 7).  Watchdog counter is 1
    5. Wolfe Condition 1 failed at iteration 10 (Step 10).  Watchdog counter is 1
    6. Wolfe Condition 1 failed at iteration 11 (Step 11).  Watchdog counter is 2
    7. Attempted step of size 1.00e+00 at iteration 12 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    8. Wolfe Condition 1 failed at iteration 12 (Step 12).  Watchdog counter is 3
    9. Attempted step of size 1.00e+00 at iteration 13 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   10. Wolfe Condition 1 failed at iteration 13 (Step 13).  Watchdog counter is 4
   11. Attempted step of size 1.00e+00 at iteration 15 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   12. Wolfe Condition 1 failed at iteration 17 (Step 17).  Watchdog counter is 1
   13. Wolfe Condition 1 failed at iteration 18 (Step 18).  Watchdog counter is 2
   14. Attempted step of size 3.81e-01 at iteration 19 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   15. Wolfe Condition 1 failed at iteration 19 (Step 19).  Watchdog counter is 3
   16. Wolfe Condition 1 failed at iteration 22 (Step 22).  Watchdog counter is 1


real	3m52.819s
user	3m43.647s
sys	0m8.251s
+ status=0
+ set +x

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


=================================================
+ echo 'pyCAPS/Camber.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/Camber.py test;
+ python -u pyCAPS/Camber.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Objective
---------
   5426.1151483814 newton

Variables
---------
   AR                :       19.2162640327        [-]         aspect ratio                                                            
   Alpha_p20_MSES_0  :       17.8914424476       degree       Angle of Attack + 20deg from MSES, segment 0                            
   Alpha_p20_MSES_1  :       17.7697968272       degree       Angle of Attack + 20deg from MSES, segment 1                            
   Alpha_p20_MSES_2  :       14.0762024635       degree       Angle of Attack + 20deg from MSES, segment 2                            
   C_D_0             :        0.0110624638        [-]         Drag Coefficient, segment 0                                             
   C_D_1             :        0.0107985659        [-]         Drag Coefficient, segment 1                                             
   C_D_2             :        0.0066444504        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0         :        0.0017867958        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1         :        0.0017867958        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2         :        0.0017867958        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0            :        0.0052915770        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1            :        0.0049110860        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2            :        0.0002509872        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0            :        0.0039840922        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1            :        0.0041006848        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2            :        0.0046066672        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0             :        0.5506832646        [-]         Lift Coefficient, segment 0                                             
   C_L_1             :        0.5306373281        [-]         Lift Coefficient, segment 1                                             
   C_L_2             :        0.1199145032        [-]         Lift Coefficient, segment 2                                             
   C_L_MSES_0        :        0.5506832646        [-]         Lift Coefficient from MSES, segment 0                                   
   C_L_MSES_1        :        0.5306373281        [-]         Lift Coefficient from MSES, segment 1                                   
   C_L_MSES_2        :        0.1199145032        [-]         Lift Coefficient from MSES, segment 2                                   
   I_cap_bar         :        0.0000216301        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar           :    33586.4310550239       newton       Root Bending unit per unit chord                                        
   P_max             :  1012883.7806372986        watt        Maximum Engine Power                                                    
   R                 :     5000.0000034463     kilometer      Single Segment range                                                    
   Re_0              :  4495822.2263598200        [-]         Reynolds Number, segment 0                                              
   Re_1              :  4401584.9845399503        [-]         Reynolds Number, segment 1                                              
   Re_2              :  9626916.1443104651        [-]         Reynolds Number, segment 2                                              
   S                 :       27.9909833450     meter ** 2     total wing area                                                         
   T_0               :      689.8159590696       newton       Thrust, segment 0                                                       
   T_1               :      645.4379395215       newton       Thrust, segment 1                                                       
   T_2               :     1902.1543451014       newton       Thrust, segment 2                                                       
   V_0               :       70.0425369997   meter / second   Velocity, segment 0                                                     
   V_1               :       68.5713261573   meter / second   Velocity, segment 1                                                     
   V_2               :      150.0000046309   meter / second   Velocity, segment 2                                                     
   V_stall           :       37.9999468104   meter / second   stall speed                                                             
   W_0               :    34329.1239584747       newton       Weight, segment 0                                                       
   W_1               :    31708.3658558579       newton       Weight, segment 1                                                       
   W_2               :    34329.1239584747       newton       Weight, segment 2                                                       
   W_MTO             :    37134.8408818262       newton       Maximum Takeoff Weight                                                  
   W_cap             :     4681.6117001178       newton       Weight of Wing Spar Cap                                                 
   W_eng             :     2471.6469879882       newton       Engine Weight                                                           
   W_fuel_out        :     2805.3570136383       newton       Weight of fuel, outbound                                                
   W_fuel_ret        :     2620.7581347431       newton       Weight of fuel, return                                                  
   W_pay             :     4905.0000233408       newton       Payload Weight                                                          
   W_tilde           :    22076.6469868519       newton       Dry Weight, no wing                                                     
   W_web             :      134.2483282176       newton       Weight of Wing Spar Shear Web                                           
   W_wing            :     9631.7196947430       newton       wing weight                                                             
   W_zfw             :    31708.3658072022       newton       Zero Fuel Weight                                                        
   camberLocation    :        0.7949613224        [-]         location of maximum airfoil camber scaled by chord                      
   eta_0_0           :        0.2728257920        [-]         Overall Efficiency, segment 0                                           
   eta_0_1           :        0.2733261445        [-]         Overall Efficiency, segment 1                                           
   eta_0_2           :        0.2817016557        [-]         Overall Efficiency, segment 2                                           
   eta_i_0           :        0.9170614858        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1           :        0.9187433430        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2           :        0.9468963218        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0        :        0.7795022629        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1        :        0.7809318415        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2        :        0.8048618736        [-]         Propeller Efficiency, segment 2                                         
   maxCamber         :        0.0404380681        [-]         maximum airfoil camber scaled by chord                                  
   nu                :        0.7859963901        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p                 :        1.9000000025        [-]         Dummy Variable (1+2*lam_w)                                              
   q                 :        1.4500000039        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar         :        0.0049899222        [-]         Spar cap thickness per unit chord                                       
   t_web_bar         :        0.0006416725        [-]         Spar web thickness per unit chord                                       
   tau               :        0.1486735000        [-]         airfoil thickness to chord ratio                                        
   z_bre_0           :        0.0785522626        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1           :        0.0794369045        [-]         Breguet Range Factor, segment 1                                         

Sensitivities
-------------
   Sensitivities not available for optimizations of type Sequential Log Convex Program 

Solve Report
------------
   Solve Method           :  Sequential Log Convex Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  76 
   Termination Status     :  Converged, relative change in the objective function (1.16e-06) is witin specified tolerance (1.00e-05) 

Messages
--------
    1. Attempted step of size 1.00e+00 at iteration 2 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    2. Attempted step of size 1.00e+00 at iteration 3 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    3. Attempted step of size 3.00e-01 at iteration 3 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    4. Attempted step of size 9.00e-02 at iteration 3 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    5. Wolfe Condition 1 failed at iteration 4 (Step 4).  Watchdog counter is 1
    6. Attempted step of size 1.00e+00 at iteration 5 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    7. Wolfe Condition 1 failed at iteration 7 (Step 7).  Watchdog counter is 1
    8. Wolfe Condition 1 failed at iteration 8 (Step 8).  Watchdog counter is 2
    9. Wolfe Condition 1 failed at iteration 9 (Step 9).  Watchdog counter is 3
   10. Attempted step of size 1.00e+00 at iteration 10 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   11. Wolfe Condition 1 failed at iteration 11 (Step 11).  Watchdog counter is 1
   12. Wolfe Condition 1 failed at iteration 13 (Step 13).  Watchdog counter is 1
   13. Attempted step of size 1.00e+00 at iteration 14 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   14. Wolfe Condition 1 failed at iteration 16 (Step 16).  Watchdog counter is 1
   15. Attempted step of size 2.68e-01 at iteration 23 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   16. Attempted step of size 2.25e-01 at iteration 26 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   17. Attempted step of size 1.49e-01 at iteration 38 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   18. Wolfe Condition 1 failed at iteration 40 (Step 40).  Watchdog counter is 1
   19. Attempted step of size 1.27e-01 at iteration 45 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   20. Attempted step of size 1.21e-01 at iteration 48 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   21. Attempted step of size 9.93e-02 at iteration 61 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   22. Wolfe Condition 1 failed at iteration 75 (Step 75).  Watchdog counter is 1


real	11m38.399s
user	11m10.796s
sys	0m25.426s
+ status=0
+ set +x

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


=================================================
+ echo 'pyCAPS/CMConstraint.py test;'
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
pyCAPS/CMConstraint.py test;
+ python -u pyCAPS/CMConstraint.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Getting CFD design variables.......
	Number of design variables - 3
	Design Variable name - camber
	Design Variable name - maxloc
	Design Variable name - thickness
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05

Objective
---------
   6382.6426006034 newton

Variables
---------
   AR                :        17.7333703368        [-]         aspect ratio                                                            
   Alpha_p20_MSES_0  :        22.5429905278       degree       Angle of Attack + 20deg from MSES, segment 0                            
   Alpha_p20_MSES_1  :        22.4111491959       degree       Angle of Attack + 20deg from MSES, segment 1                            
   Alpha_p20_MSES_2  :        18.7501009583       degree       Angle of Attack + 20deg from MSES, segment 2                            
   C_D_0             :         0.0127173739        [-]         Drag Coefficient, segment 0                                             
   C_D_1             :         0.0124235499        [-]         Drag Coefficient, segment 1                                             
   C_D_2             :         0.0076171667        [-]         Drag Coefficient, segment 2                                             
   C_Dfuse_0         :         0.0017790524        [-]         Fuselage Drag Coefficient, segment 0                                    
   C_Dfuse_1         :         0.0017790524        [-]         Fuselage Drag Coefficient, segment 1                                    
   C_Dfuse_2         :         0.0017790524        [-]         Fuselage Drag Coefficient, segment 2                                    
   C_Di_0            :         0.0054317603        [-]         Induced Drag Coefficient, segment 0                                     
   C_Di_1            :         0.0051614721        [-]         Induced Drag Coefficient, segment 1                                     
   C_Di_2            :         0.0002635564        [-]         Induced Drag Coefficient, segment 2                                     
   C_Dp_0            :         0.0055065615        [-]         Wing Profile Drag Coefficient, segment 0                                
   C_Dp_1            :         0.0054830267        [-]         Wing Profile Drag Coefficient, segment 1                                
   C_Dp_2            :         0.0055745543        [-]         Wing Profile Drag Coefficient, segment 2                                
   C_L_0             :         0.5360678775        [-]         Lift Coefficient, segment 0                                             
   C_L_1             :         0.5221785656        [-]         Lift Coefficient, segment 1                                             
   C_L_2             :         0.1180981774        [-]         Lift Coefficient, segment 2                                             
   C_L_MSES_0        :         0.5360678775        [-]         Lift Coefficient from MSES, segment 0                                   
   C_L_MSES_1        :         0.5221785656        [-]         Lift Coefficient from MSES, segment 1                                   
   C_L_MSES_2        :         0.1180981774        [-]         Lift Coefficient from MSES, segment 2                                   
   I_cap_bar         :         0.0000187470        [-]         Area moment of inertia of cap on 2D cross section, normalized by chord^4
   M_r_bar           :     31432.1630184581       newton       Root Bending unit per unit chord                                        
   P_max             :   1174722.0623270900        watt        Maximum Engine Power                                                    
   R                 :      5000.0000379642     kilometer      Single Segment range                                                    
   Re_0              :   4714269.7355839955        [-]         Reynolds Number, segment 0                                              
   Re_1              :   4560828.3991480591        [-]         Reynolds Number, segment 1                                              
   Re_2              :  10039944.6132115945        [-]         Reynolds Number, segment 2                                              
   S                 :        28.1055377816     meter ** 2     total wing area                                                         
   T_0               :       805.4977326683       newton       Thrust, segment 0                                                       
   T_1               :       735.5874132058       newton       Thrust, segment 1                                                       
   T_2               :      2189.5656770467       newton       Thrust, segment 2                                                       
   V_0               :        70.4293805792   meter / second   Velocity, segment 0                                                     
   V_1               :        68.1346248085   meter / second   Velocity, segment 1                                                     
   V_2               :       150.0000188498   meter / second   Velocity, segment 2                                                     
   V_stall           :        37.9999983650   meter / second   stall speed                                                             
   W_0               :     33947.7281781365       newton       Weight, segment 0                                                       
   W_1               :     30904.2652518139       newton       Weight, segment 1                                                       
   W_2               :     33947.7281781365       newton       Weight, segment 2                                                       
   W_MTO             :     37286.9111353013       newton       Maximum Takeoff Weight                                                  
   W_cap             :      4126.5009765832       newton       Weight of Wing Spar Cap                                                 
   W_eng             :      2784.1970728166       newton       Engine Weight                                                           
   W_fuel_out        :      3339.1797308950       newton       Weight of fuel, outbound                                                
   W_fuel_ret        :      3043.4628697084       newton       Weight of fuel, return                                                  
   W_pay             :      4905.0004716166       newton       Payload Weight                                                          
   W_tilde           :     22389.1976028674       newton       Dry Weight, no wing                                                     
   W_web             :       131.0323168331       newton       Weight of Wing Spar Shear Web                                           
   W_wing            :      8515.0668638773       newton       wing weight                                                             
   W_zfw             :     30904.2646428063       newton       Zero Fuel Weight                                                        
   camberLocation    :         0.3680356411        [-]         location of maximum airfoil camber scaled by chord                      
   eta_0_0           :         0.2696744327        [-]         Overall Efficiency, segment 0                                           
   eta_0_1           :         0.2702130567        [-]         Overall Efficiency, segment 1                                           
   eta_0_2           :         0.2795857752        [-]         Overall Efficiency, segment 2                                           
   eta_i_0           :         0.9064686815        [-]         Inviscid Propeller Efficiency, segment 0                                
   eta_i_1           :         0.9082791822        [-]         Inviscid Propeller Efficiency, segment 1                                
   eta_i_2           :         0.9397841182        [-]         Inviscid Propeller Efficiency, segment 2                                
   eta_prop_0        :         0.7704983793        [-]         Propeller Efficiency, segment 0                                         
   eta_prop_1        :         0.7720373049        [-]         Propeller Efficiency, segment 1                                         
   eta_prop_2        :         0.7988165005        [-]         Propeller Efficiency, segment 2                                         
   maxCamber         :         0.0216847844        [-]         maximum airfoil camber scaled by chord                                  
   negCMp1_0         :         1.0526444661        [-]         Negative CM about 0.25c + 1, segment 0                                  
   negCMp1_1         :         1.0529199185        [-]         Negative CM about 0.25c + 1, segment 1                                  
   negCMp1_2         :         1.0545680466        [-]         Negative CM about 0.25c + 1, segment 2                                  
   nu                :         0.7859965065        [-]         Placeholder, (1+lam_w+lam_w**2)/(1+lam_w)**2                            
   p                 :         1.9000000307        [-]         Dummy Variable (1+2*lam_w)                                              
   q                 :         1.4500000425        [-]         Dummy Variable (1+lam_w)                                                
   t_cap_bar         :         0.0042012338        [-]         Spar cap thickness per unit chord                                       
   t_web_bar         :         0.0005933949        [-]         Spar web thickness per unit chord                                       
   tau               :         0.1498553099        [-]         airfoil thickness to chord ratio                                        
   z_bre_0           :         0.0938224326        [-]         Breguet Range Factor, segment 0                                         
   z_bre_1           :         0.0939302493        [-]         Breguet Range Factor, segment 1                                         

Sensitivities
-------------
   Sensitivities not available for optimizations of type Sequential Log Convex Program 

Solve Report
------------
   Solve Method           :  Sequential Log Convex Program 
   Classification         :  Iterative 
   Solver                 :  cvxopt 
   Number of Iterations   :  21 
   Termination Status     :  Converged, relative change in the objective function (8.56e-06) is witin specified tolerance (1.00e-05) 

Messages
--------
    1. Wolfe Condition 1 failed at iteration 2 (Step 2).  Watchdog counter is 1
    2. Attempted step of size 1.00e+00 at iteration 3 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    3. Wolfe Condition 1 failed at iteration 4 (Step 4).  Watchdog counter is 1
    4. Wolfe Condition 1 failed at iteration 5 (Step 5).  Watchdog counter is 2
    5. Wolfe Condition 1 failed at iteration 7 (Step 7).  Watchdog counter is 1
    6. Wolfe Condition 1 failed at iteration 9 (Step 9).  Watchdog counter is 1
    7. Wolfe Condition 1 failed at iteration 10 (Step 10).  Watchdog counter is 2
    8. Attempted step of size 1.00e+00 at iteration 11 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
    9. Wolfe Condition 1 failed at iteration 11 (Step 11).  Watchdog counter is 3
   10. Wolfe Condition 1 failed at iteration 14 (Step 14).  Watchdog counter is 1
   11. Attempted step of size 1.00e+00 at iteration 15 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   12. Attempted step of size 3.00e-01 at iteration 15 is too large and is causing a constraint to return as imaginary.  Decreasing according to the tau schedule.
   13. Wolfe Condition 1 failed at iteration 15 (Step 15).  Watchdog counter is 2
   14. Wolfe Condition 1 failed at iteration 20 (Step 20).  Watchdog counter is 1


real	3m21.134s
user	3m13.775s
sys	0m7.174s
+ 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 50608
-rw-r--r--  1 jenkins  staff   1.2M Dec 20 15:08 ASTRO.D01
-rw-r--r--  1 jenkins  staff   277K Dec 20 15:08 ASTRO.IDX
-rwxr-xr-x  1 jenkins  staff   129K Dec 20 15:10 ESPxddm
-rwxr-xr-x  1 jenkins  staff   210K Feb 28 10:11 Slugs
-rwxr-xr-x  1 jenkins  staff    85K Feb 28 10:11 TestFit
-rwxr-xr-x  1 jenkins  staff   1.8M Dec 20 15:08 avl
-rwxr-xr-x  1 jenkins  staff    34K Feb 28 10:11 cart3dTest
-rwxr-xr-x  1 jenkins  staff    34K Mar  6 20:03 egads2cart
-rwxr-xr-x  1 jenkins  staff   416K Dec 20 15:08 friction
-rwxr-xr-x  1 jenkins  staff   8.9M Dec 20 15:08 mastros.exe
-rwxr-xr-x  1 jenkins  staff   2.2M Dec 20 15:08 mses
-rwxr-xr-x  1 jenkins  staff   2.5M Dec 20 15:08 mset
-rwxr-xr-x  1 jenkins  staff    34K Feb 28 10:11 phaseUtil
-rw-r--r--  1 jenkins  staff   1.6K Mar  6 20:32 pod.egads
-rw-r--r--  1 jenkins  staff     0B Mar  6 20:32 port7681.jrnl
-rwxr-xr-x  1 jenkins  staff   1.2M Dec 20 15:08 pplot
-rwxr-xr-x  1 jenkins  staff   1.2M Dec 20 15:08 pxplot
-rwxr-xr-x  1 jenkins  staff    68K Feb 28 10:11 sensCSM
-rwxr-xr-x  1 jenkins  staff   206K Feb 28 10:11 serveCSM
-rwxr-xr-x  1 jenkins  staff   174K Feb 28 10:11 serveESP
-rwxr-xr-x  1 jenkins  staff    51K Feb 28 10:11 vCurvature
-rwxr-xr-x  1 jenkins  staff    35K Feb 28 10:11 vGeom
-rwxr-xr-x  1 jenkins  staff    52K Feb 28 10:11 vTess
-rwxr-xr-x  1 jenkins  staff   1.9M Mar  6 20:03 vTesstatic
-rw-r--r--  1 jenkins  staff   195K Mar  6 20:32 wingMultiModel.bdf
-rwxr-xr-x  1 jenkins  staff   1.8M Dec 20 15:08 xfoil
( 1 / 4 )
data/Plugs/plugs0a.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0a.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0a.vfy", so verification is being skipped

===================================
PLUGS with 4562 points in the cloud
===================================


PLUGS phase1: match bounding boxes


PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
    Pass  1 converged, dmax= 5.416e-07,     rmsbest= 6.132e-04, reclass= 4562, unclass=    0
Starting pass 2 (of 25) of phase2
    Pass  2 converged, dmax= 5.366e-07,     rmsbest= 7.097e-04, reclass=    2, unclass=    0
Starting pass 3 (of 25) of phase2

    Phase2 passes converged because points are classified same as previous pass


==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m6.799s
user	0m6.685s
sys	0m0.393s
++ set +x
data/Plugs/plugs0a                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 2 / 4 )
data/Plugs/plugs0b.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0b.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0b.vfy", so verification is being skipped

===================================
PLUGS with 4562 points in the cloud
===================================


PLUGS phase1: match bounding boxes


PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
    Pass  1 converged, dmax= 3.039e-07,     rmsbest= 4.036e-02, reclass= 4562, unclass=    0
Starting pass 2 (of 25) of phase2
    Pass  2 converged, dmax= 2.814e-07,     rmsbest= 1.924e-03, reclass= 1033, unclass=    0
Starting pass 3 (of 25) of phase2
    Pass  3 converged, dmax= 4.494e-07,     rmsbest= 5.920e-04, reclass=  473, unclass=    0
Starting pass 4 (of 25) of phase2
    Pass  4 converged, dmax= 5.366e-07,     rmsbest= 7.097e-04, reclass=   17, unclass=    0
Starting pass 5 (of 25) of phase2

    Phase2 passes converged because points are classified same as previous pass


==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m6.202s
user	0m7.633s
sys	0m0.056s
++ set +x
data/Plugs/plugs0b                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 3 / 4 )
data/Plugs/plugs0c.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0c.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0c.vfy", so verification is being skipped

===================================
PLUGS with 4562 points in the cloud
===================================


PLUGS phase1: match bounding boxes


PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
    Pass  1 ran out of iterations,          rmsbest= 1.677e-01, reclass= 4562, unclass=  554
Starting pass 2 (of 25) of phase2
    Pass  2 converged, dmax= 4.016e-07,     rmsbest= 6.330e-02, reclass= 1676, unclass=    0
Starting pass 3 (of 25) of phase2
    Pass  3 converged, dmax= 1.881e-07,     rmsbest= 8.736e-03, reclass=  791, unclass=    0
Starting pass 4 (of 25) of phase2
    Pass  4 converged, dmax= 3.081e-07,     rmsbest= 1.037e-03, reclass=  428, unclass=    0
Starting pass 5 (of 25) of phase2
    Pass  5 converged, dmax= 5.816e-07,     rmsbest= 7.097e-04, reclass=  109, unclass=    0
Starting pass 6 (of 25) of phase2

    Phase2 passes converged because points are classified same as previous pass


==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m16.520s
user	0m24.859s
sys	0m0.112s
++ set +x
data/Plugs/plugs0c                  passed (as expected)
--------------------------------------------------------------------------------------------------
( 4 / 4 )
data/Plugs/plugs0d.csm;
++ /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/bin/serveCSM /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0d.csm -outLevel 0 -plugs 25 -plot /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/plugs0.cloud -batch -verify -jrnl /Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl
WARNING:: cannot open "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/verify_7.8.0/plugs0d.vfy", so verification is being skipped

===================================
PLUGS with 4562 points in the cloud
===================================


PLUGS phase1: match bounding boxes


PLUGS phase2: match cloud points
Starting pass 1 (of 25) of phase2
    Pass  1 ran out of iterations,          rmsbest= 1.677e-01, reclass= 4562, unclass=  554
Starting pass 2 (of 25) of phase2
    Pass  2 converged, dmax= 4.016e-07,     rmsbest= 6.330e-02, reclass= 1676, unclass=    0
Starting pass 3 (of 25) of phase2
    Pass  3 converged, dmax= 1.881e-07,     rmsbest= 8.736e-03, reclass=  791, unclass=    0
Starting pass 4 (of 25) of phase2
    Pass  4 converged, dmax= 3.081e-07,     rmsbest= 1.037e-03, reclass=  428, unclass=    0
Starting pass 5 (of 25) of phase2
    Pass  5 converged, dmax= 5.816e-07,     rmsbest= 7.097e-04, reclass=  109, unclass=    0
Starting pass 6 (of 25) of phase2

    Phase2 passes converged because points are classified same as previous pass


==> Opening input journal file "/Users/jenkins/workspace/ESP_bPreBuilt/ESPbeta/EngSketchPad/data/Plugs/buildFinal.jrnl"


==> Closing input journal file

==> serveCSM completed successfully with no verification data

real	0m16.435s
user	0m24.680s
sys	0m0.114s
++ set +x
data/Plugs/plugs0d                  passed (as expected)
--------------------------------------------------------------------------------------------------
[Execution node] check if [macys] is in [[viggen]]
Run condition [Execution node ] preventing perform for step [Execute shell]
[Execution node] check if [macys] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_bPreBuilt')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_bPreBuilt/ESPVersion=beta,buildnode=macys #67'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS