Started by upstream project "ESP_Beta" build number 711
originally caused by:
 Started by remote host 18.18.33.14
Running as SYSTEM
[EnvInject] - Loading node environment variables.
Building remotely on reynolds-centOS7 in workspace /home/jenkins/workspace/ESP_Beta/7.8/LINUX64
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] Done
Checking out a fresh workspace because there's no workspace at /home/jenkins/workspace/ESP_Beta/7.8/LINUX64
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-04-28T10:16:15.782 -0400' --quiet
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
At revision 2481

Checking out a fresh workspace because /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP doesn't exist
Cleaning local Directory JenkinsESP
Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-04-28T10:16:15.782 -0400' --quiet
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
At revision 858

No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
[GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [reynolds-centOS7] is in [[macys, macys_VM, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-ubuntu18]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[LINUX64] $ /bin/bash -ex /tmp/jenkins9588647078881648920.sh
+ bash -ex /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/ESP_Beta.sh
+ source /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.6
++ OCCTREF=7.6
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.34.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ reynolds-centOS7 == \r\e\y\n\o\l\d\s ]]
++ [[ LINUX64 == *\.\i\f\o\r\t ]]
++ '[' -f /opt/intel/oneapi/setvars.sh ']'
++ '[' -f /home/jenkins/.bashrc ']'
++ source /home/jenkins/.bashrc
+++ '[' -f /etc/bashrc ']'
+++ . /etc/bashrc
++++ '[' '' ']'
++++ shopt -q login_shell
++++ '[' 1001 -gt 199 ']'
+++++ /usr/bin/id -gn
+++++ /usr/bin/id -un
++++ '[' jenkins = jenkins ']'
++++ umask 002
++++ SHELL=/bin/bash
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/256term.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/256term.sh
+++++ local256=
+++++ '[' -n '' ']'
+++++ '[' -n '' ']'
+++++ unset local256
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/abrt-console-notification.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/abrt-console-notification.sh
+++++ tty -s
+++++ return 0
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/bash_completion.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/bash_completion.sh
+++++ '[' -z '4.2.46(2)-release' -o -z '' -o -n '' ']'
+++++ return
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/colorgrep.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/colorgrep.sh
+++++ /usr/libexec/grepconf.sh -c
+++++ alias 'grep=grep --color=auto'
+++++ alias 'egrep=egrep --color=auto'
+++++ alias 'fgrep=fgrep --color=auto'
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/colorls.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/colorls.sh
+++++ '[' '!' -t 0 ']'
+++++ return
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/flatpak.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/flatpak.sh
+++++ '[' /exports/share:/var/lib/flatpak/exports/share:/usr/local/share:/usr/share = /home/jenkins/.local/share/flatpak/exports/share:/var/lib/flatpak/exports/share:/usr/local/share:/usr/share ']'
+++++ export XDG_DATA_DIRS
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/lang.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/lang.sh
+++++ sourced=0
+++++ '[' -n en_US.UTF-8 ']'
+++++ saved_lang=en_US.UTF-8
+++++ '[' -f /home/jenkins/.i18n ']'
+++++ LANG=en_US.UTF-8
+++++ unset saved_lang
+++++ '[' 0 = 1 ']'
+++++ unset sourced
+++++ unset langfile
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/less.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/less.sh
+++++ '[' -x /usr/bin/lesspipe.sh ']'
+++++ export 'LESSOPEN=||/usr/bin/lesspipe.sh %s'
+++++ LESSOPEN='||/usr/bin/lesspipe.sh %s'
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/PackageKit.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/PackageKit.sh
+++++ [[ -n '' ]]
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/vim.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/vim.sh
+++++ '[' -n '4.2.46(2)-release' -o -n '' -o -n '' ']'
+++++ '[' -x /usr/bin/id ']'
++++++ /usr/bin/id -u
+++++ ID=1001
+++++ '[' -n 1001 -a 1001 -le 200 ']'
+++++ alias vi
+++++ alias vi=vim
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/vte.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/vte.sh
+++++ '[' -n '4.2.46(2)-release' -o -n '' ']'
+++++ [[ ehxB == *i* ]]
+++++ return 0
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/which2.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/which2.sh
+++++ alias 'which=alias | /usr/bin/which --tty-only --read-alias --show-dot --show-tilde'
++++ unset i
++++ unset -f pathmunge
++ export CAPS_OUTLEVEL=0
++ CAPS_OUTLEVEL=0
++ [[ LINUX64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64
++ ESP_BLOC=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64
++ export ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64
++ ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64
++ export JULIA_DEPOT_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/julia
++ JULIA_DEPOT_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.6 != '' ]]
++ [[ '' != '' ]]
++ [[ reynolds-centOS7 == *\r\e\y\n\o\l\d\s* ]]
++ [[ '' != '' ]]
++ [[ -d /home/jenkins/util/ESP/Python/ESP_Python-3.11.9 ]]
++ export PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9
++ PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9
++ export PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export LD_LIBRARY_PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ LD_LIBRARY_PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ export EMPnumProc=4
++ EMPnumProc=4
++ export OMP_NUM_THREADS=4
++ OMP_NUM_THREADS=4
++ '[' '!' -z '' ']'
+++ ls -d /home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASARCH=.
++ CASARCH=.
++ export LD_LIBRARY_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ LD_LIBRARY_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ export ESP_EXTERN_LIBS=/home/jenkins/util/ESP/ExternLibs
++ ESP_EXTERN_LIBS=/home/jenkins/util/ESP/ExternLibs
++ export AFLR=/home/jenkins/util/AFLR/aflr_lib_11.5.14
++ AFLR=/home/jenkins/util/AFLR/aflr_lib_11.5.14
++ export AFLR_ARCH=Linux-x86-64
++ AFLR_ARCH=Linux-x86-64
++ export PATH=/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export CART3D=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16
++ CART3D=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16
++ export CART3D_ARCH=X86_64_ICC
++ CART3D_ARCH=X86_64_ICC
++ export PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export PATH=/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export PATH=/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export MYSTRAN_directory=/home/jenkins/util/mystran/MYSTRAN/Binaries
++ MYSTRAN_directory=/home/jenkins/util/mystran/MYSTRAN/Binaries
++ export PATH=/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export PATH=/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/aim/pointwise/glyph
++ export PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ [[ reynolds-centOS7 == \r\e\y\n\o\l\d\s ]]
++ export SU2_HOME=/home/jenkins/util/SU2/SU2-v8.0.0
++ SU2_HOME=/home/jenkins/util/SU2/SU2-v8.0.0
++ export SU2_RUN=/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ SU2_RUN=/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ export PATH=/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ '[' -d /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16 ']'
++ export PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ [[ reynolds-centOS7 == \m\a\c\y\s* ]]
++ [[ reynolds-centOS7 == \v\i\g\g\e\n ]]
+++ python-config --includes
++ export 'PYTHONINC=. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
++ PYTHONINC='. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
+++ python-config --help
++ [[ Usage: /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/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/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl  -lutil -lm '
++ PYTHONLIB=' -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl  -lutil -lm '
++ [[ reynolds-centOS7 == \m\a\c\y\s ]]
++ [[ reynolds-centOS7 == \v\i\g\g\e\n ]]
++ export PYTHONUNBUFFERED=true
++ PYTHONUNBUFFERED=true
++ export PYTHONFAULTHANDLER=true
++ PYTHONFAULTHANDLER=true
++ python --version
Python 3.11.9
++ [[ LINUX64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/data
++ CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/data
+ virtualenv /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv
created virtual environment CPython3.11.9.final.0-64 in 382ms
  creator CPython3Posix(dest=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv, clear=False, no_vcs_ignore=False, global=False)
  seeder FromAppData(download=False, pip=bundle, setuptools=bundle, wheel=bundle, via=copy, app_data_dir=/home/jenkins/.local/share/virtualenv)
    added seed packages: pip==24.0, setuptools==69.2.0, wheel==0.43.0
  activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator
+ . /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/activate
++ '[' /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/activate = /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/ESP_Beta.sh ']'
++ deactivate nondestructive
++ unset -f pydoc
++ '[' -z '' ']'
++ '[' -z '' ']'
++ hash -r
++ '[' -z '' ']'
++ unset VIRTUAL_ENV
++ unset VIRTUAL_ENV_PROMPT
++ '[' '!' nondestructive = nondestructive ']'
++ VIRTUAL_ENV=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv
++ '[' linux-gnu = cygwin ']'
++ '[' linux-gnu = msys ']'
++ export VIRTUAL_ENV
++ _OLD_VIRTUAL_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH
++ '[' x '!=' x ']'
+++ basename /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv
++ VIRTUAL_ENV_PROMPT=ESP_venv
++ export VIRTUAL_ENV_PROMPT
++ '[' -z _ ']'
++ _OLD_VIRTUAL_PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9
++ unset PYTHONHOME
++ '[' -z '' ']'
++ _OLD_VIRTUAL_PS1=
++ PS1='(ESP_venv) '
++ export PS1
++ alias pydoc
++ true
++ hash -r
+ pip_install pip
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade pip
Requirement already satisfied: pip in ./ESP_venv/lib/python3.11/site-packages (24.0)
+ pip_install f90nml
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade f90nml
Collecting f90nml
  Using cached f90nml-1.4.4-py2.py3-none-any.whl.metadata (6.0 kB)
Using cached f90nml-1.4.4-py2.py3-none-any.whl (32 kB)
Installing collected packages: f90nml
Successfully installed f90nml-1.4.4
+ pip_install numpy
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade numpy
Collecting numpy
  Using cached numpy-1.26.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (61 kB)
Using cached numpy-1.26.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (18.3 MB)
Installing collected packages: numpy
Successfully installed numpy-1.26.4
+ pip_install openmdao
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade openmdao
Collecting openmdao
  Using cached openmdao-3.31.1-py3-none-any.whl
Collecting networkx>=2.0 (from openmdao)
  Using cached networkx-3.3-py3-none-any.whl.metadata (5.1 kB)
Requirement already satisfied: numpy in ./ESP_venv/lib/python3.11/site-packages (from openmdao) (1.26.4)
Collecting scipy (from openmdao)
  Using cached scipy-1.13.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (60 kB)
Collecting requests (from openmdao)
  Using cached requests-2.31.0-py3-none-any.whl.metadata (4.6 kB)
Collecting packaging (from openmdao)
  Using cached packaging-24.0-py3-none-any.whl.metadata (3.2 kB)
Collecting charset-normalizer<4,>=2 (from requests->openmdao)
  Using cached charset_normalizer-3.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (33 kB)
Collecting idna<4,>=2.5 (from requests->openmdao)
  Using cached idna-3.7-py3-none-any.whl.metadata (9.9 kB)
Collecting urllib3<3,>=1.21.1 (from requests->openmdao)
  Using cached urllib3-2.2.1-py3-none-any.whl.metadata (6.4 kB)
Collecting certifi>=2017.4.17 (from requests->openmdao)
  Using cached certifi-2024.2.2-py3-none-any.whl.metadata (2.2 kB)
Using cached networkx-3.3-py3-none-any.whl (1.7 MB)
Using cached packaging-24.0-py3-none-any.whl (53 kB)
Using cached requests-2.31.0-py3-none-any.whl (62 kB)
Using cached scipy-1.13.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (38.6 MB)
Using cached certifi-2024.2.2-py3-none-any.whl (163 kB)
Using cached charset_normalizer-3.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (140 kB)
Using cached idna-3.7-py3-none-any.whl (66 kB)
Using cached urllib3-2.2.1-py3-none-any.whl (121 kB)
Installing collected packages: urllib3, scipy, packaging, networkx, idna, charset-normalizer, certifi, requests, openmdao
Successfully installed certifi-2024.2.2 charset-normalizer-3.3.2 idna-3.7 networkx-3.3 openmdao-3.31.1 packaging-24.0 requests-2.31.0 scipy-1.13.0 urllib3-2.2.1
+ [[ reynolds-centOS7 == *\v\i\g\g\e\n* ]]
+ pip_install cvxopt
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade cvxopt
Collecting cvxopt
  Using cached cvxopt-1.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (1.3 kB)
Using cached cvxopt-1.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (13.6 MB)
Installing collected packages: cvxopt
Successfully installed cvxopt-1.3.2
+ pip_install dill
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade dill
Collecting dill
  Using cached dill-0.3.8-py3-none-any.whl.metadata (10 kB)
Using cached dill-0.3.8-py3-none-any.whl (116 kB)
Installing collected packages: dill
Successfully installed dill-0.3.8
+ pip_install packaging
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade packaging
Requirement already satisfied: packaging in ./ESP_venv/lib/python3.11/site-packages (24.0)
+ pip_install matplotlib
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib
Collecting matplotlib
  Using cached matplotlib-3.8.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (5.8 kB)
Collecting contourpy>=1.0.1 (from matplotlib)
  Using cached contourpy-1.2.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (5.8 kB)
Collecting cycler>=0.10 (from matplotlib)
  Using cached cycler-0.12.1-py3-none-any.whl.metadata (3.8 kB)
Collecting fonttools>=4.22.0 (from matplotlib)
  Using cached fonttools-4.51.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (159 kB)
Collecting kiwisolver>=1.3.1 (from matplotlib)
  Using cached kiwisolver-1.4.5-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (6.4 kB)
Requirement already satisfied: numpy>=1.21 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (1.26.4)
Requirement already satisfied: packaging>=20.0 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (24.0)
Collecting pillow>=8 (from matplotlib)
  Using cached pillow-10.3.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (9.2 kB)
Collecting pyparsing>=2.3.1 (from matplotlib)
  Using cached pyparsing-3.1.2-py3-none-any.whl.metadata (5.1 kB)
Collecting python-dateutil>=2.7 (from matplotlib)
  Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl.metadata (8.4 kB)
Collecting six>=1.5 (from python-dateutil>=2.7->matplotlib)
  Using cached six-1.16.0-py2.py3-none-any.whl.metadata (1.8 kB)
Using cached matplotlib-3.8.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (11.6 MB)
Using cached contourpy-1.2.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (306 kB)
Using cached cycler-0.12.1-py3-none-any.whl (8.3 kB)
Using cached fonttools-4.51.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (4.9 MB)
Using cached kiwisolver-1.4.5-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (1.4 MB)
Using cached pillow-10.3.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (4.4 MB)
Using cached pyparsing-3.1.2-py3-none-any.whl (103 kB)
Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl (229 kB)
Using cached six-1.16.0-py2.py3-none-any.whl (11 kB)
Installing collected packages: six, pyparsing, pillow, kiwisolver, fonttools, cycler, contourpy, python-dateutil, matplotlib
Successfully installed contourpy-1.2.1 cycler-0.12.1 fonttools-4.51.0 kiwisolver-1.4.5 matplotlib-3.8.4 pillow-10.3.0 pyparsing-3.1.2 python-dateutil-2.9.0.post0 six-1.16.0
+ pip_install scipy
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade scipy
Requirement already satisfied: scipy in ./ESP_venv/lib/python3.11/site-packages (1.13.0)
Requirement already satisfied: numpy<2.3,>=1.22.4 in ./ESP_venv/lib/python3.11/site-packages (from scipy) (1.26.4)
+ unset PYTHONINC
+ unset PYTHONLIB
+ unset UDUNITS2_XML_PATH
+ unset ESP_BLOC
+ unset ESP_ROOT
+ unset ESP_ARCH
+ unset AWAVE
+ unset AFLR
+ unset AFLR_ARCH
+ wget --tries=3 https://acdl.mit.edu/ESP/archive/ESPbeta.tgz
--2024-04-28 10:17:01--  https://acdl.mit.edu/ESP/archive/ESPbeta.tgz
Resolving acdl.mit.edu (acdl.mit.edu)... 18.18.33.14
Connecting to acdl.mit.edu (acdl.mit.edu)|18.18.33.14|:443... connected.
HTTP request sent, awaiting response... 200 OK
Length: 268483520 (256M) [application/x-gzip]
Saving to: ‘ESPbeta.tgz’

     0K .......... .......... .......... .......... ..........  0% 23.6M 11s
    50K .......... .......... .......... .......... ..........  0% 43.6M 8s
   100K .......... .......... .......... .......... ..........  0% 9.26M 15s
   150K .......... .......... .......... .......... ..........  0% 13.7M 16s
   200K .......... .......... .......... .......... ..........  0% 25.3M 15s
   250K .......... .......... .......... .......... ..........  0% 18.8M 14s
   300K .......... .......... .......... .......... ..........  0% 13.9M 15s
   350K .......... .......... .......... .......... ..........  0% 19.1M 15s
   400K .......... .......... .......... .......... ..........  0% 24.6M 14s
   450K .......... .......... .......... .......... ..........  0% 42.8M 13s
   500K .......... .......... .......... .......... ..........  0% 82.1M 13s
   550K .......... .......... .......... .......... ..........  0% 62.5M 12s
   600K .......... .......... .......... .......... ..........  0% 47.4M 11s
   650K .......... .......... .......... .......... ..........  0% 53.0M 11s
   700K .......... .......... .......... .......... ..........  0% 15.2M 11s
   750K .......... .......... .......... .......... ..........  0% 19.7M 11s
   800K .......... .......... .......... .......... ..........  0% 11.2M 12s
   850K .......... .......... .......... .......... ..........  0% 16.6M 12s
   900K .......... .......... .......... .......... ..........  0% 18.2M 12s
   950K .......... .......... .......... .......... ..........  0% 15.9M 12s
  1000K .......... .......... .......... .......... ..........  0% 16.6M 13s
  1050K .......... .......... .......... .......... ..........  0% 13.8M 13s
  1100K .......... .......... .......... .......... ..........  0% 9.41M 14s
  1150K .......... .......... .......... .......... ..........  0% 13.0M 14s
  1200K .......... .......... .......... .......... ..........  0% 8.93M 14s
  1250K .......... .......... .......... .......... ..........  0% 12.7M 15s
  1300K .......... .......... .......... .......... ..........  0% 11.2M 15s
  1350K .......... .......... .......... .......... ..........  0% 11.4M 15s
  1400K .......... .......... .......... .......... ..........  0% 12.4M 15s
  1450K .......... .......... .......... .......... ..........  0% 8.86M 16s
  1500K .......... .......... .......... .......... ..........  0% 10.9M 16s
  1550K .......... .......... .......... .......... ..........  0% 12.3M 16s
  1600K .......... .......... .......... .......... ..........  0% 8.46M 17s
  1650K .......... .......... .......... .......... ..........  0% 16.5M 17s
  1700K .......... .......... .......... .......... ..........  0% 7.89M 17s
  1750K .......... .......... .......... .......... ..........  0% 8.60M 17s
  1800K .......... .......... .......... .......... ..........  0% 10.6M 18s
  1850K .......... .......... .......... .......... ..........  0% 19.2M 17s
  1900K .......... .......... .......... .......... ..........  0% 16.7M 17s
  1950K .......... .......... .......... .......... ..........  0% 16.8M 17s
  2000K .......... .......... .......... .......... ..........  0% 15.1M 17s
  2050K .......... .......... .......... .......... ..........  0% 12.6M 17s
  2100K .......... .......... .......... .......... ..........  0% 14.9M 17s
  2150K .......... .......... .......... .......... ..........  0% 14.3M 17s
  2200K .......... .......... .......... .......... ..........  0% 13.2M 17s
  2250K .......... .......... .......... .......... ..........  0% 14.7M 17s
  2300K .......... .......... .......... .......... ..........  0% 15.6M 17s
  2350K .......... .......... .......... .......... ..........  0% 16.2M 17s
  2400K .......... .......... .......... .......... ..........  0% 12.6M 17s
  2450K .......... .......... .......... .......... ..........  0% 9.37M 18s
  2500K .......... .......... .......... .......... ..........  0% 25.9M 17s
  2550K .......... .......... .......... .......... ..........  0% 23.2M 17s
  2600K .......... .......... .......... .......... ..........  1% 15.3M 17s
  2650K .......... .......... .......... .......... ..........  1% 18.7M 17s
  2700K .......... .......... .......... .......... ..........  1% 12.4M 17s
  2750K .......... .......... .......... .......... ..........  1% 14.9M 17s
  2800K .......... .......... .......... .......... ..........  1% 14.3M 17s
  2850K .......... .......... .......... .......... ..........  1% 15.7M 17s
  2900K .......... .......... .......... .......... ..........  1% 14.9M 17s
  2950K .......... .......... .......... .......... ..........  1% 9.83M 17s
  3000K .......... .......... .......... .......... ..........  1% 13.6M 17s
  3050K .......... .......... .......... .......... ..........  1% 12.6M 17s
  3100K .......... .......... .......... .......... ..........  1% 12.5M 17s
  3150K .......... .......... .......... .......... ..........  1% 14.3M 17s
  3200K .......... .......... .......... .......... ..........  1% 10.0M 18s
  3250K .......... .......... .......... .......... ..........  1% 14.1M 18s
  3300K .......... .......... .......... .......... ..........  1% 11.9M 18s
  3350K .......... .......... .......... .......... ..........  1% 9.79M 18s
  3400K .......... .......... .......... .......... ..........  1% 19.4M 18s
  3450K .......... .......... .......... .......... ..........  1% 24.1M 18s
  3500K .......... .......... .......... .......... ..........  1% 28.1M 17s
  3550K .......... .......... .......... .......... ..........  1% 21.2M 17s
  3600K .......... .......... .......... .......... ..........  1% 30.7M 17s
  3650K .......... .......... .......... .......... ..........  1% 18.0M 17s
  3700K .......... .......... .......... .......... ..........  1% 16.8M 17s
  3750K .......... .......... .......... .......... ..........  1% 12.8M 17s
  3800K .......... .......... .......... .......... ..........  1% 16.4M 17s
  3850K .......... .......... .......... .......... ..........  1% 13.5M 17s
  3900K .......... .......... .......... .......... ..........  1% 12.8M 17s
  3950K .......... .......... .......... .......... ..........  1% 12.0M 17s
  4000K .......... .......... .......... .......... ..........  1% 10.5M 17s
  4050K .......... .......... .......... .......... ..........  1% 14.8M 17s
  4100K .......... .......... .......... .......... ..........  1% 11.1M 17s
  4150K .......... .......... .......... .......... ..........  1% 15.5M 17s
  4200K .......... .......... .......... .......... ..........  1% 17.7M 17s
  4250K .......... .......... .......... .......... ..........  1% 11.4M 17s
  4300K .......... .......... .......... .......... ..........  1% 41.0M 17s
  4350K .......... .......... .......... .......... ..........  1% 15.6M 17s
  4400K .......... .......... .......... .......... ..........  1% 16.0M 17s
  4450K .......... .......... .......... .......... ..........  1% 13.7M 17s
  4500K .......... .......... .......... .......... ..........  1% 13.2M 17s
  4550K .......... .......... .......... .......... ..........  1% 18.1M 17s
  4600K .......... .......... .......... .......... ..........  1% 7.60M 17s
  4650K .......... .......... .......... .......... ..........  1% 31.2M 17s
  4700K .......... .......... .......... .......... ..........  1% 16.5M 17s
  4750K .......... .......... .......... .......... ..........  1% 13.8M 17s
  4800K .......... .......... .......... .......... ..........  1% 10.8M 17s
  4850K .......... .......... .......... .......... ..........  1% 24.2M 17s
  4900K .......... .......... .......... .......... ..........  1% 22.1M 17s
  4950K .......... .......... .......... .......... ..........  1% 19.4M 17s
  5000K .......... .......... .......... .......... ..........  1% 11.6M 17s
  5050K .......... .......... .......... .......... ..........  1% 19.0M 17s
  5100K .......... .......... .......... .......... ..........  1% 16.6M 17s
  5150K .......... .......... .......... .......... ..........  1% 20.4M 17s
  5200K .......... .......... .......... .......... ..........  2% 12.2M 17s
  5250K .......... .......... .......... .......... ..........  2% 19.4M 17s
  5300K .......... .......... .......... .......... ..........  2% 14.4M 17s
  5350K .......... .......... .......... .......... ..........  2% 16.5M 17s
  5400K .......... .......... .......... .......... ..........  2% 16.1M 17s
  5450K .......... .......... .......... .......... ..........  2% 13.4M 17s
  5500K .......... .......... .......... .......... ..........  2% 15.6M 17s
  5550K .......... .......... .......... .......... ..........  2% 13.5M 17s
  5600K .......... .......... .......... .......... ..........  2% 15.3M 17s
  5650K .......... .......... .......... .......... ..........  2% 13.9M 17s
  5700K .......... .......... .......... .......... ..........  2% 9.30M 17s
  5750K .......... .......... .......... .......... ..........  2% 18.5M 17s
  5800K .......... .......... .......... .......... ..........  2% 18.3M 17s
  5850K .......... .......... .......... .......... ..........  2% 13.9M 17s
  5900K .......... .......... .......... .......... ..........  2% 16.5M 17s
  5950K .......... .......... .......... .......... ..........  2% 19.5M 17s
  6000K .......... .......... .......... .......... ..........  2% 20.0M 17s
  6050K .......... .......... .......... .......... ..........  2% 15.0M 17s
  6100K .......... .......... .......... .......... ..........  2% 15.0M 17s
  6150K .......... .......... .......... .......... ..........  2% 22.7M 17s
  6200K .......... .......... .......... .......... ..........  2% 14.8M 17s
  6250K .......... .......... .......... .......... ..........  2% 27.8M 17s
  6300K .......... .......... .......... .......... ..........  2% 21.3M 17s
  6350K .......... .......... .......... .......... ..........  2% 19.7M 17s
  6400K .......... .......... .......... .......... ..........  2% 22.8M 17s
  6450K .......... .......... .......... .......... ..........  2% 25.0M 17s
  6500K .......... .......... .......... .......... ..........  2% 24.8M 17s
  6550K .......... .......... .......... .......... ..........  2% 15.2M 17s
  6600K .......... .......... .......... .......... ..........  2% 15.6M 17s
  6650K .......... .......... .......... .......... ..........  2% 19.6M 17s
  6700K .......... .......... .......... .......... ..........  2% 12.7M 17s
  6750K .......... .......... .......... .......... ..........  2% 18.5M 17s
  6800K .......... .......... .......... .......... ..........  2% 20.2M 16s
  6850K .......... .......... .......... .......... ..........  2% 26.3M 16s
  6900K .......... .......... .......... .......... ..........  2% 22.4M 16s
  6950K .......... .......... .......... .......... ..........  2% 19.1M 16s
  7000K .......... .......... .......... .......... ..........  2% 15.7M 16s
  7050K .......... .......... .......... .......... ..........  2% 13.8M 16s
  7100K .......... .......... .......... .......... ..........  2% 10.7M 16s
  7150K .......... .......... .......... .......... ..........  2% 15.5M 16s
  7200K .......... .......... .......... .......... ..........  2% 13.0M 16s
  7250K .......... .......... .......... .......... ..........  2% 20.5M 16s
  7300K .......... .......... .......... .......... ..........  2% 15.3M 16s
  7350K .......... .......... .......... .......... ..........  2% 16.0M 16s
  7400K .......... .......... .......... .......... ..........  2% 18.0M 16s
  7450K .......... .......... .......... .......... ..........  2% 14.4M 16s
  7500K .......... .......... .......... .......... ..........  2% 17.7M 16s
  7550K .......... .......... .......... .......... ..........  2% 14.0M 16s
  7600K .......... .......... .......... .......... ..........  2% 14.8M 16s
  7650K .......... .......... .......... .......... ..........  2% 11.1M 16s
  7700K .......... .......... .......... .......... ..........  2% 8.34M 16s
  7750K .......... .......... .......... .......... ..........  2% 19.9M 16s
  7800K .......... .......... .......... .......... ..........  2% 21.9M 16s
  7850K .......... .......... .......... .......... ..........  3% 18.0M 16s
  7900K .......... .......... .......... .......... ..........  3% 19.8M 16s
  7950K .......... .......... .......... .......... ..........  3% 17.1M 16s
  8000K .......... .......... .......... .......... ..........  3% 13.7M 16s
  8050K .......... .......... .......... .......... ..........  3% 15.7M 16s
  8100K .......... .......... .......... .......... ..........  3% 9.80M 16s
  8150K .......... .......... .......... .......... ..........  3% 12.0M 16s
  8200K .......... .......... .......... .......... ..........  3% 12.5M 16s
  8250K .......... .......... .......... .......... ..........  3% 14.3M 16s
  8300K .......... .......... .......... .......... ..........  3% 15.9M 16s
  8350K .......... .......... .......... .......... ..........  3% 13.0M 16s
  8400K .......... .......... .......... .......... ..........  3% 15.4M 16s
  8450K .......... .......... .......... .......... ..........  3% 10.8M 16s
  8500K .......... .......... .......... .......... ..........  3% 9.71M 17s
  8550K .......... .......... .......... .......... ..........  3% 16.4M 16s
  8600K .......... .......... .......... .......... ..........  3% 15.4M 16s
  8650K .......... .......... .......... .......... ..........  3% 16.4M 16s
  8700K .......... .......... .......... .......... ..........  3% 13.5M 16s
  8750K .......... .......... .......... .......... ..........  3% 18.8M 16s
  8800K .......... .......... .......... .......... ..........  3% 21.2M 16s
  8850K .......... .......... .......... .......... ..........  3% 19.8M 16s
  8900K .......... .......... .......... .......... ..........  3% 17.1M 16s
  8950K .......... .......... .......... .......... ..........  3% 14.8M 16s
  9000K .......... .......... .......... .......... ..........  3% 29.1M 16s
  9050K .......... .......... .......... .......... ..........  3% 14.2M 16s
  9100K .......... .......... .......... .......... ..........  3% 14.4M 16s
  9150K .......... .......... .......... .......... ..........  3% 23.7M 16s
  9200K .......... .......... .......... .......... ..........  3% 13.4M 16s
  9250K .......... .......... .......... .......... ..........  3% 15.8M 16s
  9300K .......... .......... .......... .......... ..........  3% 18.7M 16s
  9350K .......... .......... .......... .......... ..........  3% 12.9M 16s
  9400K .......... .......... .......... .......... ..........  3% 18.6M 16s
  9450K .......... .......... .......... .......... ..........  3% 15.5M 16s
  9500K .......... .......... .......... .......... ..........  3% 15.7M 16s
  9550K .......... .......... .......... .......... ..........  3% 8.83M 16s
  9600K .......... .......... .......... .......... ..........  3% 8.37M 16s
  9650K .......... .......... .......... .......... ..........  3% 7.14M 16s
  9700K .......... .......... .......... .......... ..........  3%  160M 16s
  9750K .......... .......... .......... .......... ..........  3% 44.0M 16s
  9800K .......... .......... .......... .......... ..........  3% 18.4M 16s
  9850K .......... .......... .......... .......... ..........  3% 38.3M 16s
  9900K .......... .......... .......... .......... ..........  3% 28.0M 16s
  9950K .......... .......... .......... .......... ..........  3% 17.8M 16s
 10000K .......... .......... .......... .......... ..........  3% 12.6M 16s
 10050K .......... .......... .......... .......... ..........  3% 24.2M 16s
 10100K .......... .......... .......... .......... ..........  3% 10.8M 16s
 10150K .......... .......... .......... .......... ..........  3% 12.6M 16s
 10200K .......... .......... .......... .......... ..........  3% 9.01M 16s
 10250K .......... .......... .......... .......... ..........  3% 11.1M 16s
 10300K .......... .......... .......... .......... ..........  3% 10.3M 16s
 10350K .......... .......... .......... .......... ..........  3% 6.89M 16s
 10400K .......... .......... .......... .......... ..........  3% 7.71M 17s
 10450K .......... .......... .......... .......... ..........  4% 3.90M 17s
 10500K .......... .......... .......... .......... ..........  4%  887K 18s
 10550K .......... .......... .......... .......... ..........  4% 4.03M 18s
 10600K .......... .......... .......... .......... ..........  4% 1.82M 19s
 10650K .......... .......... .......... .......... ..........  4% 4.11M 19s
 10700K .......... .......... .......... .......... ..........  4% 3.61M 19s
 10750K .......... .......... .......... .......... ..........  4% 3.73M 19s
 10800K .......... .......... .......... .......... ..........  4% 3.33M 20s
 10850K .......... .......... .......... .......... ..........  4% 1.97M 20s
 10900K .......... .......... .......... .......... ..........  4% 10.6M 20s
 10950K .......... .......... .......... .......... ..........  4% 7.71M 20s
 11000K .......... .......... .......... .......... ..........  4% 10.3M 20s
 11050K .......... .......... .......... .......... ..........  4% 7.29M 20s
 11100K .......... .......... .......... .......... ..........  4% 6.31M 20s
 11150K .......... .......... .......... .......... ..........  4% 5.12M 20s
 11200K .......... .......... .......... .......... ..........  4% 8.42M 20s
 11250K .......... .......... .......... .......... ..........  4% 8.11M 20s
 11300K .......... .......... .......... .......... ..........  4% 13.3M 20s
 11350K .......... .......... .......... .......... ..........  4% 13.8M 20s
 11400K .......... .......... .......... .......... ..........  4% 19.9M 20s
 11450K .......... .......... .......... .......... ..........  4% 14.0M 20s
 11500K .......... .......... .......... .......... ..........  4% 20.3M 20s
 11550K .......... .......... .......... .......... ..........  4% 16.8M 20s
 11600K .......... .......... .......... .......... ..........  4% 17.6M 20s
 11650K .......... .......... .......... .......... ..........  4% 21.4M 20s
 11700K .......... .......... .......... .......... ..........  4% 15.9M 20s
 11750K .......... .......... .......... .......... ..........  4% 13.5M 20s
 11800K .......... .......... .......... .......... ..........  4% 19.0M 20s
 11850K .......... .......... .......... .......... ..........  4% 14.2M 20s
 11900K .......... .......... .......... .......... ..........  4% 12.0M 20s
 11950K .......... .......... .......... .......... ..........  4% 15.0M 20s
 12000K .......... .......... .......... .......... ..........  4% 19.7M 20s
 12050K .......... .......... .......... .......... ..........  4% 8.62M 20s
 12100K .......... .......... .......... .......... ..........  4% 10.8M 20s
 12150K .......... .......... .......... .......... ..........  4% 5.50M 20s
 12200K .......... .......... .......... .......... ..........  4% 4.61M 20s
 12250K .......... .......... .......... .......... ..........  4% 6.47M 20s
 12300K .......... .......... .......... .......... ..........  4% 5.24M 21s
 12350K .......... .......... .......... .......... ..........  4% 5.74M 21s
 12400K .......... .......... .......... .......... ..........  4% 8.13M 21s
 12450K .......... .......... .......... .......... ..........  4% 6.47M 21s
 12500K .......... .......... .......... .......... ..........  4% 13.8M 21s
 12550K .......... .......... .......... .......... ..........  4% 76.7M 21s
 12600K .......... .......... .......... .......... ..........  4% 15.2M 21s
 12650K .......... .......... .......... .......... ..........  4% 24.2M 21s
 12700K .......... .......... .......... .......... ..........  4% 11.5M 21s
 12750K .......... .......... .......... .......... ..........  4% 18.4M 21s
 12800K .......... .......... .......... .......... ..........  4% 17.4M 21s
 12850K .......... .......... .......... .......... ..........  4% 17.1M 20s
 12900K .......... .......... .......... .......... ..........  4% 27.4M 20s
 12950K .......... .......... .......... .......... ..........  4% 19.8M 20s
 13000K .......... .......... .......... .......... ..........  4% 19.7M 20s
 13050K .......... .......... .......... .......... ..........  4% 15.3M 20s
 13100K .......... .......... .......... .......... ..........  5% 9.27M 20s
 13150K .......... .......... .......... .......... ..........  5% 8.00M 20s
 13200K .......... .......... .......... .......... ..........  5% 9.34M 20s
 13250K .......... .......... .......... .......... ..........  5% 10.1M 20s
 13300K .......... .......... .......... .......... ..........  5% 10.3M 20s
 13350K .......... .......... .......... .......... ..........  5% 7.19M 20s
 13400K .......... .......... .......... .......... ..........  5% 8.22M 20s
 13450K .......... .......... .......... .......... ..........  5% 4.86M 21s
 13500K .......... .......... .......... .......... ..........  5% 5.17M 21s
 13550K .......... .......... .......... .......... ..........  5% 8.48M 21s
 13600K .......... .......... .......... .......... ..........  5% 6.99M 21s
 13650K .......... .......... .......... .......... ..........  5% 6.70M 21s
 13700K .......... .......... .......... .......... ..........  5% 6.43M 21s
 13750K .......... .......... .......... .......... ..........  5% 9.73M 21s
 13800K .......... .......... .......... .......... ..........  5% 8.28M 21s
 13850K .......... .......... .......... .......... ..........  5% 8.51M 21s
 13900K .......... .......... .......... .......... ..........  5% 6.36M 21s
 13950K .......... .......... .......... .......... ..........  5% 17.2M 21s
 14000K .......... .......... .......... .......... ..........  5% 17.5M 21s
 14050K .......... .......... .......... .......... ..........  5% 13.8M 21s
 14100K .......... .......... .......... .......... ..........  5% 8.12M 21s
 14150K .......... .......... .......... .......... ..........  5% 9.63M 21s
 14200K .......... .......... .......... .......... ..........  5% 6.64M 21s
 14250K .......... .......... .......... .......... ..........  5% 7.68M 21s
 14300K .......... .......... .......... .......... ..........  5% 10.4M 21s
 14350K .......... .......... .......... .......... ..........  5% 8.56M 21s
 14400K .......... .......... .......... .......... ..........  5% 8.02M 21s
 14450K .......... .......... .......... .......... ..........  5% 8.19M 21s
 14500K .......... .......... .......... .......... ..........  5% 11.5M 21s
 14550K .......... .......... .......... .......... ..........  5% 10.2M 21s
 14600K .......... .......... .......... .......... ..........  5% 12.6M 21s
 14650K .......... .......... .......... .......... ..........  5% 12.7M 21s
 14700K .......... .......... .......... .......... ..........  5% 14.1M 21s
 14750K .......... .......... .......... .......... ..........  5% 41.0M 21s
 14800K .......... .......... .......... .......... ..........  5% 16.0M 21s
 14850K .......... .......... .......... .......... ..........  5% 12.9M 21s
 14900K .......... .......... .......... .......... ..........  5% 11.5M 21s
 14950K .......... .......... .......... .......... ..........  5% 10.8M 21s
 15000K .......... .......... .......... .......... ..........  5% 10.6M 21s
 15050K .......... .......... .......... .......... ..........  5% 12.5M 21s
 15100K .......... .......... .......... .......... ..........  5% 5.90M 21s
 15150K .......... .......... .......... .......... ..........  5% 6.84M 21s
 15200K .......... .......... .......... .......... ..........  5% 4.62M 21s
 15250K .......... .......... .......... .......... ..........  5% 11.9M 21s
 15300K .......... .......... .......... .......... ..........  5% 8.82M 21s
 15350K .......... .......... .......... .......... ..........  5% 7.85M 21s
 15400K .......... .......... .......... .......... ..........  5% 9.12M 21s
 15450K .......... .......... .......... .......... ..........  5% 7.49M 21s
 15500K .......... .......... .......... .......... ..........  5% 9.15M 21s
 15550K .......... .......... .......... .......... ..........  5% 10.1M 21s
 15600K .......... .......... .......... .......... ..........  5% 7.46M 21s
 15650K .......... .......... .......... .......... ..........  5% 8.60M 21s
 15700K .......... .......... .......... .......... ..........  6% 4.49M 21s
 15750K .......... .......... .......... .......... ..........  6% 5.97M 21s
 15800K .......... .......... .......... .......... ..........  6% 4.30M 22s
 15850K .......... .......... .......... .......... ..........  6% 5.86M 22s
 15900K .......... .......... .......... .......... ..........  6% 7.13M 22s
 15950K .......... .......... .......... .......... ..........  6% 13.8M 22s
 16000K .......... .......... .......... .......... ..........  6% 9.82M 22s
 16050K .......... .......... .......... .......... ..........  6% 11.0M 22s
 16100K .......... .......... .......... .......... ..........  6% 7.63M 22s
 16150K .......... .......... .......... .......... ..........  6% 12.0M 22s
 16200K .......... .......... .......... .......... ..........  6% 11.9M 22s
 16250K .......... .......... .......... .......... ..........  6% 8.47M 22s
 16300K .......... .......... .......... .......... ..........  6% 14.7M 22s
 16350K .......... .......... .......... .......... ..........  6% 6.65M 22s
 16400K .......... .......... .......... .......... ..........  6% 8.13M 22s
 16450K .......... .......... .......... .......... ..........  6% 5.30M 22s
 16500K .......... .......... .......... .......... ..........  6% 6.72M 22s
 16550K .......... .......... .......... .......... ..........  6% 6.33M 22s
 16600K .......... .......... .......... .......... ..........  6% 9.89M 22s
 16650K .......... .......... .......... .......... ..........  6% 10.0M 22s
 16700K .......... .......... .......... .......... ..........  6% 7.29M 22s
 16750K .......... .......... .......... .......... ..........  6% 17.5M 22s
 16800K .......... .......... .......... .......... ..........  6% 22.7M 22s
 16850K .......... .......... .......... .......... ..........  6% 25.2M 22s
 16900K .......... .......... .......... .......... ..........  6% 16.2M 22s
 16950K .......... .......... .......... .......... ..........  6% 26.7M 22s
 17000K .......... .......... .......... .......... ..........  6% 18.2M 22s
 17050K .......... .......... .......... .......... ..........  6% 18.3M 22s
 17100K .......... .......... .......... .......... ..........  6% 14.2M 22s
 17150K .......... .......... .......... .......... ..........  6% 18.9M 22s
 17200K .......... .......... .......... .......... ..........  6% 18.3M 22s
 17250K .......... .......... .......... .......... ..........  6% 10.2M 22s
 17300K .......... .......... .......... .......... ..........  6% 15.5M 22s
 17350K .......... .......... .......... .......... ..........  6% 10.0M 22s
 17400K .......... .......... .......... .......... ..........  6% 14.6M 22s
 17450K .......... .......... .......... .......... ..........  6% 19.4M 22s
 17500K .......... .......... .......... .......... ..........  6% 19.9M 21s
 17550K .......... .......... .......... .......... ..........  6% 16.5M 21s
 17600K .......... .......... .......... .......... ..........  6% 12.7M 21s
 17650K .......... .......... .......... .......... ..........  6% 11.9M 21s
 17700K .......... .......... .......... .......... ..........  6% 12.3M 21s
 17750K .......... .......... .......... .......... ..........  6% 12.2M 21s
 17800K .......... .......... .......... .......... ..........  6% 9.12M 21s
 17850K .......... .......... .......... .......... ..........  6% 6.01M 21s
 17900K .......... .......... .......... .......... ..........  6% 6.42M 22s
 17950K .......... .......... .......... .......... ..........  6% 3.67M 22s
 18000K .......... .......... .......... .......... ..........  6% 4.59M 22s
 18050K .......... .......... .......... .......... ..........  6% 19.1M 22s
 18100K .......... .......... .......... .......... ..........  6% 29.1M 22s
 18150K .......... .......... .......... .......... ..........  6% 14.3M 22s
 18200K .......... .......... .......... .......... ..........  6% 48.6M 22s
 18250K .......... .......... .......... .......... ..........  6% 21.5M 22s
 18300K .......... .......... .......... .......... ..........  6% 14.3M 22s
 18350K .......... .......... .......... .......... ..........  7% 27.0M 21s
 18400K .......... .......... .......... .......... ..........  7% 15.2M 21s
 18450K .......... .......... .......... .......... ..........  7% 19.5M 21s
 18500K .......... .......... .......... .......... ..........  7% 13.1M 21s
 18550K .......... .......... .......... .......... ..........  7% 7.47M 21s
 18600K .......... .......... .......... .......... ..........  7% 3.98M 22s
 18650K .......... .......... .......... .......... ..........  7% 4.71M 22s
 18700K .......... .......... .......... .......... ..........  7% 1.53M 22s
 18750K .......... .......... .......... .......... ..........  7% 3.56M 22s
 18800K .......... .......... .......... .......... ..........  7% 2.52M 22s
 18850K .......... .......... .......... .......... ..........  7% 6.14M 22s
 18900K .......... .......... .......... .......... ..........  7% 12.0M 22s
 18950K .......... .......... .......... .......... ..........  7% 26.7M 22s
 19000K .......... .......... .......... .......... ..........  7% 12.6M 22s
 19050K .......... .......... .......... .......... ..........  7% 9.66M 22s
 19100K .......... .......... .......... .......... ..........  7% 12.0M 22s
 19150K .......... .......... .......... .......... ..........  7% 11.4M 22s
 19200K .......... .......... .......... .......... ..........  7% 11.6M 22s
 19250K .......... .......... .......... .......... ..........  7% 6.79M 22s
 19300K .......... .......... .......... .......... ..........  7% 35.4M 22s
 19350K .......... .......... .......... .......... ..........  7% 13.5M 22s
 19400K .......... .......... .......... .......... ..........  7% 31.0M 22s
 19450K .......... .......... .......... .......... ..........  7% 10.1M 22s
 19500K .......... .......... .......... .......... ..........  7% 11.2M 22s
 19550K .......... .......... .......... .......... ..........  7% 8.17M 22s
 19600K .......... .......... .......... .......... ..........  7% 6.79M 22s
 19650K .......... .......... .......... .......... ..........  7% 7.45M 22s
 19700K .......... .......... .......... .......... ..........  7% 4.54M 22s
 19750K .......... .......... .......... .......... ..........  7% 10.4M 22s
 19800K .......... .......... .......... .......... ..........  7% 9.54M 22s
 19850K .......... .......... .......... .......... ..........  7% 6.32M 22s
 19900K .......... .......... .......... .......... ..........  7% 10.9M 22s
 19950K .......... .......... .......... .......... ..........  7% 11.0M 22s
 20000K .......... .......... .......... .......... ..........  7% 18.4M 22s
 20050K .......... .......... .......... .......... ..........  7% 47.0M 22s
 20100K .......... .......... .......... .......... ..........  7% 10.7M 22s
 20150K .......... .......... .......... .......... ..........  7%  101M 22s
 20200K .......... .......... .......... .......... ..........  7% 36.9M 22s
 20250K .......... .......... .......... .......... ..........  7% 10.7M 22s
 20300K .......... .......... .......... .......... ..........  7% 23.7M 22s
 20350K .......... .......... .......... .......... ..........  7% 13.8M 22s
 20400K .......... .......... .......... .......... ..........  7% 14.2M 22s
 20450K .......... .......... .......... .......... ..........  7% 9.39M 22s
 20500K .......... .......... .......... .......... ..........  7% 13.0M 22s
 20550K .......... .......... .......... .......... ..........  7% 7.24M 22s
 20600K .......... .......... .......... .......... ..........  7% 7.86M 22s
 20650K .......... .......... .......... .......... ..........  7% 4.25M 22s
 20700K .......... .......... .......... .......... ..........  7% 4.02M 22s
 20750K .......... .......... .......... .......... ..........  7% 4.64M 22s
 20800K .......... .......... .......... .......... ..........  7% 4.32M 22s
 20850K .......... .......... .......... .......... ..........  7% 3.62M 22s
 20900K .......... .......... .......... .......... ..........  7% 4.20M 23s
 20950K .......... .......... .......... .......... ..........  8% 1.59M 23s
 21000K .......... .......... .......... .......... ..........  8% 3.40M 23s
 21050K .......... .......... .......... .......... ..........  8% 6.40M 23s
 21100K .......... .......... .......... .......... ..........  8% 6.49M 23s
 21150K .......... .......... .......... .......... ..........  8% 9.50M 23s
 21200K .......... .......... .......... .......... ..........  8% 5.78M 23s
 21250K .......... .......... .......... .......... ..........  8% 8.85M 23s
 21300K .......... .......... .......... .......... ..........  8% 7.57M 23s
 21350K .......... .......... .......... .......... ..........  8% 7.12M 23s
 21400K .......... .......... .......... .......... ..........  8% 19.9M 23s
 21450K .......... .......... .......... .......... ..........  8% 14.9M 23s
 21500K .......... .......... .......... .......... ..........  8% 14.6M 23s
 21550K .......... .......... .......... .......... ..........  8% 22.4M 23s
 21600K .......... .......... .......... .......... ..........  8% 12.8M 23s
 21650K .......... .......... .......... .......... ..........  8% 16.0M 23s
 21700K .......... .......... .......... .......... ..........  8% 12.8M 23s
 21750K .......... .......... .......... .......... ..........  8% 18.5M 23s
 21800K .......... .......... .......... .......... ..........  8% 10.2M 23s
 21850K .......... .......... .......... .......... ..........  8% 8.95M 23s
 21900K .......... .......... .......... .......... ..........  8% 9.87M 23s
 21950K .......... .......... .......... .......... ..........  8% 8.34M 23s
 22000K .......... .......... .......... .......... ..........  8% 7.99M 23s
 22050K .......... .......... .......... .......... ..........  8% 6.66M 23s
 22100K .......... .......... .......... .......... ..........  8% 4.68M 23s
 22150K .......... .......... .......... .......... ..........  8% 3.88M 23s
 22200K .......... .......... .......... .......... ..........  8% 3.80M 23s
 22250K .......... .......... .......... .......... ..........  8% 3.02M 23s
 22300K .......... .......... .......... .......... ..........  8% 2.18M 23s
 22350K .......... .......... .......... .......... ..........  8% 1.22M 24s
 22400K .......... .......... .......... .......... ..........  8% 3.45M 24s
 22450K .......... .......... .......... .......... ..........  8% 1.47M 24s
 22500K .......... .......... .......... .......... ..........  8% 2.42M 24s
 22550K .......... .......... .......... .......... ..........  8% 7.71M 24s
 22600K .......... .......... .......... .......... ..........  8% 5.64M 24s
 22650K .......... .......... .......... .......... ..........  8% 6.49M 24s
 22700K .......... .......... .......... .......... ..........  8% 5.94M 24s
 22750K .......... .......... .......... .......... ..........  8% 6.55M 24s
 22800K .......... .......... .......... .......... ..........  8% 10.4M 24s
 22850K .......... .......... .......... .......... ..........  8% 10.5M 24s
 22900K .......... .......... .......... .......... ..........  8% 21.7M 24s
 22950K .......... .......... .......... .......... ..........  8% 10.5M 24s
 23000K .......... .......... .......... .......... ..........  8% 10.5M 24s
 23050K .......... .......... .......... .......... ..........  8% 7.12M 24s
 23100K .......... .......... .......... .......... ..........  8% 7.79M 24s
 23150K .......... .......... .......... .......... ..........  8% 7.97M 24s
 23200K .......... .......... .......... .......... ..........  8% 7.96M 24s
 23250K .......... .......... .......... .......... ..........  8% 8.61M 24s
 23300K .......... .......... .......... .......... ..........  8% 11.6M 24s
 23350K .......... .......... .......... .......... ..........  8% 7.02M 24s
 23400K .......... .......... .......... .......... ..........  8% 18.7M 24s
 23450K .......... .......... .......... .......... ..........  8% 13.4M 24s
 23500K .......... .......... .......... .......... ..........  8% 29.3M 24s
 23550K .......... .......... .......... .......... ..........  9% 10.3M 24s
 23600K .......... .......... .......... .......... ..........  9% 34.5M 24s
 23650K .......... .......... .......... .......... ..........  9% 9.26M 24s
 23700K .......... .......... .......... .......... ..........  9% 8.00M 24s
 23750K .......... .......... .......... .......... ..........  9% 10.2M 24s
 23800K .......... .......... .......... .......... ..........  9% 8.83M 24s
 23850K .......... .......... .......... .......... ..........  9% 8.66M 24s
 23900K .......... .......... .......... .......... ..........  9% 8.24M 24s
 23950K .......... .......... .......... .......... ..........  9% 6.76M 24s
 24000K .......... .......... .......... .......... ..........  9% 6.52M 24s
 24050K .......... .......... .......... .......... ..........  9% 19.2M 24s
 24100K .......... .......... .......... .......... ..........  9% 8.45M 24s
 24150K .......... .......... .......... .......... ..........  9% 8.21M 24s
 24200K .......... .......... .......... .......... ..........  9% 8.60M 24s
 24250K .......... .......... .......... .......... ..........  9% 10.9M 24s
 24300K .......... .......... .......... .......... ..........  9% 8.31M 24s
 24350K .......... .......... .......... .......... ..........  9% 6.78M 24s
 24400K .......... .......... .......... .......... ..........  9% 9.10M 24s
 24450K .......... .......... .......... .......... ..........  9% 11.1M 24s
 24500K .......... .......... .......... .......... ..........  9% 11.4M 24s
 24550K .......... .......... .......... .......... ..........  9% 9.15M 24s
 24600K .......... .......... .......... .......... ..........  9% 5.93M 24s
 24650K .......... .......... .......... .......... ..........  9% 5.73M 24s
 24700K .......... .......... .......... .......... ..........  9% 5.49M 24s
 24750K .......... .......... .......... .......... ..........  9% 6.29M 24s
 24800K .......... .......... .......... .......... ..........  9% 7.68M 24s
 24850K .......... .......... .......... .......... ..........  9% 6.09M 24s
 24900K .......... .......... .......... .......... ..........  9% 9.44M 24s
 24950K .......... .......... .......... .......... ..........  9% 7.98M 24s
 25000K .......... .......... .......... .......... ..........  9% 8.21M 24s
 25050K .......... .......... .......... .......... ..........  9% 6.88M 24s
 25100K .......... .......... .......... .......... ..........  9% 5.78M 24s
 25150K .......... .......... .......... .......... ..........  9% 6.51M 24s
 25200K .......... .......... .......... .......... ..........  9% 5.44M 24s
 25250K .......... .......... .......... .......... ..........  9% 6.62M 24s
 25300K .......... .......... .......... .......... ..........  9% 6.02M 25s
 25350K .......... .......... .......... .......... ..........  9% 4.63M 25s
 25400K .......... .......... .......... .......... ..........  9% 6.06M 25s
 25450K .......... .......... .......... .......... ..........  9% 4.80M 25s
 25500K .......... .......... .......... .......... ..........  9% 4.78M 25s
 25550K .......... .......... .......... .......... ..........  9% 4.09M 25s
 25600K .......... .......... .......... .......... ..........  9% 1.24M 25s
 25650K .......... .......... .......... .......... ..........  9% 2.60M 25s
 25700K .......... .......... .......... .......... ..........  9% 4.55M 25s
 25750K .......... .......... .......... .......... ..........  9% 14.7M 25s
 25800K .......... .......... .......... .......... ..........  9% 21.4M 25s
 25850K .......... .......... .......... .......... ..........  9% 11.4M 25s
 25900K .......... .......... .......... .......... ..........  9% 60.5M 25s
 25950K .......... .......... .......... .......... ..........  9% 9.56M 25s
 26000K .......... .......... .......... .......... ..........  9% 18.3M 25s
 26050K .......... .......... .......... .......... ..........  9% 11.4M 25s
 26100K .......... .......... .......... .......... ..........  9% 9.21M 25s
 26150K .......... .......... .......... .......... ..........  9% 6.68M 25s
 26200K .......... .......... .......... .......... .......... 10% 6.80M 25s
 26250K .......... .......... .......... .......... .......... 10% 9.46M 25s
 26300K .......... .......... .......... .......... .......... 10% 6.11M 25s
 26350K .......... .......... .......... .......... .......... 10% 5.65M 25s
 26400K .......... .......... .......... .......... .......... 10% 8.99M 25s
 26450K .......... .......... .......... .......... .......... 10% 4.73M 25s
 26500K .......... .......... .......... .......... .......... 10% 4.63M 25s
 26550K .......... .......... .......... .......... .......... 10% 4.97M 25s
 26600K .......... .......... .......... .......... .......... 10% 4.42M 25s
 26650K .......... .......... .......... .......... .......... 10% 5.93M 25s
 26700K .......... .......... .......... .......... .......... 10% 5.24M 25s
 26750K .......... .......... .......... .......... .......... 10% 7.26M 25s
 26800K .......... .......... .......... .......... .......... 10% 8.29M 25s
 26850K .......... .......... .......... .......... .......... 10% 4.80M 25s
 26900K .......... .......... .......... .......... .......... 10% 9.08M 25s
 26950K .......... .......... .......... .......... .......... 10% 5.21M 25s
 27000K .......... .......... .......... .......... .......... 10% 6.75M 25s
 27050K .......... .......... .......... .......... .......... 10% 4.72M 25s
 27100K .......... .......... .......... .......... .......... 10% 3.16M 25s
 27150K .......... .......... .......... .......... .......... 10% 3.54M 26s
 27200K .......... .......... .......... .......... .......... 10% 3.33M 26s
 27250K .......... .......... .......... .......... .......... 10% 9.12M 26s
 27300K .......... .......... .......... .......... .......... 10% 12.0M 26s
 27350K .......... .......... .......... .......... .......... 10% 10.5M 26s
 27400K .......... .......... .......... .......... .......... 10% 12.4M 26s
 27450K .......... .......... .......... .......... .......... 10% 9.95M 26s
 27500K .......... .......... .......... .......... .......... 10% 8.34M 26s
 27550K .......... .......... .......... .......... .......... 10% 6.77M 26s
 27600K .......... .......... .......... .......... .......... 10% 5.03M 26s
 27650K .......... .......... .......... .......... .......... 10% 5.18M 26s
 27700K .......... .......... .......... .......... .......... 10% 3.97M 26s
 27750K .......... .......... .......... .......... .......... 10% 4.16M 26s
 27800K .......... .......... .......... .......... .......... 10% 4.52M 26s
 27850K .......... .......... .......... .......... .......... 10% 2.90M 26s
 27900K .......... .......... .......... .......... .......... 10% 5.83M 26s
 27950K .......... .......... .......... .......... .......... 10% 4.48M 26s
 28000K .......... .......... .......... .......... .......... 10% 5.56M 26s
 28050K .......... .......... .......... .......... .......... 10% 7.14M 26s
 28100K .......... .......... .......... .......... .......... 10% 5.57M 26s
 28150K .......... .......... .......... .......... .......... 10% 24.2M 26s
 28200K .......... .......... .......... .......... .......... 10% 8.72M 26s
 28250K .......... .......... .......... .......... .......... 10% 9.21M 26s
 28300K .......... .......... .......... .......... .......... 10% 14.9M 26s
 28350K .......... .......... .......... .......... .......... 10% 6.90M 26s
 28400K .......... .......... .......... .......... .......... 10% 9.61M 26s
 28450K .......... .......... .......... .......... .......... 10% 8.77M 26s
 28500K .......... .......... .......... .......... .......... 10% 6.61M 26s
 28550K .......... .......... .......... .......... .......... 10% 7.62M 26s
 28600K .......... .......... .......... .......... .......... 10% 5.76M 26s
 28650K .......... .......... .......... .......... .......... 10% 7.82M 26s
 28700K .......... .......... .......... .......... .......... 10% 5.79M 26s
 28750K .......... .......... .......... .......... .......... 10% 6.84M 26s
 28800K .......... .......... .......... .......... .......... 11% 6.59M 26s
 28850K .......... .......... .......... .......... .......... 11% 5.58M 26s
 28900K .......... .......... .......... .......... .......... 11% 13.5M 26s
 28950K .......... .......... .......... .......... .......... 11% 4.72M 26s
 29000K .......... .......... .......... .......... .......... 11% 4.37M 26s
 29050K .......... .......... .......... .......... .......... 11% 4.02M 26s
 29100K .......... .......... .......... .......... .......... 11% 3.75M 26s
 29150K .......... .......... .......... .......... .......... 11% 3.70M 26s
 29200K .......... .......... .......... .......... .......... 11% 2.28M 26s
 29250K .......... .......... .......... .......... .......... 11% 2.01M 26s
 29300K .......... .......... .......... .......... .......... 11% 4.85M 26s
 29350K .......... .......... .......... .......... .......... 11% 12.6M 26s
 29400K .......... .......... .......... .......... .......... 11% 15.7M 26s
 29450K .......... .......... .......... .......... .......... 11% 32.1M 26s
 29500K .......... .......... .......... .......... .......... 11% 16.7M 26s
 29550K .......... .......... .......... .......... .......... 11% 16.9M 26s
 29600K .......... .......... .......... .......... .......... 11% 17.5M 26s
 29650K .......... .......... .......... .......... .......... 11% 13.9M 26s
 29700K .......... .......... .......... .......... .......... 11% 10.7M 26s
 29750K .......... .......... .......... .......... .......... 11% 11.9M 26s
 29800K .......... .......... .......... .......... .......... 11% 10.2M 26s
 29850K .......... .......... .......... .......... .......... 11% 5.80M 26s
 29900K .......... .......... .......... .......... .......... 11% 6.90M 26s
 29950K .......... .......... .......... .......... .......... 11% 4.15M 26s
 30000K .......... .......... .......... .......... .......... 11% 6.10M 26s
 30050K .......... .......... .......... .......... .......... 11% 4.43M 26s
 30100K .......... .......... .......... .......... .......... 11% 3.67M 26s
 30150K .......... .......... .......... .......... .......... 11% 9.52M 26s
 30200K .......... .......... .......... .......... .......... 11% 6.21M 26s
 30250K .......... .......... .......... .......... .......... 11% 6.05M 26s
 30300K .......... .......... .......... .......... .......... 11% 7.81M 26s
 30350K .......... .......... .......... .......... .......... 11% 5.93M 26s
 30400K .......... .......... .......... .......... .......... 11% 6.65M 26s
 30450K .......... .......... .......... .......... .......... 11% 4.52M 26s
 30500K .......... .......... .......... .......... .......... 11% 14.8M 26s
 30550K .......... .......... .......... .......... .......... 11% 6.19M 26s
 30600K .......... .......... .......... .......... .......... 11% 5.22M 26s
 30650K .......... .......... .......... .......... .......... 11% 6.88M 26s
 30700K .......... .......... .......... .......... .......... 11% 6.38M 26s
 30750K .......... .......... .......... .......... .......... 11% 6.37M 26s
 30800K .......... .......... .......... .......... .......... 11% 7.48M 26s
 30850K .......... .......... .......... .......... .......... 11% 8.85M 26s
 30900K .......... .......... .......... .......... .......... 11% 8.63M 26s
 30950K .......... .......... .......... .......... .......... 11% 6.71M 26s
 31000K .......... .......... .......... .......... .......... 11% 8.03M 26s
 31050K .......... .......... .......... .......... .......... 11% 5.52M 26s
 31100K .......... .......... .......... .......... .......... 11% 7.49M 26s
 31150K .......... .......... .......... .......... .......... 11% 8.58M 26s
 31200K .......... .......... .......... .......... .......... 11% 5.90M 26s
 31250K .......... .......... .......... .......... .......... 11% 7.95M 26s
 31300K .......... .......... .......... .......... .......... 11% 7.67M 26s
 31350K .......... .......... .......... .......... .......... 11% 29.2M 26s
 31400K .......... .......... .......... .......... .......... 11% 19.7M 26s
 31450K .......... .......... .......... .......... .......... 12% 11.1M 26s
 31500K .......... .......... .......... .......... .......... 12% 11.1M 26s
 31550K .......... .......... .......... .......... .......... 12% 1.91M 27s
 31600K .......... .......... .......... .......... .......... 12% 3.66M 27s
 31650K .......... .......... .......... .......... .......... 12% 10.4M 27s
 31700K .......... .......... .......... .......... .......... 12% 6.17M 27s
 31750K .......... .......... .......... .......... .......... 12% 6.46M 27s
 31800K .......... .......... .......... .......... .......... 12% 7.26M 27s
 31850K .......... .......... .......... .......... .......... 12% 13.4M 27s
 31900K .......... .......... .......... .......... .......... 12% 8.51M 27s
 31950K .......... .......... .......... .......... .......... 12% 12.2M 27s
 32000K .......... .......... .......... .......... .......... 12% 7.38M 27s
 32050K .......... .......... .......... .......... .......... 12% 10.7M 27s
 32100K .......... .......... .......... .......... .......... 12% 6.78M 27s
 32150K .......... .......... .......... .......... .......... 12% 6.34M 27s
 32200K .......... .......... .......... .......... .......... 12% 7.59M 27s
 32250K .......... .......... .......... .......... .......... 12% 6.58M 27s
 32300K .......... .......... .......... .......... .......... 12% 6.06M 27s
 32350K .......... .......... .......... .......... .......... 12% 4.48M 27s
 32400K .......... .......... .......... .......... .......... 12% 5.26M 27s
 32450K .......... .......... .......... .......... .......... 12% 3.46M 27s
 32500K .......... .......... .......... .......... .......... 12% 3.77M 27s
 32550K .......... .......... .......... .......... .......... 12% 2.92M 27s
 32600K .......... .......... .......... .......... .......... 12% 1.40M 27s
 32650K .......... .......... .......... .......... .......... 12% 4.30M 27s
 32700K .......... .......... .......... .......... .......... 12% 4.19M 27s
 32750K .......... .......... .......... .......... .......... 12% 4.43M 27s
 32800K .......... .......... .......... .......... .......... 12% 3.73M 27s
 32850K .......... .......... .......... .......... .......... 12% 3.96M 27s
 32900K .......... .......... .......... .......... .......... 12% 4.75M 27s
 32950K .......... .......... .......... .......... .......... 12% 6.69M 27s
 33000K .......... .......... .......... .......... .......... 12% 3.47M 27s
 33050K .......... .......... .......... .......... .......... 12%  114M 27s
 33100K .......... .......... .......... .......... .......... 12% 4.19M 27s
 33150K .......... .......... .......... .......... .......... 12% 97.6M 27s
 33200K .......... .......... .......... .......... .......... 12% 5.96M 27s
 33250K .......... .......... .......... .......... .......... 12%  138M 27s
 33300K .......... .......... .......... .......... .......... 12% 12.9M 27s
 33350K .......... .......... .......... .......... .......... 12% 7.82M 27s
 33400K .......... .......... .......... .......... .......... 12% 10.8M 27s
 33450K .......... .......... .......... .......... .......... 12% 10.2M 27s
 33500K .......... .......... .......... .......... .......... 12% 12.1M 27s
 33550K .......... .......... .......... .......... .......... 12% 7.53M 27s
 33600K .......... .......... .......... .......... .......... 12% 7.83M 27s
 33650K .......... .......... .......... .......... .......... 12% 5.79M 27s
 33700K .......... .......... .......... .......... .......... 12% 4.03M 27s
 33750K .......... .......... .......... .......... .......... 12% 4.21M 27s
 33800K .......... .......... .......... .......... .......... 12% 4.74M 27s
 33850K .......... .......... .......... .......... .......... 12% 8.44M 27s
 33900K .......... .......... .......... .......... .......... 12% 12.6M 27s
 33950K .......... .......... .......... .......... .......... 12% 10.4M 27s
 34000K .......... .......... .......... .......... .......... 12% 14.8M 27s
 34050K .......... .......... .......... .......... .......... 13% 8.61M 27s
 34100K .......... .......... .......... .......... .......... 13% 9.70M 27s
 34150K .......... .......... .......... .......... .......... 13% 6.46M 27s
 34200K .......... .......... .......... .......... .......... 13% 4.96M 27s
 34250K .......... .......... .......... .......... .......... 13% 6.02M 27s
 34300K .......... .......... .......... .......... .......... 13% 7.49M 27s
 34350K .......... .......... .......... .......... .......... 13% 5.96M 27s
 34400K .......... .......... .......... .......... .......... 13% 7.89M 27s
 34450K .......... .......... .......... .......... .......... 13% 5.91M 27s
 34500K .......... .......... .......... .......... .......... 13% 5.79M 27s
 34550K .......... .......... .......... .......... .......... 13% 7.70M 27s
 34600K .......... .......... .......... .......... .......... 13% 7.15M 27s
 34650K .......... .......... .......... .......... .......... 13% 8.85M 27s
 34700K .......... .......... .......... .......... .......... 13% 4.43M 27s
 34750K .......... .......... .......... .......... .......... 13% 4.72M 27s
 34800K .......... .......... .......... .......... .......... 13% 3.09M 27s
 34850K .......... .......... .......... .......... .......... 13% 2.18M 27s
 34900K .......... .......... .......... .......... .......... 13% 3.31M 27s
 34950K .......... .......... .......... .......... .......... 13% 4.23M 27s
 35000K .......... .......... .......... .......... .......... 13% 4.50M 27s
 35050K .......... .......... .......... .......... .......... 13% 5.62M 27s
 35100K .......... .......... .......... .......... .......... 13% 3.90M 27s
 35150K .......... .......... .......... .......... .......... 13% 4.98M 28s
 35200K .......... .......... .......... .......... .......... 13% 3.62M 28s
 35250K .......... .......... .......... .......... .......... 13% 4.87M 28s
 35300K .......... .......... .......... .......... .......... 13% 6.12M 28s
 35350K .......... .......... .......... .......... .......... 13% 6.00M 28s
 35400K .......... .......... .......... .......... .......... 13% 31.6M 28s
 35450K .......... .......... .......... .......... .......... 13% 30.4M 28s
 35500K .......... .......... .......... .......... .......... 13% 15.9M 27s
 35550K .......... .......... .......... .......... .......... 13% 53.6M 27s
 35600K .......... .......... .......... .......... .......... 13% 13.2M 27s
 35650K .......... .......... .......... .......... .......... 13% 14.5M 27s
 35700K .......... .......... .......... .......... .......... 13% 5.80M 27s
 35750K .......... .......... .......... .......... .......... 13% 7.70M 27s
 35800K .......... .......... .......... .......... .......... 13% 12.3M 27s
 35850K .......... .......... .......... .......... .......... 13% 7.54M 27s
 35900K .......... .......... .......... .......... .......... 13% 8.01M 27s
 35950K .......... .......... .......... .......... .......... 13% 7.40M 27s
 36000K .......... .......... .......... .......... .......... 13% 9.33M 27s
 36050K .......... .......... .......... .......... .......... 13% 11.5M 27s
 36100K .......... .......... .......... .......... .......... 13% 7.90M 27s
 36150K .......... .......... .......... .......... .......... 13% 8.38M 27s
 36200K .......... .......... .......... .......... .......... 13% 7.04M 27s
 36250K .......... .......... .......... .......... .......... 13% 7.55M 27s
 36300K .......... .......... .......... .......... .......... 13% 7.38M 27s
 36350K .......... .......... .......... .......... .......... 13% 6.77M 27s
 36400K .......... .......... .......... .......... .......... 13% 8.92M 27s
 36450K .......... .......... .......... .......... .......... 13% 13.8M 27s
 36500K .......... .......... .......... .......... .......... 13% 26.4M 27s
 36550K .......... .......... .......... .......... .......... 13% 15.8M 27s
 36600K .......... .......... .......... .......... .......... 13% 11.7M 27s
 36650K .......... .......... .......... .......... .......... 13% 24.2M 27s
 36700K .......... .......... .......... .......... .......... 14% 11.6M 27s
 36750K .......... .......... .......... .......... .......... 14% 16.9M 27s
 36800K .......... .......... .......... .......... .......... 14% 15.3M 27s
 36850K .......... .......... .......... .......... .......... 14% 12.7M 27s
 36900K .......... .......... .......... .......... .......... 14% 12.7M 27s
 36950K .......... .......... .......... .......... .......... 14% 15.1M 27s
 37000K .......... .......... .......... .......... .......... 14% 19.5M 27s
 37050K .......... .......... .......... .......... .......... 14% 19.0M 27s
 37100K .......... .......... .......... .......... .......... 14% 12.4M 27s
 37150K .......... .......... .......... .......... .......... 14% 21.7M 27s
 37200K .......... .......... .......... .......... .......... 14% 11.1M 27s
 37250K .......... .......... .......... .......... .......... 14% 11.3M 27s
 37300K .......... .......... .......... .......... .......... 14% 12.3M 27s
 37350K .......... .......... .......... .......... .......... 14% 14.3M 27s
 37400K .......... .......... .......... .......... .......... 14% 14.0M 27s
 37450K .......... .......... .......... .......... .......... 14% 11.9M 27s
 37500K .......... .......... .......... .......... .......... 14% 8.08M 27s
 37550K .......... .......... .......... .......... .......... 14% 7.86M 27s
 37600K .......... .......... .......... .......... .......... 14% 3.10M 27s
 37650K .......... .......... .......... .......... .......... 14% 4.34M 27s
 37700K .......... .......... .......... .......... .......... 14%  129M 27s
 37750K .......... .......... .......... .......... .......... 14% 11.2M 27s
 37800K .......... .......... .......... .......... .......... 14% 7.55M 27s
 37850K .......... .......... .......... .......... .......... 14% 5.96M 27s
 37900K .......... .......... .......... .......... .......... 14% 9.58M 27s
 37950K .......... .......... .......... .......... .......... 14% 4.91M 27s
 38000K .......... .......... .......... .......... .......... 14% 7.59M 27s
 38050K .......... .......... .......... .......... .......... 14%  214K 28s
 38100K .......... .......... .......... .......... .......... 14% 3.07M 28s
 38150K .......... .......... .......... .......... .......... 14% 8.59M 28s
 38200K .......... .......... .......... .......... .......... 14% 6.99M 28s
 38250K .......... .......... .......... .......... .......... 14% 7.74M 28s
 38300K .......... .......... .......... .......... .......... 14% 7.54M 28s
 38350K .......... .......... .......... .......... .......... 14% 8.04M 28s
 38400K .......... .......... .......... .......... .......... 14% 12.1M 28s
 38450K .......... .......... .......... .......... .......... 14% 7.05M 28s
 38500K .......... .......... .......... .......... .......... 14% 8.46M 28s
 38550K .......... .......... .......... .......... .......... 14% 6.33M 28s
 38600K .......... .......... .......... .......... .......... 14% 10.6M 28s
 38650K .......... .......... .......... .......... .......... 14% 30.3M 28s
 38700K .......... .......... .......... .......... .......... 14% 10.9M 28s
 38750K .......... .......... .......... .......... .......... 14% 27.3M 28s
 38800K .......... .......... .......... .......... .......... 14% 22.7M 28s
 38850K .......... .......... .......... .......... .......... 14% 25.0M 28s
 38900K .......... .......... .......... .......... .......... 14% 63.6M 28s
 38950K .......... .......... .......... .......... .......... 14% 27.1M 28s
 39000K .......... .......... .......... .......... .......... 14% 27.5M 28s
 39050K .......... .......... .......... .......... .......... 14% 12.9M 28s
 39100K .......... .......... .......... .......... .......... 14% 12.1M 28s
 39150K .......... .......... .......... .......... .......... 14% 51.2M 28s
 39200K .......... .......... .......... .......... .......... 14% 18.9M 28s
 39250K .......... .......... .......... .......... .......... 14% 21.5M 28s
 39300K .......... .......... .......... .......... .......... 15% 22.2M 28s
 39350K .......... .......... .......... .......... .......... 15% 22.6M 28s
 39400K .......... .......... .......... .......... .......... 15% 10.4M 28s
 39450K .......... .......... .......... .......... .......... 15% 95.6M 28s
 39500K .......... .......... .......... .......... .......... 15% 23.4M 28s
 39550K .......... .......... .......... .......... .......... 15% 9.45M 28s
 39600K .......... .......... .......... .......... .......... 15% 97.2M 28s
 39650K .......... .......... .......... .......... .......... 15% 11.2M 28s
 39700K .......... .......... .......... .......... .......... 15% 9.75M 28s
 39750K .......... .......... .......... .......... .......... 15% 19.4M 28s
 39800K .......... .......... .......... .......... .......... 15% 12.6M 28s
 39850K .......... .......... .......... .......... .......... 15% 9.22M 28s
 39900K .......... .......... .......... .......... .......... 15% 18.7M 28s
 39950K .......... .......... .......... .......... .......... 15% 5.61M 28s
 40000K .......... .......... .......... .......... .......... 15% 8.48M 28s
 40050K .......... .......... .......... .......... .......... 15% 10.2M 27s
 40100K .......... .......... .......... .......... .......... 15% 6.50M 27s
 40150K .......... .......... .......... .......... .......... 15% 8.03M 27s
 40200K .......... .......... .......... .......... .......... 15% 9.56M 27s
 40250K .......... .......... .......... .......... .......... 15% 10.6M 27s
 40300K .......... .......... .......... .......... .......... 15% 18.7M 27s
 40350K .......... .......... .......... .......... .......... 15% 11.6M 27s
 40400K .......... .......... .......... .......... .......... 15% 12.5M 27s
 40450K .......... .......... .......... .......... .......... 15% 8.19M 27s
 40500K .......... .......... .......... .......... .......... 15% 7.55M 27s
 40550K .......... .......... .......... .......... .......... 15% 5.73M 27s
 40600K .......... .......... .......... .......... .......... 15% 3.63M 27s
 40650K .......... .......... .......... .......... .......... 15% 4.07M 27s
 40700K .......... .......... .......... .......... .......... 15% 2.50M 28s
 40750K .......... .......... .......... .......... .......... 15% 2.69M 28s
 40800K .......... .......... .......... .......... .......... 15% 3.95M 28s
 40850K .......... .......... .......... .......... .......... 15% 4.65M 28s
 40900K .......... .......... .......... .......... .......... 15% 4.57M 28s
 40950K .......... .......... .......... .......... .......... 15% 6.09M 28s
 41000K .......... .......... .......... .......... .......... 15% 13.5M 28s
 41050K .......... .......... .......... .......... .......... 15% 18.2M 28s
 41100K .......... .......... .......... .......... .......... 15% 17.8M 28s
 41150K .......... .......... .......... .......... .......... 15% 30.1M 28s
 41200K .......... .......... .......... .......... .......... 15% 14.3M 28s
 41250K .......... .......... .......... .......... .......... 15% 18.1M 27s
 41300K .......... .......... .......... .......... .......... 15% 17.9M 27s
 41350K .......... .......... .......... .......... .......... 15% 13.3M 27s
 41400K .......... .......... .......... .......... .......... 15% 13.9M 27s
 41450K .......... .......... .......... .......... .......... 15% 15.5M 27s
 41500K .......... .......... .......... .......... .......... 15% 9.97M 27s
 41550K .......... .......... .......... .......... .......... 15% 16.4M 27s
 41600K .......... .......... .......... .......... .......... 15% 15.9M 27s
 41650K .......... .......... .......... .......... .......... 15% 12.4M 27s
 41700K .......... .......... .......... .......... .......... 15% 13.2M 27s
 41750K .......... .......... .......... .......... .......... 15% 6.91M 27s
 41800K .......... .......... .......... .......... .......... 15% 6.33M 27s
 41850K .......... .......... .......... .......... .......... 15% 5.88M 27s
 41900K .......... .......... .......... .......... .......... 15% 6.09M 27s
 41950K .......... .......... .......... .......... .......... 16% 4.33M 27s
 42000K .......... .......... .......... .......... .......... 16% 7.47M 27s
 42050K .......... .......... .......... .......... .......... 16% 4.41M 27s
 42100K .......... .......... .......... .......... .......... 16% 3.66M 27s
 42150K .......... .......... .......... .......... .......... 16% 4.30M 27s
 42200K .......... .......... .......... .......... .......... 16% 3.86M 27s
 42250K .......... .......... .......... .......... .......... 16% 5.27M 27s
 42300K .......... .......... .......... .......... .......... 16% 6.29M 27s
 42350K .......... .......... .......... .......... .......... 16% 6.08M 27s
 42400K .......... .......... .......... .......... .......... 16% 5.52M 27s
 42450K .......... .......... .......... .......... .......... 16% 3.96M 27s
 42500K .......... .......... .......... .......... .......... 16% 3.28M 28s
 42550K .......... .......... .......... .......... .......... 16% 3.03M 28s
 42600K .......... .......... .......... .......... .......... 16% 3.00M 28s
 42650K .......... .......... .......... .......... .......... 16% 3.18M 28s
 42700K .......... .......... .......... .......... .......... 16% 3.07M 28s
 42750K .......... .......... .......... .......... .......... 16% 3.71M 28s
 42800K .......... .......... .......... .......... .......... 16% 2.51M 28s
 42850K .......... .......... .......... .......... .......... 16% 2.85M 28s
 42900K .......... .......... .......... .......... .......... 16% 10.1M 28s
 42950K .......... .......... .......... .......... .......... 16% 19.8M 28s
 43000K .......... .......... .......... .......... .......... 16% 18.3M 28s
 43050K .......... .......... .......... .......... .......... 16% 13.2M 28s
 43100K .......... .......... .......... .......... .......... 16% 13.8M 28s
 43150K .......... .......... .......... .......... .......... 16% 17.7M 28s
 43200K .......... .......... .......... .......... .......... 16% 9.65M 28s
 43250K .......... .......... .......... .......... .......... 16% 13.0M 28s
 43300K .......... .......... .......... .......... .......... 16% 11.8M 28s
 43350K .......... .......... .......... .......... .......... 16% 9.55M 28s
 43400K .......... .......... .......... .......... .......... 16% 9.43M 28s
 43450K .......... .......... .......... .......... .......... 16% 8.95M 28s
 43500K .......... .......... .......... .......... .......... 16% 7.61M 28s
 43550K .......... .......... .......... .......... .......... 16% 7.41M 28s
 43600K .......... .......... .......... .......... .......... 16% 16.7M 28s
 43650K .......... .......... .......... .......... .......... 16% 12.2M 28s
 43700K .......... .......... .......... .......... .......... 16% 11.9M 28s
 43750K .......... .......... .......... .......... .......... 16% 14.6M 28s
 43800K .......... .......... .......... .......... .......... 16% 13.0M 27s
 43850K .......... .......... .......... .......... .......... 16% 14.5M 27s
 43900K .......... .......... .......... .......... .......... 16% 8.76M 27s
 43950K .......... .......... .......... .......... .......... 16% 9.52M 27s
 44000K .......... .......... .......... .......... .......... 16% 7.84M 27s
 44050K .......... .......... .......... .......... .......... 16% 8.64M 27s
 44100K .......... .......... .......... .......... .......... 16% 6.27M 27s
 44150K .......... .......... .......... .......... .......... 16% 7.27M 27s
 44200K .......... .......... .......... .......... .......... 16% 5.62M 27s
 44250K .......... .......... .......... .......... .......... 16% 6.89M 27s
 44300K .......... .......... .......... .......... .......... 16% 5.70M 27s
 44350K .......... .......... .......... .......... .......... 16% 3.83M 27s
 44400K .......... .......... .......... .......... .......... 16% 2.44M 28s
 44450K .......... .......... .......... .......... .......... 16% 5.87M 28s
 44500K .......... .......... .......... .......... .......... 16% 6.43M 28s
 44550K .......... .......... .......... .......... .......... 17% 5.73M 28s
 44600K .......... .......... .......... .......... .......... 17% 2.85M 28s
 44650K .......... .......... .......... .......... .......... 17% 3.67M 28s
 44700K .......... .......... .......... .......... .......... 17% 8.90M 28s
 44750K .......... .......... .......... .......... .......... 17% 10.4M 28s
 44800K .......... .......... .......... .......... .......... 17% 9.75M 28s
 44850K .......... .......... .......... .......... .......... 17% 11.5M 28s
 44900K .......... .......... .......... .......... .......... 17% 7.06M 28s
 44950K .......... .......... .......... .......... .......... 17% 6.35M 28s
 45000K .......... .......... .......... .......... .......... 17% 7.53M 28s
 45050K .......... .......... .......... .......... .......... 17% 5.19M 28s
 45100K .......... .......... .......... .......... .......... 17% 7.20M 28s
 45150K .......... .......... .......... .......... .......... 17% 8.61M 28s
 45200K .......... .......... .......... .......... .......... 17% 8.17M 28s
 45250K .......... .......... .......... .......... .......... 17% 10.8M 28s
 45300K .......... .......... .......... .......... .......... 17% 11.1M 28s
 45350K .......... .......... .......... .......... .......... 17% 9.34M 27s
 45400K .......... .......... .......... .......... .......... 17% 9.96M 27s
 45450K .......... .......... .......... .......... .......... 17% 21.7M 27s
 45500K .......... .......... .......... .......... .......... 17% 14.3M 27s
 45550K .......... .......... .......... .......... .......... 17% 27.8M 27s
 45600K .......... .......... .......... .......... .......... 17% 19.5M 27s
 45650K .......... .......... .......... .......... .......... 17% 21.3M 27s
 45700K .......... .......... .......... .......... .......... 17% 21.1M 27s
 45750K .......... .......... .......... .......... .......... 17% 24.0M 27s
 45800K .......... .......... .......... .......... .......... 17% 16.6M 27s
 45850K .......... .......... .......... .......... .......... 17% 12.4M 27s
 45900K .......... .......... .......... .......... .......... 17% 21.2M 27s
 45950K .......... .......... .......... .......... .......... 17% 31.0M 27s
 46000K .......... .......... .......... .......... .......... 17% 28.0M 27s
 46050K .......... .......... .......... .......... .......... 17% 45.4M 27s
 46100K .......... .......... .......... .......... .......... 17% 24.2M 27s
 46150K .......... .......... .......... .......... .......... 17% 26.5M 27s
 46200K .......... .......... .......... .......... .......... 17% 38.2M 27s
 46250K .......... .......... .......... .......... .......... 17% 9.95M 27s
 46300K .......... .......... .......... .......... .......... 17%  106M 27s
 46350K .......... .......... .......... .......... .......... 17% 11.3M 27s
 46400K .......... .......... .......... .......... .......... 17% 14.1M 27s
 46450K .......... .......... .......... .......... .......... 17% 7.86M 27s
 46500K .......... .......... .......... .......... .......... 17% 11.2M 27s
 46550K .......... .......... .......... .......... .......... 17% 8.16M 27s
 46600K .......... .......... .......... .......... .......... 17% 9.88M 27s
 46650K .......... .......... .......... .......... .......... 17% 12.0M 27s
 46700K .......... .......... .......... .......... .......... 17% 9.44M 27s
 46750K .......... .......... .......... .......... .......... 17% 14.7M 27s
 46800K .......... .......... .......... .......... .......... 17% 10.2M 27s
 46850K .......... .......... .......... .......... .......... 17% 14.1M 27s
 46900K .......... .......... .......... .......... .......... 17% 30.9M 27s
 46950K .......... .......... .......... .......... .......... 17% 14.4M 27s
 47000K .......... .......... .......... .......... .......... 17% 27.2M 27s
 47050K .......... .......... .......... .......... .......... 17% 20.1M 27s
 47100K .......... .......... .......... .......... .......... 17% 34.9M 27s
 47150K .......... .......... .......... .......... .......... 18% 19.7M 27s
 47200K .......... .......... .......... .......... .......... 18% 72.1M 27s
 47250K .......... .......... .......... .......... .......... 18% 12.8M 27s
 47300K .......... .......... .......... .......... .......... 18% 18.1M 27s
 47350K .......... .......... .......... .......... .......... 18% 21.6M 27s
 47400K .......... .......... .......... .......... .......... 18% 10.7M 27s
 47450K .......... .......... .......... .......... .......... 18% 26.3M 27s
 47500K .......... .......... .......... .......... .......... 18% 10.2M 27s
 47550K .......... .......... .......... .......... .......... 18% 12.9M 27s
 47600K .......... .......... .......... .......... .......... 18% 10.4M 27s
 47650K .......... .......... .......... .......... .......... 18% 10.2M 27s
 47700K .......... .......... .......... .......... .......... 18% 6.97M 27s
 47750K .......... .......... .......... .......... .......... 18% 8.06M 27s
 47800K .......... .......... .......... .......... .......... 18% 5.91M 27s
 47850K .......... .......... .......... .......... .......... 18% 5.84M 27s
 47900K .......... .......... .......... .......... .......... 18% 5.52M 27s
 47950K .......... .......... .......... .......... .......... 18% 6.60M 27s
 48000K .......... .......... .......... .......... .......... 18% 4.89M 27s
 48050K .......... .......... .......... .......... .......... 18% 7.91M 27s
 48100K .......... .......... .......... .......... .......... 18% 6.83M 27s
 48150K .......... .......... .......... .......... .......... 18% 5.03M 27s
 48200K .......... .......... .......... .......... .......... 18% 4.64M 27s
 48250K .......... .......... .......... .......... .......... 18% 5.44M 27s
 48300K .......... .......... .......... .......... .......... 18% 5.93M 27s
 48350K .......... .......... .......... .......... .......... 18% 4.51M 27s
 48400K .......... .......... .......... .......... .......... 18% 3.75M 27s
 48450K .......... .......... .......... .......... .......... 18% 2.86M 27s
 48500K .......... .......... .......... .......... .......... 18% 3.40M 27s
 48550K .......... .......... .......... .......... .......... 18% 4.70M 27s
 48600K .......... .......... .......... .......... .......... 18% 9.51M 27s
 48650K .......... .......... .......... .......... .......... 18% 58.5M 27s
 48700K .......... .......... .......... .......... .......... 18% 18.0M 27s
 48750K .......... .......... .......... .......... .......... 18% 22.8M 27s
 48800K .......... .......... .......... .......... .......... 18% 16.8M 27s
 48850K .......... .......... .......... .......... .......... 18% 3.57M 27s
 48900K .......... .......... .......... .......... .......... 18% 49.4M 27s
 48950K .......... .......... .......... .......... .......... 18% 10.3M 27s
 49000K .......... .......... .......... .......... .......... 18% 12.8M 27s
 49050K .......... .......... .......... .......... .......... 18% 10.0M 27s
 49100K .......... .......... .......... .......... .......... 18% 8.68M 27s
 49150K .......... .......... .......... .......... .......... 18% 9.68M 27s
 49200K .......... .......... .......... .......... .......... 18% 8.76M 27s
 49250K .......... .......... .......... .......... .......... 18% 6.20M 27s
 49300K .......... .......... .......... .......... .......... 18% 6.32M 27s
 49350K .......... .......... .......... .......... .......... 18% 5.53M 27s
 49400K .......... .......... .......... .......... .......... 18% 4.48M 27s
 49450K .......... .......... .......... .......... .......... 18% 2.54M 27s
 49500K .......... .......... .......... .......... .......... 18% 2.78M 27s
 49550K .......... .......... .......... .......... .......... 18% 2.89M 27s
 49600K .......... .......... .......... .......... .......... 18% 2.25M 27s
 49650K .......... .......... .......... .......... .......... 18% 10.2M 27s
 49700K .......... .......... .......... .......... .......... 18% 11.7M 27s
 49750K .......... .......... .......... .......... .......... 18% 15.8M 27s
 49800K .......... .......... .......... .......... .......... 19% 19.2M 27s
 49850K .......... .......... .......... .......... .......... 19% 12.1M 27s
 49900K .......... .......... .......... .......... .......... 19% 8.30M 27s
 49950K .......... .......... .......... .......... .......... 19% 11.9M 27s
 50000K .......... .......... .......... .......... .......... 19% 7.30M 27s
 50050K .......... .......... .......... .......... .......... 19% 4.80M 27s
 50100K .......... .......... .......... .......... .......... 19% 3.51M 27s
 50150K .......... .......... .......... .......... .......... 19% 3.99M 27s
 50200K .......... .......... .......... .......... .......... 19% 2.89M 27s
 50250K .......... .......... .......... .......... .......... 19% 3.88M 27s
 50300K .......... .......... .......... .......... .......... 19% 4.22M 27s
 50350K .......... .......... .......... .......... .......... 19% 11.0M 27s
 50400K .......... .......... .......... .......... .......... 19% 14.8M 27s
 50450K .......... .......... .......... .......... .......... 19% 17.9M 27s
 50500K .......... .......... .......... .......... .......... 19% 9.49M 27s
 50550K .......... .......... .......... .......... .......... 19% 93.3M 27s
 50600K .......... .......... .......... .......... .......... 19% 8.29M 27s
 50650K .......... .......... .......... .......... .......... 19% 7.37M 27s
 50700K .......... .......... .......... .......... .......... 19% 8.42M 27s
 50750K .......... .......... .......... .......... .......... 19% 10.9M 27s
 50800K .......... .......... .......... .......... .......... 19% 7.16M 27s
 50850K .......... .......... .......... .......... .......... 19% 5.30M 27s
 50900K .......... .......... .......... .......... .......... 19% 6.73M 27s
 50950K .......... .......... .......... .......... .......... 19% 9.87M 27s
 51000K .......... .......... .......... .......... .......... 19% 7.03M 27s
 51050K .......... .......... .......... .......... .......... 19% 12.7M 27s
 51100K .......... .......... .......... .......... .......... 19% 9.18M 27s
 51150K .......... .......... .......... .......... .......... 19% 12.4M 27s
 51200K .......... .......... .......... .......... .......... 19% 10.8M 27s
 51250K .......... .......... .......... .......... .......... 19% 13.4M 27s
 51300K .......... .......... .......... .......... .......... 19% 12.3M 26s
 51350K .......... .......... .......... .......... .......... 19% 10.9M 26s
 51400K .......... .......... .......... .......... .......... 19% 7.44M 26s
 51450K .......... .......... .......... .......... .......... 19% 13.2M 26s
 51500K .......... .......... .......... .......... .......... 19% 6.32M 26s
 51550K .......... .......... .......... .......... .......... 19% 7.13M 26s
 51600K .......... .......... .......... .......... .......... 19% 4.97M 26s
 51650K .......... .......... .......... .......... .......... 19% 11.3M 26s
 51700K .......... .......... .......... .......... .......... 19% 8.41M 26s
 51750K .......... .......... .......... .......... .......... 19% 5.97M 26s
 51800K .......... .......... .......... .......... .......... 19% 9.23M 26s
 51850K .......... .......... .......... .......... .......... 19% 8.65M 26s
 51900K .......... .......... .......... .......... .......... 19% 7.84M 26s
 51950K .......... .......... .......... .......... .......... 19% 5.98M 26s
 52000K .......... .......... .......... .......... .......... 19% 7.31M 26s
 52050K .......... .......... .......... .......... .......... 19% 11.7M 26s
 52100K .......... .......... .......... .......... .......... 19% 10.0M 26s
 52150K .......... .......... .......... .......... .......... 19% 6.56M 26s
 52200K .......... .......... .......... .......... .......... 19% 6.90M 26s
 52250K .......... .......... .......... .......... .......... 19% 7.43M 26s
 52300K .......... .......... .......... .......... .......... 19% 4.95M 26s
 52350K .......... .......... .......... .......... .......... 19% 3.06M 26s
 52400K .......... .......... .......... .......... .......... 20% 4.35M 26s
 52450K .......... .......... .......... .......... .......... 20% 3.92M 26s
 52500K .......... .......... .......... .......... .......... 20% 3.77M 26s
 52550K .......... .......... .......... .......... .......... 20% 3.84M 26s
 52600K .......... .......... .......... .......... .......... 20% 3.36M 27s
 52650K .......... .......... .......... .......... .......... 20% 3.94M 27s
 52700K .......... .......... .......... .......... .......... 20%  214K 27s
 52750K .......... .......... .......... .......... .......... 20% 3.82M 27s
 52800K .......... .......... .......... .......... .......... 20% 9.40M 27s
 52850K .......... .......... .......... .......... .......... 20% 9.20M 27s
 52900K .......... .......... .......... .......... .......... 20% 6.97M 27s
 52950K .......... .......... .......... .......... .......... 20% 8.51M 27s
 53000K .......... .......... .......... .......... .......... 20% 8.63M 27s
 53050K .......... .......... .......... .......... .......... 20% 8.43M 27s
 53100K .......... .......... .......... .......... .......... 20% 8.41M 27s
 53150K .......... .......... .......... .......... .......... 20% 8.91M 27s
 53200K .......... .......... .......... .......... .......... 20% 6.64M 27s
 53250K .......... .......... .......... .......... .......... 20% 11.5M 27s
 53300K .......... .......... .......... .......... .......... 20% 22.4M 27s
 53350K .......... .......... .......... .......... .......... 20% 9.89M 27s
 53400K .......... .......... .......... .......... .......... 20% 12.2M 27s
 53450K .......... .......... .......... .......... .......... 20% 8.25M 27s
 53500K .......... .......... .......... .......... .......... 20% 12.9M 27s
 53550K .......... .......... .......... .......... .......... 20% 5.47M 27s
 53600K .......... .......... .......... .......... .......... 20% 3.87M 27s
 53650K .......... .......... .......... .......... .......... 20% 4.64M 27s
 53700K .......... .......... .......... .......... .......... 20% 4.76M 27s
 53750K .......... .......... .......... .......... .......... 20% 9.41M 27s
 53800K .......... .......... .......... .......... .......... 20% 7.89M 27s
 53850K .......... .......... .......... .......... .......... 20% 4.79M 27s
 53900K .......... .......... .......... .......... .......... 20% 5.24M 27s
 53950K .......... .......... .......... .......... .......... 20% 4.80M 27s
 54000K .......... .......... .......... .......... .......... 20% 3.94M 27s
 54050K .......... .......... .......... .......... .......... 20% 3.76M 27s
 54100K .......... .......... .......... .......... .......... 20% 3.07M 27s
 54150K .......... .......... .......... .......... .......... 20% 5.18M 27s
 54200K .......... .......... .......... .......... .......... 20% 2.66M 27s
 54250K .......... .......... .......... .......... .......... 20% 3.64M 27s
 54300K .......... .......... .......... .......... .......... 20% 5.04M 27s
 54350K .......... .......... .......... .......... .......... 20% 16.8M 27s
 54400K .......... .......... .......... .......... .......... 20% 18.1M 27s
 54450K .......... .......... .......... .......... .......... 20% 15.7M 27s
 54500K .......... .......... .......... .......... .......... 20% 16.5M 27s
 54550K .......... .......... .......... .......... .......... 20% 9.58M 27s
 54600K .......... .......... .......... .......... .......... 20% 30.3M 27s
 54650K .......... .......... .......... .......... .......... 20% 14.5M 27s
 54700K .......... .......... .......... .......... .......... 20% 12.6M 27s
 54750K .......... .......... .......... .......... .......... 20% 7.81M 27s
 54800K .......... .......... .......... .......... .......... 20% 23.8M 27s
 54850K .......... .......... .......... .......... .......... 20% 6.64M 27s
 54900K .......... .......... .......... .......... .......... 20% 8.41M 27s
 54950K .......... .......... .......... .......... .......... 20% 7.62M 27s
 55000K .......... .......... .......... .......... .......... 20% 5.84M 27s
 55050K .......... .......... .......... .......... .......... 21% 11.4M 27s
 55100K .......... .......... .......... .......... .......... 21% 9.10M 27s
 55150K .......... .......... .......... .......... .......... 21% 8.51M 27s
 55200K .......... .......... .......... .......... .......... 21% 5.50M 27s
 55250K .......... .......... .......... .......... .......... 21% 6.68M 27s
 55300K .......... .......... .......... .......... .......... 21% 6.47M 27s
 55350K .......... .......... .......... .......... .......... 21% 4.50M 27s
 55400K .......... .......... .......... .......... .......... 21% 4.52M 27s
 55450K .......... .......... .......... .......... .......... 21% 3.90M 27s
 55500K .......... .......... .......... .......... .......... 21% 4.30M 27s
 55550K .......... .......... .......... .......... .......... 21% 6.42M 27s
 55600K .......... .......... .......... .......... .......... 21% 6.50M 27s
 55650K .......... .......... .......... .......... .......... 21% 8.67M 27s
 55700K .......... .......... .......... .......... .......... 21% 7.50M 27s
 55750K .......... .......... .......... .......... .......... 21% 11.0M 27s
 55800K .......... .......... .......... .......... .......... 21% 16.5M 27s
 55850K .......... .......... .......... .......... .......... 21% 20.6M 27s
 55900K .......... .......... .......... .......... .......... 21% 28.0M 27s
 55950K .......... .......... .......... .......... .......... 21% 30.4M 27s
 56000K .......... .......... .......... .......... .......... 21% 46.6M 27s
 56050K .......... .......... .......... .......... .......... 21% 73.2M 27s
 56100K .......... .......... .......... .......... .......... 21% 27.5M 27s
 56150K .......... .......... .......... .......... .......... 21% 55.9M 27s
 56200K .......... .......... .......... .......... .......... 21% 14.2M 27s
 56250K .......... .......... .......... .......... .......... 21% 54.9M 27s
 56300K .......... .......... .......... .......... .......... 21%  147M 27s
 56350K .......... .......... .......... .......... .......... 21% 23.5M 27s
 56400K .......... .......... .......... .......... .......... 21% 22.1M 27s
 56450K .......... .......... .......... .......... .......... 21% 26.8M 27s
 56500K .......... .......... .......... .......... .......... 21% 45.4M 27s
 56550K .......... .......... .......... .......... .......... 21% 24.8M 27s
 56600K .......... .......... .......... .......... .......... 21% 47.3M 27s
 56650K .......... .......... .......... .......... .......... 21% 22.0M 27s
 56700K .......... .......... .......... .......... .......... 21% 20.7M 27s
 56750K .......... .......... .......... .......... .......... 21% 23.3M 27s
 56800K .......... .......... .......... .......... .......... 21% 23.3M 27s
 56850K .......... .......... .......... .......... .......... 21% 31.0M 27s
 56900K .......... .......... .......... .......... .......... 21% 28.1M 27s
 56950K .......... .......... .......... .......... .......... 21% 19.0M 27s
 57000K .......... .......... .......... .......... .......... 21% 13.5M 27s
 57050K .......... .......... .......... .......... .......... 21% 16.0M 27s
 57100K .......... .......... .......... .......... .......... 21% 11.3M 27s
 57150K .......... .......... .......... .......... .......... 21% 17.1M 27s
 57200K .......... .......... .......... .......... .......... 21% 13.7M 27s
 57250K .......... .......... .......... .......... .......... 21% 11.0M 27s
 57300K .......... .......... .......... .......... .......... 21% 9.53M 27s
 57350K .......... .......... .......... .......... .......... 21% 20.5M 26s
 57400K .......... .......... .......... .......... .......... 21% 15.8M 26s
 57450K .......... .......... .......... .......... .......... 21% 8.73M 26s
 57500K .......... .......... .......... .......... .......... 21% 13.7M 26s
 57550K .......... .......... .......... .......... .......... 21% 14.6M 26s
 57600K .......... .......... .......... .......... .......... 21% 12.1M 26s
 57650K .......... .......... .......... .......... .......... 22% 15.0M 26s
 57700K .......... .......... .......... .......... .......... 22% 9.38M 26s
 57750K .......... .......... .......... .......... .......... 22% 12.0M 26s
 57800K .......... .......... .......... .......... .......... 22% 6.38M 26s
 57850K .......... .......... .......... .......... .......... 22% 5.16M 26s
 57900K .......... .......... .......... .......... .......... 22% 5.94M 26s
 57950K .......... .......... .......... .......... .......... 22% 6.41M 26s
 58000K .......... .......... .......... .......... .......... 22% 8.65M 26s
 58050K .......... .......... .......... .......... .......... 22% 17.0M 26s
 58100K .......... .......... .......... .......... .......... 22% 8.90M 26s
 58150K .......... .......... .......... .......... .......... 22% 19.4M 26s
 58200K .......... .......... .......... .......... .......... 22% 11.4M 26s
 58250K .......... .......... .......... .......... .......... 22% 8.12M 26s
 58300K .......... .......... .......... .......... .......... 22% 11.3M 26s
 58350K .......... .......... .......... .......... .......... 22% 7.96M 26s
 58400K .......... .......... .......... .......... .......... 22% 10.9M 26s
 58450K .......... .......... .......... .......... .......... 22% 8.54M 26s
 58500K .......... .......... .......... .......... .......... 22% 10.6M 26s
 58550K .......... .......... .......... .......... .......... 22% 7.99M 26s
 58600K .......... .......... .......... .......... .......... 22% 16.4M 26s
 58650K .......... .......... .......... .......... .......... 22% 27.0M 26s
 58700K .......... .......... .......... .......... .......... 22% 16.6M 26s
 58750K .......... .......... .......... .......... .......... 22% 17.2M 26s
 58800K .......... .......... .......... .......... .......... 22% 30.0M 26s
 58850K .......... .......... .......... .......... .......... 22% 32.9M 26s
 58900K .......... .......... .......... .......... .......... 22% 29.1M 26s
 58950K .......... .......... .......... .......... .......... 22% 20.9M 26s
 59000K .......... .......... .......... .......... .......... 22% 28.9M 26s
 59050K .......... .......... .......... .......... .......... 22% 24.6M 26s
 59100K .......... .......... .......... .......... .......... 22% 15.9M 26s
 59150K .......... .......... .......... .......... .......... 22% 18.4M 26s
 59200K .......... .......... .......... .......... .......... 22% 9.84M 26s
 59250K .......... .......... .......... .......... .......... 22% 7.56M 26s
 59300K .......... .......... .......... .......... .......... 22% 9.38M 26s
 59350K .......... .......... .......... .......... .......... 22% 9.27M 26s
 59400K .......... .......... .......... .......... .......... 22% 10.2M 26s
 59450K .......... .......... .......... .......... .......... 22% 9.27M 26s
 59500K .......... .......... .......... .......... .......... 22% 7.40M 26s
 59550K .......... .......... .......... .......... .......... 22% 14.4M 26s
 59600K .......... .......... .......... .......... .......... 22% 30.4M 26s
 59650K .......... .......... .......... .......... .......... 22% 28.9M 26s
 59700K .......... .......... .......... .......... .......... 22% 31.8M 26s
 59750K .......... .......... .......... .......... .......... 22% 34.6M 26s
 59800K .......... .......... .......... .......... .......... 22% 47.8M 26s
 59850K .......... .......... .......... .......... .......... 22% 34.6M 26s
 59900K .......... .......... .......... .......... .......... 22% 72.4M 26s
 59950K .......... .......... .......... .......... .......... 22% 15.4M 26s
 60000K .......... .......... .......... .......... .......... 22% 89.1M 26s
 60050K .......... .......... .......... .......... .......... 22% 7.02M 26s
 60100K .......... .......... .......... .......... .......... 22% 38.0M 26s
 60150K .......... .......... .......... .......... .......... 22% 48.5M 26s
 60200K .......... .......... .......... .......... .......... 22% 40.1M 26s
 60250K .......... .......... .......... .......... .......... 22% 27.8M 26s
 60300K .......... .......... .......... .......... .......... 23% 20.4M 26s
 60350K .......... .......... .......... .......... .......... 23% 21.8M 26s
 60400K .......... .......... .......... .......... .......... 23% 24.1M 26s
 60450K .......... .......... .......... .......... .......... 23% 15.7M 26s
 60500K .......... .......... .......... .......... .......... 23% 21.8M 25s
 60550K .......... .......... .......... .......... .......... 23% 17.9M 25s
 60600K .......... .......... .......... .......... .......... 23% 22.4M 25s
 60650K .......... .......... .......... .......... .......... 23% 13.9M 25s
 60700K .......... .......... .......... .......... .......... 23% 33.5M 25s
 60750K .......... .......... .......... .......... .......... 23% 22.4M 25s
 60800K .......... .......... .......... .......... .......... 23% 19.0M 25s
 60850K .......... .......... .......... .......... .......... 23% 13.2M 25s
 60900K .......... .......... .......... .......... .......... 23% 14.5M 25s
 60950K .......... .......... .......... .......... .......... 23% 7.92M 25s
 61000K .......... .......... .......... .......... .......... 23% 14.0M 25s
 61050K .......... .......... .......... .......... .......... 23% 11.6M 25s
 61100K .......... .......... .......... .......... .......... 23% 12.8M 25s
 61150K .......... .......... .......... .......... .......... 23% 11.6M 25s
 61200K .......... .......... .......... .......... .......... 23% 12.8M 25s
 61250K .......... .......... .......... .......... .......... 23% 13.6M 25s
 61300K .......... .......... .......... .......... .......... 23% 10.3M 25s
 61350K .......... .......... .......... .......... .......... 23% 44.7M 25s
 61400K .......... .......... .......... .......... .......... 23% 16.9M 25s
 61450K .......... .......... .......... .......... .......... 23% 53.0M 25s
 61500K .......... .......... .......... .......... .......... 23% 16.4M 25s
 61550K .......... .......... .......... .......... .......... 23% 13.3M 25s
 61600K .......... .......... .......... .......... .......... 23% 21.3M 25s
 61650K .......... .......... .......... .......... .......... 23% 21.1M 25s
 61700K .......... .......... .......... .......... .......... 23% 17.1M 25s
 61750K .......... .......... .......... .......... .......... 23% 13.3M 25s
 61800K .......... .......... .......... .......... .......... 23% 17.0M 25s
 61850K .......... .......... .......... .......... .......... 23% 9.79M 25s
 61900K .......... .......... .......... .......... .......... 23% 16.8M 25s
 61950K .......... .......... .......... .......... .......... 23% 14.6M 25s
 62000K .......... .......... .......... .......... .......... 23% 14.7M 25s
 62050K .......... .......... .......... .......... .......... 23% 15.3M 25s
 62100K .......... .......... .......... .......... .......... 23% 22.0M 25s
 62150K .......... .......... .......... .......... .......... 23% 21.1M 25s
 62200K .......... .......... .......... .......... .......... 23% 9.30M 25s
 62250K .......... .......... .......... .......... .......... 23% 45.2M 25s
 62300K .......... .......... .......... .......... .......... 23% 7.97M 25s
 62350K .......... .......... .......... .......... .......... 23%  124M 25s
 62400K .......... .......... .......... .......... .......... 23% 10.7M 25s
 62450K .......... .......... .......... .......... .......... 23% 6.77M 25s
 62500K .......... .......... .......... .......... .......... 23% 60.1M 25s
 62550K .......... .......... .......... .......... .......... 23% 73.9M 25s
 62600K .......... .......... .......... .......... .......... 23% 10.6M 25s
 62650K .......... .......... .......... .......... .......... 23% 50.3M 25s
 62700K .......... .......... .......... .......... .......... 23% 13.9M 25s
 62750K .......... .......... .......... .......... .......... 23% 21.9M 25s
 62800K .......... .......... .......... .......... .......... 23% 12.8M 25s
 62850K .......... .......... .......... .......... .......... 23% 10.9M 25s
 62900K .......... .......... .......... .......... .......... 24% 17.6M 25s
 62950K .......... .......... .......... .......... .......... 24% 11.8M 25s
 63000K .......... .......... .......... .......... .......... 24% 13.8M 25s
 63050K .......... .......... .......... .......... .......... 24% 16.0M 25s
 63100K .......... .......... .......... .......... .......... 24% 13.7M 25s
 63150K .......... .......... .......... .......... .......... 24% 13.0M 25s
 63200K .......... .......... .......... .......... .......... 24% 14.2M 25s
 63250K .......... .......... .......... .......... .......... 24% 9.47M 25s
 63300K .......... .......... .......... .......... .......... 24% 7.77M 25s
 63350K .......... .......... .......... .......... .......... 24% 7.49M 25s
 63400K .......... .......... .......... .......... .......... 24% 8.61M 25s
 63450K .......... .......... .......... .......... .......... 24% 8.40M 25s
 63500K .......... .......... .......... .......... .......... 24% 7.95M 25s
 63550K .......... .......... .......... .......... .......... 24% 9.56M 25s
 63600K .......... .......... .......... .......... .......... 24% 9.27M 25s
 63650K .......... .......... .......... .......... .......... 24% 9.89M 25s
 63700K .......... .......... .......... .......... .......... 24% 8.47M 25s
 63750K .......... .......... .......... .......... .......... 24% 9.76M 25s
 63800K .......... .......... .......... .......... .......... 24% 10.3M 25s
 63850K .......... .......... .......... .......... .......... 24% 10.3M 25s
 63900K .......... .......... .......... .......... .......... 24% 25.1M 24s
 63950K .......... .......... .......... .......... .......... 24% 77.5M 24s
 64000K .......... .......... .......... .......... .......... 24% 46.4M 24s
 64050K .......... .......... .......... .......... .......... 24% 14.7M 24s
 64100K .......... .......... .......... .......... .......... 24% 47.7M 24s
 64150K .......... .......... .......... .......... .......... 24% 68.1M 24s
 64200K .......... .......... .......... .......... .......... 24% 37.3M 24s
 64250K .......... .......... .......... .......... .......... 24% 23.5M 24s
 64300K .......... .......... .......... .......... .......... 24% 45.5M 24s
 64350K .......... .......... .......... .......... .......... 24% 20.1M 24s
 64400K .......... .......... .......... .......... .......... 24% 39.6M 24s
 64450K .......... .......... .......... .......... .......... 24% 25.4M 24s
 64500K .......... .......... .......... .......... .......... 24% 27.1M 24s
 64550K .......... .......... .......... .......... .......... 24% 29.1M 24s
 64600K .......... .......... .......... .......... .......... 24% 26.9M 24s
 64650K .......... .......... .......... .......... .......... 24% 26.3M 24s
 64700K .......... .......... .......... .......... .......... 24% 27.4M 24s
 64750K .......... .......... .......... .......... .......... 24% 18.4M 24s
 64800K .......... .......... .......... .......... .......... 24% 31.6M 24s
 64850K .......... .......... .......... .......... .......... 24% 16.1M 24s
 64900K .......... .......... .......... .......... .......... 24% 29.1M 24s
 64950K .......... .......... .......... .......... .......... 24% 16.7M 24s
 65000K .......... .......... .......... .......... .......... 24% 23.2M 24s
 65050K .......... .......... .......... .......... .......... 24% 26.2M 24s
 65100K .......... .......... .......... .......... .......... 24% 24.1M 24s
 65150K .......... .......... .......... .......... .......... 24% 53.2M 24s
 65200K .......... .......... .......... .......... .......... 24% 37.0M 24s
 65250K .......... .......... .......... .......... .......... 24% 33.5M 24s
 65300K .......... .......... .......... .......... .......... 24% 96.5M 24s
 65350K .......... .......... .......... .......... .......... 24% 9.42M 24s
 65400K .......... .......... .......... .......... .......... 24%  106M 24s
 65450K .......... .......... .......... .......... .......... 24% 61.4M 24s
 65500K .......... .......... .......... .......... .......... 25% 10.2M 24s
 65550K .......... .......... .......... .......... .......... 25% 99.4M 24s
 65600K .......... .......... .......... .......... .......... 25% 11.1M 24s
 65650K .......... .......... .......... .......... .......... 25%  223M 24s
 65700K .......... .......... .......... .......... .......... 25% 7.62M 24s
 65750K .......... .......... .......... .......... .......... 25% 14.2M 24s
 65800K .......... .......... .......... .......... .......... 25% 8.69M 24s
 65850K .......... .......... .......... .......... .......... 25% 7.00M 24s
 65900K .......... .......... .......... .......... .......... 25% 8.74M 24s
 65950K .......... .......... .......... .......... .......... 25% 8.19M 24s
 66000K .......... .......... .......... .......... .......... 25% 11.8M 24s
 66050K .......... .......... .......... .......... .......... 25% 9.68M 24s
 66100K .......... .......... .......... .......... .......... 25% 8.69M 24s
 66150K .......... .......... .......... .......... .......... 25% 6.72M 24s
 66200K .......... .......... .......... .......... .......... 25% 4.91M 24s
 66250K .......... .......... .......... .......... .......... 25% 5.50M 24s
 66300K .......... .......... .......... .......... .......... 25% 5.74M 24s
 66350K .......... .......... .......... .......... .......... 25% 10.1M 24s
 66400K .......... .......... .......... .......... .......... 25% 9.92M 24s
 66450K .......... .......... .......... .......... .......... 25% 8.69M 24s
 66500K .......... .......... .......... .......... .......... 25% 7.51M 24s
 66550K .......... .......... .......... .......... .......... 25% 6.24M 24s
 66600K .......... .......... .......... .......... .......... 25% 5.73M 24s
 66650K .......... .......... .......... .......... .......... 25% 7.15M 24s
 66700K .......... .......... .......... .......... .......... 25% 8.09M 24s
 66750K .......... .......... .......... .......... .......... 25% 7.92M 24s
 66800K .......... .......... .......... .......... .......... 25% 17.4M 24s
 66850K .......... .......... .......... .......... .......... 25% 9.71M 24s
 66900K .......... .......... .......... .......... .......... 25% 10.4M 24s
 66950K .......... .......... .......... .......... .......... 25% 9.31M 24s
 67000K .......... .......... .......... .......... .......... 25% 13.3M 24s
 67050K .......... .......... .......... .......... .......... 25% 11.1M 24s
 67100K .......... .......... .......... .......... .......... 25% 8.97M 24s
 67150K .......... .......... .......... .......... .......... 25% 9.57M 24s
 67200K .......... .......... .......... .......... .......... 25% 6.00M 24s
 67250K .......... .......... .......... .......... .......... 25% 6.25M 24s
 67300K .......... .......... .......... .......... .......... 25% 3.89M 24s
 67350K .......... .......... .......... .......... .......... 25% 2.68M 24s
 67400K .......... .......... .......... .......... .......... 25% 2.90M 24s
 67450K .......... .......... .......... .......... .......... 25% 2.10M 24s
 67500K .......... .......... .......... .......... .......... 25% 3.12M 24s
 67550K .......... .......... .......... .......... .......... 25% 13.2M 24s
 67600K .......... .......... .......... .......... .......... 25% 15.2M 24s
 67650K .......... .......... .......... .......... .......... 25% 14.4M 24s
 67700K .......... .......... .......... .......... .......... 25% 9.37M 24s
 67750K .......... .......... .......... .......... .......... 25% 18.8M 24s
 67800K .......... .......... .......... .......... .......... 25% 7.44M 24s
 67850K .......... .......... .......... .......... .......... 25% 7.38M 24s
 67900K .......... .......... .......... .......... .......... 25% 9.22M 24s
 67950K .......... .......... .......... .......... .......... 25% 8.36M 24s
 68000K .......... .......... .......... .......... .......... 25% 10.6M 24s
 68050K .......... .......... .......... .......... .......... 25% 8.44M 24s
 68100K .......... .......... .......... .......... .......... 25% 5.47M 24s
 68150K .......... .......... .......... .......... .......... 26% 3.16M 24s
 68200K .......... .......... .......... .......... .......... 26% 1.95M 24s
 68250K .......... .......... .......... .......... .......... 26% 1.77M 24s
 68300K .......... .......... .......... .......... .......... 26% 2.03M 24s
 68350K .......... .......... .......... .......... .......... 26% 6.42M 24s
 68400K .......... .......... .......... .......... .......... 26% 14.2M 24s
 68450K .......... .......... .......... .......... .......... 26% 10.0M 24s
 68500K .......... .......... .......... .......... .......... 26% 20.8M 24s
 68550K .......... .......... .......... .......... .......... 26% 14.5M 24s
 68600K .......... .......... .......... .......... .......... 26% 10.5M 24s
 68650K .......... .......... .......... .......... .......... 26% 13.1M 24s
 68700K .......... .......... .......... .......... .......... 26% 7.49M 24s
 68750K .......... .......... .......... .......... .......... 26% 17.6M 24s
 68800K .......... .......... .......... .......... .......... 26% 14.3M 24s
 68850K .......... .......... .......... .......... .......... 26% 13.0M 24s
 68900K .......... .......... .......... .......... .......... 26% 7.74M 24s
 68950K .......... .......... .......... .......... .......... 26% 16.9M 24s
 69000K .......... .......... .......... .......... .......... 26% 17.5M 24s
 69050K .......... .......... .......... .......... .......... 26% 11.1M 24s
 69100K .......... .......... .......... .......... .......... 26% 18.6M 24s
 69150K .......... .......... .......... .......... .......... 26% 16.0M 24s
 69200K .......... .......... .......... .......... .......... 26% 12.4M 24s
 69250K .......... .......... .......... .......... .......... 26% 12.2M 24s
 69300K .......... .......... .......... .......... .......... 26% 23.0M 24s
 69350K .......... .......... .......... .......... .......... 26% 14.9M 24s
 69400K .......... .......... .......... .......... .......... 26% 10.9M 24s
 69450K .......... .......... .......... .......... .......... 26% 17.2M 24s
 69500K .......... .......... .......... .......... .......... 26% 9.84M 24s
 69550K .......... .......... .......... .......... .......... 26% 15.7M 24s
 69600K .......... .......... .......... .......... .......... 26% 15.2M 23s
 69650K .......... .......... .......... .......... .......... 26% 10.5M 23s
 69700K .......... .......... .......... .......... .......... 26% 7.18M 23s
 69750K .......... .......... .......... .......... .......... 26% 9.29M 23s
 69800K .......... .......... .......... .......... .......... 26% 7.52M 23s
 69850K .......... .......... .......... .......... .......... 26% 6.18M 23s
 69900K .......... .......... .......... .......... .......... 26% 8.62M 23s
 69950K .......... .......... .......... .......... .......... 26% 9.66M 23s
 70000K .......... .......... .......... .......... .......... 26% 14.7M 23s
 70050K .......... .......... .......... .......... .......... 26% 15.9M 23s
 70100K .......... .......... .......... .......... .......... 26% 7.82M 23s
 70150K .......... .......... .......... .......... .......... 26% 23.3M 23s
 70200K .......... .......... .......... .......... .......... 26% 8.16M 23s
 70250K .......... .......... .......... .......... .......... 26% 17.7M 23s
 70300K .......... .......... .......... .......... .......... 26% 27.9M 23s
 70350K .......... .......... .......... .......... .......... 26% 10.1M 23s
 70400K .......... .......... .......... .......... .......... 26% 23.3M 23s
 70450K .......... .......... .......... .......... .......... 26% 11.3M 23s
 70500K .......... .......... .......... .......... .......... 26% 11.1M 23s
 70550K .......... .......... .......... .......... .......... 26% 9.02M 23s
 70600K .......... .......... .......... .......... .......... 26% 4.71M 23s
 70650K .......... .......... .......... .......... .......... 26% 4.60M 23s
 70700K .......... .......... .......... .......... .......... 26% 25.7M 23s
 70750K .......... .......... .......... .......... .......... 27% 10.4M 23s
 70800K .......... .......... .......... .......... .......... 27% 7.75M 23s
 70850K .......... .......... .......... .......... .......... 27% 6.32M 23s
 70900K .......... .......... .......... .......... .......... 27% 4.46M 23s
 70950K .......... .......... .......... .......... .......... 27%  204K 24s
 71000K .......... .......... .......... .......... .......... 27% 2.69M 24s
 71050K .......... .......... .......... .......... .......... 27% 4.28M 24s
 71100K .......... .......... .......... .......... .......... 27% 3.66M 24s
 71150K .......... .......... .......... .......... .......... 27% 4.74M 24s
 71200K .......... .......... .......... .......... .......... 27% 4.11M 24s
 71250K .......... .......... .......... .......... .......... 27% 5.23M 24s
 71300K .......... .......... .......... .......... .......... 27% 6.20M 24s
 71350K .......... .......... .......... .......... .......... 27% 4.94M 24s
 71400K .......... .......... .......... .......... .......... 27% 6.67M 24s
 71450K .......... .......... .......... .......... .......... 27% 6.21M 24s
 71500K .......... .......... .......... .......... .......... 27% 6.90M 24s
 71550K .......... .......... .......... .......... .......... 27% 7.02M 24s
 71600K .......... .......... .......... .......... .......... 27% 5.32M 24s
 71650K .......... .......... .......... .......... .......... 27% 7.36M 24s
 71700K .......... .......... .......... .......... .......... 27% 7.44M 24s
 71750K .......... .......... .......... .......... .......... 27% 7.91M 24s
 71800K .......... .......... .......... .......... .......... 27% 16.2M 24s
 71850K .......... .......... .......... .......... .......... 27% 7.45M 24s
 71900K .......... .......... .......... .......... .......... 27% 8.42M 24s
 71950K .......... .......... .......... .......... .......... 27% 5.03M 24s
 72000K .......... .......... .......... .......... .......... 27% 6.30M 24s
 72050K .......... .......... .......... .......... .......... 27% 5.35M 24s
 72100K .......... .......... .......... .......... .......... 27% 4.96M 24s
 72150K .......... .......... .......... .......... .......... 27% 6.21M 24s
 72200K .......... .......... .......... .......... .......... 27% 3.72M 24s
 72250K .......... .......... .......... .......... .......... 27% 5.98M 24s
 72300K .......... .......... .......... .......... .......... 27% 6.76M 24s
 72350K .......... .......... .......... .......... .......... 27% 4.14M 24s
 72400K .......... .......... .......... .......... .......... 27% 5.79M 24s
 72450K .......... .......... .......... .......... .......... 27% 4.79M 24s
 72500K .......... .......... .......... .......... .......... 27% 4.73M 24s
 72550K .......... .......... .......... .......... .......... 27% 5.61M 24s
 72600K .......... .......... .......... .......... .......... 27% 4.84M 24s
 72650K .......... .......... .......... .......... .......... 27% 13.6M 24s
 72700K .......... .......... .......... .......... .......... 27% 13.8M 24s
 72750K .......... .......... .......... .......... .......... 27% 11.7M 24s
 72800K .......... .......... .......... .......... .......... 27% 11.0M 24s
 72850K .......... .......... .......... .......... .......... 27% 8.28M 24s
 72900K .......... .......... .......... .......... .......... 27% 9.48M 24s
 72950K .......... .......... .......... .......... .......... 27% 8.37M 24s
 73000K .......... .......... .......... .......... .......... 27% 6.92M 24s
 73050K .......... .......... .......... .......... .......... 27% 24.7M 24s
 73100K .......... .......... .......... .......... .......... 27% 9.91M 24s
 73150K .......... .......... .......... .......... .......... 27% 11.7M 24s
 73200K .......... .......... .......... .......... .......... 27% 8.66M 24s
 73250K .......... .......... .......... .......... .......... 27% 14.7M 24s
 73300K .......... .......... .......... .......... .......... 27% 16.5M 24s
 73350K .......... .......... .......... .......... .......... 27% 20.9M 24s
 73400K .......... .......... .......... .......... .......... 28% 15.2M 24s
 73450K .......... .......... .......... .......... .......... 28% 24.1M 24s
 73500K .......... .......... .......... .......... .......... 28% 15.5M 24s
 73550K .......... .......... .......... .......... .......... 28% 7.91M 24s
 73600K .......... .......... .......... .......... .......... 28% 72.0M 24s
 73650K .......... .......... .......... .......... .......... 28% 24.1M 24s
 73700K .......... .......... .......... .......... .......... 28% 8.93M 24s
 73750K .......... .......... .......... .......... .......... 28% 15.3M 24s
 73800K .......... .......... .......... .......... .......... 28% 27.4M 24s
 73850K .......... .......... .......... .......... .......... 28% 10.9M 24s
 73900K .......... .......... .......... .......... .......... 28% 16.1M 24s
 73950K .......... .......... .......... .......... .......... 28% 8.72M 24s
 74000K .......... .......... .......... .......... .......... 28% 9.07M 24s
 74050K .......... .......... .......... .......... .......... 28% 2.63M 24s
 74100K .......... .......... .......... .......... .......... 28%  118M 24s
 74150K .......... .......... .......... .......... .......... 28% 6.74M 24s
 74200K .......... .......... .......... .......... .......... 28% 3.06M 24s
 74250K .......... .......... .......... .......... .......... 28% 3.59M 24s
 74300K .......... .......... .......... .......... .......... 28% 4.38M 24s
 74350K .......... .......... .......... .......... .......... 28% 5.70M 24s
 74400K .......... .......... .......... .......... .......... 28% 6.44M 24s
 74450K .......... .......... .......... .......... .......... 28% 6.21M 24s
 74500K .......... .......... .......... .......... .......... 28% 6.40M 24s
 74550K .......... .......... .......... .......... .......... 28% 4.85M 24s
 74600K .......... .......... .......... .......... .......... 28% 4.72M 24s
 74650K .......... .......... .......... .......... .......... 28% 6.21M 24s
 74700K .......... .......... .......... .......... .......... 28% 2.89M 24s
 74750K .......... .......... .......... .......... .......... 28% 4.69M 24s
 74800K .......... .......... .......... .......... .......... 28% 3.28M 24s
 74850K .......... .......... .......... .......... .......... 28% 2.27M 24s
 74900K .......... .......... .......... .......... .......... 28% 1.85M 24s
 74950K .......... .......... .......... .......... .......... 28% 8.21M 24s
 75000K .......... .......... .......... .......... .......... 28% 7.97M 24s
 75050K .......... .......... .......... .......... .......... 28% 6.04M 24s
 75100K .......... .......... .......... .......... .......... 28% 11.9M 24s
 75150K .......... .......... .......... .......... .......... 28% 8.53M 24s
 75200K .......... .......... .......... .......... .......... 28% 6.65M 24s
 75250K .......... .......... .......... .......... .......... 28% 9.50M 24s
 75300K .......... .......... .......... .......... .......... 28% 6.46M 24s
 75350K .......... .......... .......... .......... .......... 28% 6.57M 24s
 75400K .......... .......... .......... .......... .......... 28% 9.85M 24s
 75450K .......... .......... .......... .......... .......... 28% 7.13M 24s
 75500K .......... .......... .......... .......... .......... 28% 7.82M 24s
 75550K .......... .......... .......... .......... .......... 28% 10.4M 24s
 75600K .......... .......... .......... .......... .......... 28% 9.02M 24s
 75650K .......... .......... .......... .......... .......... 28% 7.48M 24s
 75700K .......... .......... .......... .......... .......... 28% 6.38M 24s
 75750K .......... .......... .......... .......... .......... 28% 7.23M 24s
 75800K .......... .......... .......... .......... .......... 28% 7.68M 24s
 75850K .......... .......... .......... .......... .......... 28% 6.94M 24s
 75900K .......... .......... .......... .......... .......... 28% 7.58M 24s
 75950K .......... .......... .......... .......... .......... 28% 7.68M 24s
 76000K .......... .......... .......... .......... .......... 29% 10.1M 24s
 76050K .......... .......... .......... .......... .......... 29% 6.24M 24s
 76100K .......... .......... .......... .......... .......... 29% 6.98M 24s
 76150K .......... .......... .......... .......... .......... 29% 6.59M 24s
 76200K .......... .......... .......... .......... .......... 29%  710K 24s
 76250K .......... .......... .......... .......... .......... 29% 3.73M 24s
 76300K .......... .......... .......... .......... .......... 29% 3.00M 24s
 76350K .......... .......... .......... .......... .......... 29% 3.69M 24s
 76400K .......... .......... .......... .......... .......... 29% 20.3M 24s
 76450K .......... .......... .......... .......... .......... 29% 16.8M 24s
 76500K .......... .......... .......... .......... .......... 29% 70.3M 24s
 76550K .......... .......... .......... .......... .......... 29% 79.0M 24s
 76600K .......... .......... .......... .......... .......... 29% 38.7M 24s
 76650K .......... .......... .......... .......... .......... 29% 62.9M 24s
 76700K .......... .......... .......... .......... .......... 29% 11.0M 24s
 76750K .......... .......... .......... .......... .......... 29% 47.3M 24s
 76800K .......... .......... .......... .......... .......... 29%  126M 24s
 76850K .......... .......... .......... .......... .......... 29% 11.7M 24s
 76900K .......... .......... .......... .......... .......... 29% 60.9M 24s
 76950K .......... .......... .......... .......... .......... 29% 42.2M 24s
 77000K .......... .......... .......... .......... .......... 29% 20.2M 24s
 77050K .......... .......... .......... .......... .......... 29% 13.8M 24s
 77100K .......... .......... .......... .......... .......... 29% 13.6M 24s
 77150K .......... .......... .......... .......... .......... 29% 26.6M 24s
 77200K .......... .......... .......... .......... .......... 29% 6.77M 24s
 77250K .......... .......... .......... .......... .......... 29% 10.2M 24s
 77300K .......... .......... .......... .......... .......... 29% 9.49M 23s
 77350K .......... .......... .......... .......... .......... 29% 7.04M 23s
 77400K .......... .......... .......... .......... .......... 29% 9.50M 23s
 77450K .......... .......... .......... .......... .......... 29% 4.62M 23s
 77500K .......... .......... .......... .......... .......... 29% 5.46M 23s
 77550K .......... .......... .......... .......... .......... 29% 4.98M 23s
 77600K .......... .......... .......... .......... .......... 29% 4.60M 23s
 77650K .......... .......... .......... .......... .......... 29% 5.98M 23s
 77700K .......... .......... .......... .......... .......... 29% 8.02M 23s
 77750K .......... .......... .......... .......... .......... 29% 20.5M 23s
 77800K .......... .......... .......... .......... .......... 29% 28.0M 23s
 77850K .......... .......... .......... .......... .......... 29% 20.8M 23s
 77900K .......... .......... .......... .......... .......... 29% 25.5M 23s
 77950K .......... .......... .......... .......... .......... 29% 20.5M 23s
 78000K .......... .......... .......... .......... .......... 29% 18.2M 23s
 78050K .......... .......... .......... .......... .......... 29% 18.3M 23s
 78100K .......... .......... .......... .......... .......... 29% 19.6M 23s
 78150K .......... .......... .......... .......... .......... 29% 18.9M 23s
 78200K .......... .......... .......... .......... .......... 29% 12.4M 23s
 78250K .......... .......... .......... .......... .......... 29% 18.7M 23s
 78300K .......... .......... .......... .......... .......... 29% 11.5M 23s
 78350K .......... .......... .......... .......... .......... 29% 4.97M 23s
 78400K .......... .......... .......... .......... .......... 29% 21.1M 23s
 78450K .......... .......... .......... .......... .......... 29% 7.84M 23s
 78500K .......... .......... .......... .......... .......... 29% 12.5M 23s
 78550K .......... .......... .......... .......... .......... 29% 7.68M 23s
 78600K .......... .......... .......... .......... .......... 29% 4.82M 23s
 78650K .......... .......... .......... .......... .......... 30% 5.14M 23s
 78700K .......... .......... .......... .......... .......... 30% 3.99M 23s
 78750K .......... .......... .......... .......... .......... 30% 3.60M 23s
 78800K .......... .......... .......... .......... .......... 30% 3.58M 23s
 78850K .......... .......... .......... .......... .......... 30% 9.94M 23s
 78900K .......... .......... .......... .......... .......... 30% 13.3M 23s
 78950K .......... .......... .......... .......... .......... 30% 9.95M 23s
 79000K .......... .......... .......... .......... .......... 30% 11.7M 23s
 79050K .......... .......... .......... .......... .......... 30% 7.38M 23s
 79100K .......... .......... .......... .......... .......... 30% 6.13M 23s
 79150K .......... .......... .......... .......... .......... 30% 7.34M 23s
 79200K .......... .......... .......... .......... .......... 30% 5.17M 23s
 79250K .......... .......... .......... .......... .......... 30% 5.63M 23s
 79300K .......... .......... .......... .......... .......... 30% 3.87M 23s
 79350K .......... .......... .......... .......... .......... 30% 3.10M 23s
 79400K .......... .......... .......... .......... .......... 30% 3.89M 23s
 79450K .......... .......... .......... .......... .......... 30% 3.53M 23s
 79500K .......... .......... .......... .......... .......... 30% 5.10M 23s
 79550K .......... .......... .......... .......... .......... 30% 7.53M 23s
 79600K .......... .......... .......... .......... .......... 30% 5.80M 23s
 79650K .......... .......... .......... .......... .......... 30% 5.35M 23s
 79700K .......... .......... .......... .......... .......... 30% 4.45M 23s
 79750K .......... .......... .......... .......... .......... 30% 12.2M 23s
 79800K .......... .......... .......... .......... .......... 30% 13.4M 23s
 79850K .......... .......... .......... .......... .......... 30% 12.2M 23s
 79900K .......... .......... .......... .......... .......... 30% 13.4M 23s
 79950K .......... .......... .......... .......... .......... 30% 12.2M 23s
 80000K .......... .......... .......... .......... .......... 30% 12.3M 23s
 80050K .......... .......... .......... .......... .......... 30% 13.1M 23s
 80100K .......... .......... .......... .......... .......... 30% 9.05M 23s
 80150K .......... .......... .......... .......... .......... 30% 12.4M 23s
 80200K .......... .......... .......... .......... .......... 30% 6.84M 23s
 80250K .......... .......... .......... .......... .......... 30% 6.90M 23s
 80300K .......... .......... .......... .......... .......... 30% 7.07M 23s
 80350K .......... .......... .......... .......... .......... 30% 5.84M 23s
 80400K .......... .......... .......... .......... .......... 30% 5.60M 23s
 80450K .......... .......... .......... .......... .......... 30% 5.43M 23s
 80500K .......... .......... .......... .......... .......... 30% 6.25M 23s
 80550K .......... .......... .......... .......... .......... 30% 6.72M 23s
 80600K .......... .......... .......... .......... .......... 30% 5.19M 23s
 80650K .......... .......... .......... .......... .......... 30% 9.29M 23s
 80700K .......... .......... .......... .......... .......... 30% 16.3M 23s
 80750K .......... .......... .......... .......... .......... 30% 11.7M 23s
 80800K .......... .......... .......... .......... .......... 30% 14.1M 23s
 80850K .......... .......... .......... .......... .......... 30% 9.56M 23s
 80900K .......... .......... .......... .......... .......... 30% 9.71M 23s
 80950K .......... .......... .......... .......... .......... 30% 6.10M 23s
 81000K .......... .......... .......... .......... .......... 30% 8.29M 23s
 81050K .......... .......... .......... .......... .......... 30% 11.3M 23s
 81100K .......... .......... .......... .......... .......... 30% 3.90M 23s
 81150K .......... .......... .......... .......... .......... 30% 64.5M 23s
 81200K .......... .......... .......... .......... .......... 30% 4.11M 23s
 81250K .......... .......... .......... .......... .......... 31% 10.7M 23s
 81300K .......... .......... .......... .......... .......... 31% 3.31M 23s
 81350K .......... .......... .......... .......... .......... 31% 4.43M 23s
 81400K .......... .......... .......... .......... .......... 31% 2.75M 23s
 81450K .......... .......... .......... .......... .......... 31% 3.83M 23s
 81500K .......... .......... .......... .......... .......... 31% 4.69M 23s
 81550K .......... .......... .......... .......... .......... 31% 4.63M 23s
 81600K .......... .......... .......... .......... .......... 31% 2.24M 23s
 81650K .......... .......... .......... .......... .......... 31% 2.55M 23s
 81700K .......... .......... .......... .......... .......... 31% 1.01M 23s
 81750K .......... .......... .......... .......... .......... 31% 2.71M 23s
 81800K .......... .......... .......... .......... .......... 31% 3.95M 23s
 81850K .......... .......... .......... .......... .......... 31% 11.5M 23s
 81900K .......... .......... .......... .......... .......... 31% 13.4M 23s
 81950K .......... .......... .......... .......... .......... 31% 10.0M 23s
 82000K .......... .......... .......... .......... .......... 31% 12.3M 23s
 82050K .......... .......... .......... .......... .......... 31% 7.21M 23s
 82100K .......... .......... .......... .......... .......... 31% 8.68M 23s
 82150K .......... .......... .......... .......... .......... 31% 9.72M 23s
 82200K .......... .......... .......... .......... .......... 31% 6.87M 23s
 82250K .......... .......... .......... .......... .......... 31% 12.7M 23s
 82300K .......... .......... .......... .......... .......... 31% 7.95M 23s
 82350K .......... .......... .......... .......... .......... 31% 16.9M 23s
 82400K .......... .......... .......... .......... .......... 31% 8.91M 23s
 82450K .......... .......... .......... .......... .......... 31% 13.0M 23s
 82500K .......... .......... .......... .......... .......... 31% 15.1M 23s
 82550K .......... .......... .......... .......... .......... 31% 12.0M 23s
 82600K .......... .......... .......... .......... .......... 31% 13.2M 23s
 82650K .......... .......... .......... .......... .......... 31% 11.9M 23s
 82700K .......... .......... .......... .......... .......... 31% 10.9M 23s
 82750K .......... .......... .......... .......... .......... 31% 12.6M 23s
 82800K .......... .......... .......... .......... .......... 31% 7.52M 23s
 82850K .......... .......... .......... .......... .......... 31% 5.17M 23s
 82900K .......... .......... .......... .......... .......... 31% 6.20M 23s
 82950K .......... .......... .......... .......... .......... 31% 4.18M 23s
 83000K .......... .......... .......... .......... .......... 31% 5.00M 23s
 83050K .......... .......... .......... .......... .......... 31% 9.24M 23s
 83100K .......... .......... .......... .......... .......... 31% 18.3M 23s
 83150K .......... .......... .......... .......... .......... 31% 11.7M 23s
 83200K .......... .......... .......... .......... .......... 31% 12.6M 23s
 83250K .......... .......... .......... .......... .......... 31% 13.5M 23s
 83300K .......... .......... .......... .......... .......... 31% 9.44M 23s
 83350K .......... .......... .......... .......... .......... 31% 11.4M 23s
 83400K .......... .......... .......... .......... .......... 31% 11.3M 23s
 83450K .......... .......... .......... .......... .......... 31% 10.4M 23s
 83500K .......... .......... .......... .......... .......... 31% 13.3M 23s
 83550K .......... .......... .......... .......... .......... 31% 12.3M 23s
 83600K .......... .......... .......... .......... .......... 31% 7.67M 23s
 83650K .......... .......... .......... .......... .......... 31% 8.52M 23s
 83700K .......... .......... .......... .......... .......... 31% 5.59M 23s
 83750K .......... .......... .......... .......... .......... 31% 5.29M 23s
 83800K .......... .......... .......... .......... .......... 31% 5.34M 23s
 83850K .......... .......... .......... .......... .......... 31% 3.02M 23s
 83900K .......... .......... .......... .......... .......... 32% 4.63M 23s
 83950K .......... .......... .......... .......... .......... 32% 3.20M 23s
 84000K .......... .......... .......... .......... .......... 32% 6.44M 23s
 84050K .......... .......... .......... .......... .......... 32% 7.56M 23s
 84100K .......... .......... .......... .......... .......... 32% 8.62M 23s
 84150K .......... .......... .......... .......... .......... 32% 11.7M 23s
 84200K .......... .......... .......... .......... .......... 32% 7.92M 23s
 84250K .......... .......... .......... .......... .......... 32% 7.88M 23s
 84300K .......... .......... .......... .......... .......... 32% 9.30M 23s
 84350K .......... .......... .......... .......... .......... 32% 9.53M 23s
 84400K .......... .......... .......... .......... .......... 32% 11.8M 23s
 84450K .......... .......... .......... .......... .......... 32% 8.73M 23s
 84500K .......... .......... .......... .......... .......... 32% 10.9M 23s
 84550K .......... .......... .......... .......... .......... 32% 9.48M 23s
 84600K .......... .......... .......... .......... .......... 32% 14.8M 23s
 84650K .......... .......... .......... .......... .......... 32% 11.5M 23s
 84700K .......... .......... .......... .......... .......... 32% 9.10M 23s
 84750K .......... .......... .......... .......... .......... 32% 15.9M 23s
 84800K .......... .......... .......... .......... .......... 32% 15.4M 23s
 84850K .......... .......... .......... .......... .......... 32% 12.6M 23s
 84900K .......... .......... .......... .......... .......... 32% 10.4M 23s
 84950K .......... .......... .......... .......... .......... 32% 7.59M 23s
 85000K .......... .......... .......... .......... .......... 32% 7.64M 23s
 85050K .......... .......... .......... .......... .......... 32% 13.0M 23s
 85100K .......... .......... .......... .......... .......... 32% 11.6M 23s
 85150K .......... .......... .......... .......... .......... 32% 10.2M 23s
 85200K .......... .......... .......... .......... .......... 32% 12.0M 23s
 85250K .......... .......... .......... .......... .......... 32% 16.9M 23s
 85300K .......... .......... .......... .......... .......... 32% 8.64M 23s
 85350K .......... .......... .......... .......... .......... 32% 9.71M 23s
 85400K .......... .......... .......... .......... .......... 32% 11.8M 23s
 85450K .......... .......... .......... .......... .......... 32% 19.3M 23s
 85500K .......... .......... .......... .......... .......... 32% 24.7M 23s
 85550K .......... .......... .......... .......... .......... 32% 37.3M 23s
 85600K .......... .......... .......... .......... .......... 32% 17.3M 23s
 85650K .......... .......... .......... .......... .......... 32%  152M 23s
 85700K .......... .......... .......... .......... .......... 32% 18.5M 23s
 85750K .......... .......... .......... .......... .......... 32% 19.1M 23s
 85800K .......... .......... .......... .......... .......... 32% 28.0M 23s
 85850K .......... .......... .......... .......... .......... 32% 14.3M 23s
 85900K .......... .......... .......... .......... .......... 32% 27.3M 23s
 85950K .......... .......... .......... .......... .......... 32% 19.7M 22s
 86000K .......... .......... .......... .......... .......... 32% 16.2M 22s
 86050K .......... .......... .......... .......... .......... 32% 26.0M 22s
 86100K .......... .......... .......... .......... .......... 32% 16.4M 22s
 86150K .......... .......... .......... .......... .......... 32% 15.0M 22s
 86200K .......... .......... .......... .......... .......... 32% 13.9M 22s
 86250K .......... .......... .......... .......... .......... 32% 14.3M 22s
 86300K .......... .......... .......... .......... .......... 32% 12.3M 22s
 86350K .......... .......... .......... .......... .......... 32% 6.68M 22s
 86400K .......... .......... .......... .......... .......... 32% 6.22M 22s
 86450K .......... .......... .......... .......... .......... 32% 7.49M 22s
 86500K .......... .......... .......... .......... .......... 33% 5.49M 22s
 86550K .......... .......... .......... .......... .......... 33% 5.02M 22s
 86600K .......... .......... .......... .......... .......... 33% 9.41M 22s
 86650K .......... .......... .......... .......... .......... 33% 11.7M 22s
 86700K .......... .......... .......... .......... .......... 33% 14.4M 22s
 86750K .......... .......... .......... .......... .......... 33% 21.2M 22s
 86800K .......... .......... .......... .......... .......... 33% 19.0M 22s
 86850K .......... .......... .......... .......... .......... 33% 17.7M 22s
 86900K .......... .......... .......... .......... .......... 33% 15.4M 22s
 86950K .......... .......... .......... .......... .......... 33% 9.80M 22s
 87000K .......... .......... .......... .......... .......... 33% 8.33M 22s
 87050K .......... .......... .......... .......... .......... 33% 9.44M 22s
 87100K .......... .......... .......... .......... .......... 33% 6.76M 22s
 87150K .......... .......... .......... .......... .......... 33% 5.74M 22s
 87200K .......... .......... .......... .......... .......... 33% 6.19M 22s
 87250K .......... .......... .......... .......... .......... 33% 21.6M 22s
 87300K .......... .......... .......... .......... .......... 33% 19.2M 22s
 87350K .......... .......... .......... .......... .......... 33% 10.9M 22s
 87400K .......... .......... .......... .......... .......... 33% 34.0M 22s
 87450K .......... .......... .......... .......... .......... 33% 8.41M 22s
 87500K .......... .......... .......... .......... .......... 33% 16.7M 22s
 87550K .......... .......... .......... .......... .......... 33% 15.0M 22s
 87600K .......... .......... .......... .......... .......... 33% 8.57M 22s
 87650K .......... .......... .......... .......... .......... 33% 14.7M 22s
 87700K .......... .......... .......... .......... .......... 33% 37.4M 22s
 87750K .......... .......... .......... .......... .......... 33% 11.2M 22s
 87800K .......... .......... .......... .......... .......... 33% 11.6M 22s
 87850K .......... .......... .......... .......... .......... 33% 12.3M 22s
 87900K .......... .......... .......... .......... .......... 33% 17.1M 22s
 87950K .......... .......... .......... .......... .......... 33% 4.86M 22s
 88000K .......... .......... .......... .......... .......... 33%  223M 22s
 88050K .......... .......... .......... .......... .......... 33% 8.01M 22s
 88100K .......... .......... .......... .......... .......... 33% 6.74M 22s
 88150K .......... .......... .......... .......... .......... 33% 6.94M 22s
 88200K .......... .......... .......... .......... .......... 33% 5.59M 22s
 88250K .......... .......... .......... .......... .......... 33% 5.51M 22s
 88300K .......... .......... .......... .......... .......... 33% 4.31M 22s
 88350K .......... .......... .......... .......... .......... 33% 4.47M 22s
 88400K .......... .......... .......... .......... .......... 33% 4.58M 22s
 88450K .......... .......... .......... .......... .......... 33% 7.00M 22s
 88500K .......... .......... .......... .......... .......... 33% 14.6M 22s
 88550K .......... .......... .......... .......... .......... 33% 37.8M 22s
 88600K .......... .......... .......... .......... .......... 33% 16.9M 22s
 88650K .......... .......... .......... .......... .......... 33% 31.5M 22s
 88700K .......... .......... .......... .......... .......... 33% 13.7M 22s
 88750K .......... .......... .......... .......... .......... 33% 12.5M 22s
 88800K .......... .......... .......... .......... .......... 33% 16.7M 22s
 88850K .......... .......... .......... .......... .......... 33% 9.98M 22s
 88900K .......... .......... .......... .......... .......... 33% 8.93M 22s
 88950K .......... .......... .......... .......... .......... 33% 7.34M 22s
 89000K .......... .......... .......... .......... .......... 33% 9.58M 22s
 89050K .......... .......... .......... .......... .......... 33% 14.4M 22s
 89100K .......... .......... .......... .......... .......... 34% 8.01M 22s
 89150K .......... .......... .......... .......... .......... 34% 10.8M 22s
 89200K .......... .......... .......... .......... .......... 34% 13.7M 22s
 89250K .......... .......... .......... .......... .......... 34% 15.3M 22s
 89300K .......... .......... .......... .......... .......... 34% 67.8M 22s
 89350K .......... .......... .......... .......... .......... 34% 38.2M 22s
 89400K .......... .......... .......... .......... .......... 34% 63.9M 22s
 89450K .......... .......... .......... .......... .......... 34% 11.5M 22s
 89500K .......... .......... .......... .......... .......... 34% 50.4M 22s
 89550K .......... .......... .......... .......... .......... 34% 47.8M 22s
 89600K .......... .......... .......... .......... .......... 34% 67.6M 22s
 89650K .......... .......... .......... .......... .......... 34% 33.5M 22s
 89700K .......... .......... .......... .......... .......... 34% 22.7M 22s
 89750K .......... .......... .......... .......... .......... 34% 31.7M 22s
 89800K .......... .......... .......... .......... .......... 34% 24.3M 22s
 89850K .......... .......... .......... .......... .......... 34% 49.4M 22s
 89900K .......... .......... .......... .......... .......... 34% 36.6M 22s
 89950K .......... .......... .......... .......... .......... 34% 23.3M 22s
 90000K .......... .......... .......... .......... .......... 34% 23.7M 22s
 90050K .......... .......... .......... .......... .......... 34% 26.5M 22s
 90100K .......... .......... .......... .......... .......... 34% 19.2M 22s
 90150K .......... .......... .......... .......... .......... 34% 11.9M 22s
 90200K .......... .......... .......... .......... .......... 34% 14.8M 22s
 90250K .......... .......... .......... .......... .......... 34% 6.65M 22s
 90300K .......... .......... .......... .......... .......... 34% 52.9M 22s
 90350K .......... .......... .......... .......... .......... 34% 11.7M 22s
 90400K .......... .......... .......... .......... .......... 34% 12.2M 22s
 90450K .......... .......... .......... .......... .......... 34% 9.49M 22s
 90500K .......... .......... .......... .......... .......... 34% 20.7M 22s
 90550K .......... .......... .......... .......... .......... 34% 12.0M 22s
 90600K .......... .......... .......... .......... .......... 34% 12.7M 22s
 90650K .......... .......... .......... .......... .......... 34% 7.98M 22s
 90700K .......... .......... .......... .......... .......... 34% 10.7M 21s
 90750K .......... .......... .......... .......... .......... 34% 16.2M 21s
 90800K .......... .......... .......... .......... .......... 34% 15.3M 21s
 90850K .......... .......... .......... .......... .......... 34% 18.0M 21s
 90900K .......... .......... .......... .......... .......... 34% 7.97M 21s
 90950K .......... .......... .......... .......... .......... 34%  138M 21s
 91000K .......... .......... .......... .......... .......... 34%  149M 21s
 91050K .......... .......... .......... .......... .......... 34% 31.6M 21s
 91100K .......... .......... .......... .......... .......... 34% 15.8M 21s
 91150K .......... .......... .......... .......... .......... 34% 18.2M 21s
 91200K .......... .......... .......... .......... .......... 34% 12.0M 21s
 91250K .......... .......... .......... .......... .......... 34% 14.7M 21s
 91300K .......... .......... .......... .......... .......... 34% 20.1M 21s
 91350K .......... .......... .......... .......... .......... 34% 17.0M 21s
 91400K .......... .......... .......... .......... .......... 34% 17.3M 21s
 91450K .......... .......... .......... .......... .......... 34% 14.2M 21s
 91500K .......... .......... .......... .......... .......... 34% 15.5M 21s
 91550K .......... .......... .......... .......... .......... 34% 22.2M 21s
 91600K .......... .......... .......... .......... .......... 34% 21.9M 21s
 91650K .......... .......... .......... .......... .......... 34% 15.0M 21s
 91700K .......... .......... .......... .......... .......... 34% 15.1M 21s
 91750K .......... .......... .......... .......... .......... 35% 15.4M 21s
 91800K .......... .......... .......... .......... .......... 35% 27.4M 21s
 91850K .......... .......... .......... .......... .......... 35% 17.0M 21s
 91900K .......... .......... .......... .......... .......... 35% 35.9M 21s
 91950K .......... .......... .......... .......... .......... 35% 17.2M 21s
 92000K .......... .......... .......... .......... .......... 35% 22.2M 21s
 92050K .......... .......... .......... .......... .......... 35% 23.5M 21s
 92100K .......... .......... .......... .......... .......... 35% 15.6M 21s
 92150K .......... .......... .......... .......... .......... 35% 18.8M 21s
 92200K .......... .......... .......... .......... .......... 35% 14.3M 21s
 92250K .......... .......... .......... .......... .......... 35% 10.4M 21s
 92300K .......... .......... .......... .......... .......... 35% 13.7M 21s
 92350K .......... .......... .......... .......... .......... 35% 12.0M 21s
 92400K .......... .......... .......... .......... .......... 35% 5.85M 21s
 92450K .......... .......... .......... .......... .......... 35% 3.62M 21s
 92500K .......... .......... .......... .......... .......... 35% 3.85M 21s
 92550K .......... .......... .......... .......... .......... 35% 1.05M 21s
 92600K .......... .......... .......... .......... .......... 35% 1.68M 21s
 92650K .......... .......... .......... .......... .......... 35% 4.09M 21s
 92700K .......... .......... .......... .......... .......... 35% 6.11M 21s
 92750K .......... .......... .......... .......... .......... 35% 12.9M 21s
 92800K .......... .......... .......... .......... .......... 35% 11.9M 21s
 92850K .......... .......... .......... .......... .......... 35% 9.37M 21s
 92900K .......... .......... .......... .......... .......... 35% 13.1M 21s
 92950K .......... .......... .......... .......... .......... 35% 10.1M 21s
 93000K .......... .......... .......... .......... .......... 35% 9.24M 21s
 93050K .......... .......... .......... .......... .......... 35% 8.71M 21s
 93100K .......... .......... .......... .......... .......... 35% 8.21M 21s
 93150K .......... .......... .......... .......... .......... 35% 4.66M 21s
 93200K .......... .......... .......... .......... .......... 35% 5.03M 21s
 93250K .......... .......... .......... .......... .......... 35% 5.01M 21s
 93300K .......... .......... .......... .......... .......... 35% 11.2M 21s
 93350K .......... .......... .......... .......... .......... 35% 10.8M 21s
 93400K .......... .......... .......... .......... .......... 35% 10.0M 21s
 93450K .......... .......... .......... .......... .......... 35% 11.8M 21s
 93500K .......... .......... .......... .......... .......... 35% 11.5M 21s
 93550K .......... .......... .......... .......... .......... 35% 13.6M 21s
 93600K .......... .......... .......... .......... .......... 35% 9.15M 21s
 93650K .......... .......... .......... .......... .......... 35% 10.8M 21s
 93700K .......... .......... .......... .......... .......... 35% 3.54M 21s
 93750K .......... .......... .......... .......... .......... 35% 6.92M 21s
 93800K .......... .......... .......... .......... .......... 35% 7.86M 21s
 93850K .......... .......... .......... .......... .......... 35% 7.99M 21s
 93900K .......... .......... .......... .......... .......... 35% 8.22M 21s
 93950K .......... .......... .......... .......... .......... 35% 6.91M 21s
 94000K .......... .......... .......... .......... .......... 35% 10.5M 21s
 94050K .......... .......... .......... .......... .......... 35% 8.25M 21s
 94100K .......... .......... .......... .......... .......... 35% 5.86M 21s
 94150K .......... .......... .......... .......... .......... 35% 7.79M 21s
 94200K .......... .......... .......... .......... .......... 35% 6.26M 21s
 94250K .......... .......... .......... .......... .......... 35% 16.2M 21s
 94300K .......... .......... .......... .......... .......... 35% 24.5M 21s
 94350K .......... .......... .......... .......... .......... 36% 13.3M 21s
 94400K .......... .......... .......... .......... .......... 36% 19.5M 21s
 94450K .......... .......... .......... .......... .......... 36% 25.4M 21s
 94500K .......... .......... .......... .......... .......... 36% 11.8M 21s
 94550K .......... .......... .......... .......... .......... 36% 11.3M 21s
 94600K .......... .......... .......... .......... .......... 36% 7.94M 21s
 94650K .......... .......... .......... .......... .......... 36% 6.50M 21s
 94700K .......... .......... .......... .......... .......... 36% 6.11M 21s
 94750K .......... .......... .......... .......... .......... 36% 9.76M 21s
 94800K .......... .......... .......... .......... .......... 36% 8.02M 21s
 94850K .......... .......... .......... .......... .......... 36% 8.57M 21s
 94900K .......... .......... .......... .......... .......... 36% 9.27M 21s
 94950K .......... .......... .......... .......... .......... 36% 12.6M 21s
 95000K .......... .......... .......... .......... .......... 36% 22.0M 21s
 95050K .......... .......... .......... .......... .......... 36% 26.1M 21s
 95100K .......... .......... .......... .......... .......... 36% 14.6M 21s
 95150K .......... .......... .......... .......... .......... 36%  112M 21s
 95200K .......... .......... .......... .......... .......... 36% 15.3M 21s
 95250K .......... .......... .......... .......... .......... 36% 18.5M 21s
 95300K .......... .......... .......... .......... .......... 36% 31.6M 21s
 95350K .......... .......... .......... .......... .......... 36% 17.6M 21s
 95400K .......... .......... .......... .......... .......... 36% 16.6M 21s
 95450K .......... .......... .......... .......... .......... 36% 18.3M 21s
 95500K .......... .......... .......... .......... .......... 36% 16.9M 21s
 95550K .......... .......... .......... .......... .......... 36% 10.4M 21s
 95600K .......... .......... .......... .......... .......... 36% 9.51M 21s
 95650K .......... .......... .......... .......... .......... 36% 10.1M 21s
 95700K .......... .......... .......... .......... .......... 36% 5.86M 21s
 95750K .......... .......... .......... .......... .......... 36% 14.2M 21s
 95800K .......... .......... .......... .......... .......... 36% 9.55M 21s
 95850K .......... .......... .......... .......... .......... 36% 5.95M 21s
 95900K .......... .......... .......... .......... .......... 36% 6.51M 21s
 95950K .......... .......... .......... .......... .......... 36% 4.38M 21s
 96000K .......... .......... .......... .......... .......... 36% 4.35M 21s
 96050K .......... .......... .......... .......... .......... 36% 4.98M 21s
 96100K .......... .......... .......... .......... .......... 36% 4.37M 21s
 96150K .......... .......... .......... .......... .......... 36% 4.97M 21s
 96200K .......... .......... .......... .......... .......... 36% 5.29M 21s
 96250K .......... .......... .......... .......... .......... 36% 7.75M 21s
 96300K .......... .......... .......... .......... .......... 36% 16.6M 21s
 96350K .......... .......... .......... .......... .......... 36% 17.1M 21s
 96400K .......... .......... .......... .......... .......... 36% 38.6M 21s
 96450K .......... .......... .......... .......... .......... 36% 16.2M 21s
 96500K .......... .......... .......... .......... .......... 36% 24.5M 21s
 96550K .......... .......... .......... .......... .......... 36% 11.0M 21s
 96600K .......... .......... .......... .......... .......... 36% 16.5M 21s
 96650K .......... .......... .......... .......... .......... 36% 8.83M 21s
 96700K .......... .......... .......... .......... .......... 36% 6.85M 21s
 96750K .......... .......... .......... .......... .......... 36% 8.85M 21s
 96800K .......... .......... .......... .......... .......... 36% 8.10M 21s
 96850K .......... .......... .......... .......... .......... 36% 4.24M 21s
 96900K .......... .......... .......... .......... .......... 36% 4.21M 21s
 96950K .......... .......... .......... .......... .......... 36% 4.10M 21s
 97000K .......... .......... .......... .......... .......... 37% 4.90M 21s
 97050K .......... .......... .......... .......... .......... 37% 9.65M 21s
 97100K .......... .......... .......... .......... .......... 37% 12.7M 21s
 97150K .......... .......... .......... .......... .......... 37% 10.2M 21s
 97200K .......... .......... .......... .......... .......... 37% 12.3M 21s
 97250K .......... .......... .......... .......... .......... 37% 10.1M 21s
 97300K .......... .......... .......... .......... .......... 37% 13.4M 21s
 97350K .......... .......... .......... .......... .......... 37% 13.9M 21s
 97400K .......... .......... .......... .......... .......... 37% 10.9M 20s
 97450K .......... .......... .......... .......... .......... 37% 20.4M 20s
 97500K .......... .......... .......... .......... .......... 37% 14.0M 20s
 97550K .......... .......... .......... .......... .......... 37% 23.8M 20s
 97600K .......... .......... .......... .......... .......... 37% 20.5M 20s
 97650K .......... .......... .......... .......... .......... 37% 86.2M 20s
 97700K .......... .......... .......... .......... .......... 37% 11.5M 20s
 97750K .......... .......... .......... .......... .......... 37% 36.9M 20s
 97800K .......... .......... .......... .......... .......... 37% 15.1M 20s
 97850K .......... .......... .......... .......... .......... 37% 12.0M 20s
 97900K .......... .......... .......... .......... .......... 37% 13.6M 20s
 97950K .......... .......... .......... .......... .......... 37% 18.0M 20s
 98000K .......... .......... .......... .......... .......... 37% 15.8M 20s
 98050K .......... .......... .......... .......... .......... 37% 13.8M 20s
 98100K .......... .......... .......... .......... .......... 37% 10.7M 20s
 98150K .......... .......... .......... .......... .......... 37% 12.4M 20s
 98200K .......... .......... .......... .......... .......... 37% 12.5M 20s
 98250K .......... .......... .......... .......... .......... 37% 12.0M 20s
 98300K .......... .......... .......... .......... .......... 37% 11.1M 20s
 98350K .......... .......... .......... .......... .......... 37% 59.9M 20s
 98400K .......... .......... .......... .......... .......... 37% 21.5M 20s
 98450K .......... .......... .......... .......... .......... 37% 17.7M 20s
 98500K .......... .......... .......... .......... .......... 37% 16.5M 20s
 98550K .......... .......... .......... .......... .......... 37% 25.0M 20s
 98600K .......... .......... .......... .......... .......... 37% 10.1M 20s
 98650K .......... .......... .......... .......... .......... 37% 29.0M 20s
 98700K .......... .......... .......... .......... .......... 37% 22.3M 20s
 98750K .......... .......... .......... .......... .......... 37% 15.1M 20s
 98800K .......... .......... .......... .......... .......... 37% 21.7M 20s
 98850K .......... .......... .......... .......... .......... 37% 10.5M 20s
 98900K .......... .......... .......... .......... .......... 37% 11.6M 20s
 98950K .......... .......... .......... .......... .......... 37% 7.02M 20s
 99000K .......... .......... .......... .......... .......... 37% 9.34M 20s
 99050K .......... .......... .......... .......... .......... 37% 7.74M 20s
 99100K .......... .......... .......... .......... .......... 37% 7.26M 20s
 99150K .......... .......... .......... .......... .......... 37% 10.3M 20s
 99200K .......... .......... .......... .......... .......... 37% 7.99M 20s
 99250K .......... .......... .......... .......... .......... 37% 10.0M 20s
 99300K .......... .......... .......... .......... .......... 37% 14.0M 20s
 99350K .......... .......... .......... .......... .......... 37% 8.82M 20s
 99400K .......... .......... .......... .......... .......... 37% 33.4M 20s
 99450K .......... .......... .......... .......... .......... 37% 12.0M 20s
 99500K .......... .......... .......... .......... .......... 37% 11.7M 20s
 99550K .......... .......... .......... .......... .......... 37% 14.2M 20s
 99600K .......... .......... .......... .......... .......... 38% 8.88M 20s
 99650K .......... .......... .......... .......... .......... 38% 6.32M 20s
 99700K .......... .......... .......... .......... .......... 38% 8.47M 20s
 99750K .......... .......... .......... .......... .......... 38% 7.07M 20s
 99800K .......... .......... .......... .......... .......... 38% 6.76M 20s
 99850K .......... .......... .......... .......... .......... 38% 6.17M 20s
 99900K .......... .......... .......... .......... .......... 38% 6.03M 20s
 99950K .......... .......... .......... .......... .......... 38% 6.32M 20s
100000K .......... .......... .......... .......... .......... 38% 6.72M 20s
100050K .......... .......... .......... .......... .......... 38% 6.23M 20s
100100K .......... .......... .......... .......... .......... 38% 7.01M 20s
100150K .......... .......... .......... .......... .......... 38% 7.19M 20s
100200K .......... .......... .......... .......... .......... 38% 8.12M 20s
100250K .......... .......... .......... .......... .......... 38% 11.2M 20s
100300K .......... .......... .......... .......... .......... 38% 11.2M 20s
100350K .......... .......... .......... .......... .......... 38% 7.81M 20s
100400K .......... .......... .......... .......... .......... 38% 10.2M 20s
100450K .......... .......... .......... .......... .......... 38% 7.06M 20s
100500K .......... .......... .......... .......... .......... 38% 8.84M 20s
100550K .......... .......... .......... .......... .......... 38% 11.1M 20s
100600K .......... .......... .......... .......... .......... 38% 5.83M 20s
100650K .......... .......... .......... .......... .......... 38% 10.6M 20s
100700K .......... .......... .......... .......... .......... 38% 7.04M 20s
100750K .......... .......... .......... .......... .......... 38% 7.68M 20s
100800K .......... .......... .......... .......... .......... 38% 6.89M 20s
100850K .......... .......... .......... .......... .......... 38% 7.18M 20s
100900K .......... .......... .......... .......... .......... 38% 7.05M 20s
100950K .......... .......... .......... .......... .......... 38% 5.59M 20s
101000K .......... .......... .......... .......... .......... 38% 6.23M 20s
101050K .......... .......... .......... .......... .......... 38% 9.87M 20s
101100K .......... .......... .......... .......... .......... 38% 26.8M 20s
101150K .......... .......... .......... .......... .......... 38% 11.2M 20s
101200K .......... .......... .......... .......... .......... 38% 8.34M 20s
101250K .......... .......... .......... .......... .......... 38% 16.2M 20s
101300K .......... .......... .......... .......... .......... 38% 8.34M 20s
101350K .......... .......... .......... .......... .......... 38% 6.31M 20s
101400K .......... .......... .......... .......... .......... 38% 8.64M 20s
101450K .......... .......... .......... .......... .......... 38% 7.36M 20s
101500K .......... .......... .......... .......... .......... 38% 9.75M 20s
101550K .......... .......... .......... .......... .......... 38% 9.84M 20s
101600K .......... .......... .......... .......... .......... 38% 5.19M 20s
101650K .......... .......... .......... .......... .......... 38% 5.08M 20s
101700K .......... .......... .......... .......... .......... 38% 5.24M 20s
101750K .......... .......... .......... .......... .......... 38% 5.05M 20s
101800K .......... .......... .......... .......... .......... 38% 4.43M 20s
101850K .......... .......... .......... .......... .......... 38% 4.10M 20s
101900K .......... .......... .......... .......... .......... 38% 5.39M 20s
101950K .......... .......... .......... .......... .......... 38% 6.25M 20s
102000K .......... .......... .......... .......... .......... 38% 5.83M 20s
102050K .......... .......... .......... .......... .......... 38% 5.66M 20s
102100K .......... .......... .......... .......... .......... 38% 5.48M 20s
102150K .......... .......... .......... .......... .......... 38% 10.2M 20s
102200K .......... .......... .......... .......... .......... 38% 8.09M 20s
102250K .......... .......... .......... .......... .......... 39% 10.1M 20s
102300K .......... .......... .......... .......... .......... 39% 9.70M 20s
102350K .......... .......... .......... .......... .......... 39% 8.59M 20s
102400K .......... .......... .......... .......... .......... 39% 11.0M 20s
102450K .......... .......... .......... .......... .......... 39% 16.2M 20s
102500K .......... .......... .......... .......... .......... 39% 10.7M 20s
102550K .......... .......... .......... .......... .......... 39% 20.7M 20s
102600K .......... .......... .......... .......... .......... 39% 17.8M 20s
102650K .......... .......... .......... .......... .......... 39% 13.7M 20s
102700K .......... .......... .......... .......... .......... 39% 9.93M 20s
102750K .......... .......... .......... .......... .......... 39% 8.88M 20s
102800K .......... .......... .......... .......... .......... 39% 11.2M 20s
102850K .......... .......... .......... .......... .......... 39% 8.27M 20s
102900K .......... .......... .......... .......... .......... 39% 9.89M 20s
102950K .......... .......... .......... .......... .......... 39% 10.4M 20s
103000K .......... .......... .......... .......... .......... 39% 9.10M 20s
103050K .......... .......... .......... .......... .......... 39% 5.78M 20s
103100K .......... .......... .......... .......... .......... 39% 10.1M 20s
103150K .......... .......... .......... .......... .......... 39% 10.4M 20s
103200K .......... .......... .......... .......... .......... 39% 9.24M 20s
103250K .......... .......... .......... .......... .......... 39% 11.6M 20s
103300K .......... .......... .......... .......... .......... 39% 9.18M 20s
103350K .......... .......... .......... .......... .......... 39% 9.75M 20s
103400K .......... .......... .......... .......... .......... 39% 9.98M 20s
103450K .......... .......... .......... .......... .......... 39% 6.45M 20s
103500K .......... .......... .......... .......... .......... 39% 6.42M 20s
103550K .......... .......... .......... .......... .......... 39% 4.98M 20s
103600K .......... .......... .......... .......... .......... 39% 5.24M 20s
103650K .......... .......... .......... .......... .......... 39% 7.77M 20s
103700K .......... .......... .......... .......... .......... 39% 11.5M 20s
103750K .......... .......... .......... .......... .......... 39% 13.1M 20s
103800K .......... .......... .......... .......... .......... 39% 12.2M 20s
103850K .......... .......... .......... .......... .......... 39% 10.4M 20s
103900K .......... .......... .......... .......... .......... 39% 11.9M 20s
103950K .......... .......... .......... .......... .......... 39% 8.42M 19s
104000K .......... .......... .......... .......... .......... 39% 9.01M 19s
104050K .......... .......... .......... .......... .......... 39% 10.1M 19s
104100K .......... .......... .......... .......... .......... 39% 8.79M 19s
104150K .......... .......... .......... .......... .......... 39% 9.80M 19s
104200K .......... .......... .......... .......... .......... 39% 7.47M 19s
104250K .......... .......... .......... .......... .......... 39% 10.8M 19s
104300K .......... .......... .......... .......... .......... 39% 10.2M 19s
104350K .......... .......... .......... .......... .......... 39% 5.01M 19s
104400K .......... .......... .......... .......... .......... 39% 7.27M 19s
104450K .......... .......... .......... .......... .......... 39% 4.23M 19s
104500K .......... .......... .......... .......... .......... 39% 8.06M 19s
104550K .......... .......... .......... .......... .......... 39% 6.92M 19s
104600K .......... .......... .......... .......... .......... 39% 5.37M 19s
104650K .......... .......... .......... .......... .......... 39% 6.12M 19s
104700K .......... .......... .......... .......... .......... 39% 5.73M 19s
104750K .......... .......... .......... .......... .......... 39% 7.90M 19s
104800K .......... .......... .......... .......... .......... 39% 7.23M 19s
104850K .......... .......... .......... .......... .......... 40% 7.02M 19s
104900K .......... .......... .......... .......... .......... 40% 18.7M 19s
104950K .......... .......... .......... .......... .......... 40% 14.8M 19s
105000K .......... .......... .......... .......... .......... 40% 15.0M 19s
105050K .......... .......... .......... .......... .......... 40% 15.2M 19s
105100K .......... .......... .......... .......... .......... 40% 14.6M 19s
105150K .......... .......... .......... .......... .......... 40% 14.1M 19s
105200K .......... .......... .......... .......... .......... 40% 9.11M 19s
105250K .......... .......... .......... .......... .......... 40% 9.10M 19s
105300K .......... .......... .......... .......... .......... 40% 10.7M 19s
105350K .......... .......... .......... .......... .......... 40% 8.57M 19s
105400K .......... .......... .......... .......... .......... 40% 9.78M 19s
105450K .......... .......... .......... .......... .......... 40% 9.33M 19s
105500K .......... .......... .......... .......... .......... 40% 7.67M 19s
105550K .......... .......... .......... .......... .......... 40% 8.11M 19s
105600K .......... .......... .......... .......... .......... 40% 5.38M 19s
105650K .......... .......... .......... .......... .......... 40% 6.71M 19s
105700K .......... .......... .......... .......... .......... 40% 5.43M 19s
105750K .......... .......... .......... .......... .......... 40% 7.78M 19s
105800K .......... .......... .......... .......... .......... 40% 7.58M 19s
105850K .......... .......... .......... .......... .......... 40% 7.00M 19s
105900K .......... .......... .......... .......... .......... 40% 9.17M 19s
105950K .......... .......... .......... .......... .......... 40% 15.4M 19s
106000K .......... .......... .......... .......... .......... 40% 17.6M 19s
106050K .......... .......... .......... .......... .......... 40% 13.8M 19s
106100K .......... .......... .......... .......... .......... 40% 12.7M 19s
106150K .......... .......... .......... .......... .......... 40% 13.0M 19s
106200K .......... .......... .......... .......... .......... 40% 11.6M 19s
106250K .......... .......... .......... .......... .......... 40% 18.1M 19s
106300K .......... .......... .......... .......... .......... 40% 11.5M 19s
106350K .......... .......... .......... .......... .......... 40% 6.79M 19s
106400K .......... .......... .......... .......... .......... 40% 7.94M 19s
106450K .......... .......... .......... .......... .......... 40% 6.88M 19s
106500K .......... .......... .......... .......... .......... 40% 9.04M 19s
106550K .......... .......... .......... .......... .......... 40% 7.09M 19s
106600K .......... .......... .......... .......... .......... 40% 3.11M 19s
106650K .......... .......... .......... .......... .......... 40% 3.71M 19s
106700K .......... .......... .......... .......... .......... 40% 3.20M 19s
106750K .......... .......... .......... .......... .......... 40% 8.08M 19s
106800K .......... .......... .......... .......... .......... 40% 5.25M 19s
106850K .......... .......... .......... .......... .......... 40% 4.21M 19s
106900K .......... .......... .......... .......... .......... 40% 5.16M 19s
106950K .......... .......... .......... .......... .......... 40% 3.75M 19s
107000K .......... .......... .......... .......... .......... 40% 4.04M 19s
107050K .......... .......... .......... .......... .......... 40% 3.60M 19s
107100K .......... .......... .......... .......... .......... 40% 3.54M 19s
107150K .......... .......... .......... .......... .......... 40% 4.22M 19s
107200K .......... .......... .......... .......... .......... 40% 4.19M 19s
107250K .......... .......... .......... .......... .......... 40% 5.83M 19s
107300K .......... .......... .......... .......... .......... 40% 6.20M 19s
107350K .......... .......... .......... .......... .......... 40% 4.92M 19s
107400K .......... .......... .......... .......... .......... 40% 9.04M 19s
107450K .......... .......... .......... .......... .......... 41% 10.4M 19s
107500K .......... .......... .......... .......... .......... 41% 12.6M 19s
107550K .......... .......... .......... .......... .......... 41% 12.4M 19s
107600K .......... .......... .......... .......... .......... 41% 11.9M 19s
107650K .......... .......... .......... .......... .......... 41% 15.0M 19s
107700K .......... .......... .......... .......... .......... 41% 10.3M 19s
107750K .......... .......... .......... .......... .......... 41% 12.7M 19s
107800K .......... .......... .......... .......... .......... 41% 6.79M 19s
107850K .......... .......... .......... .......... .......... 41% 8.18M 19s
107900K .......... .......... .......... .......... .......... 41% 6.35M 19s
107950K .......... .......... .......... .......... .......... 41% 5.86M 19s
108000K .......... .......... .......... .......... .......... 41% 5.90M 19s
108050K .......... .......... .......... .......... .......... 41% 5.62M 19s
108100K .......... .......... .......... .......... .......... 41% 10.2M 19s
108150K .......... .......... .......... .......... .......... 41% 19.2M 19s
108200K .......... .......... .......... .......... .......... 41% 10.6M 19s
108250K .......... .......... .......... .......... .......... 41% 7.98M 19s
108300K .......... .......... .......... .......... .......... 41% 14.3M 19s
108350K .......... .......... .......... .......... .......... 41% 4.79M 19s
108400K .......... .......... .......... .......... .......... 41% 7.72M 19s
108450K .......... .......... .......... .......... .......... 41% 4.88M 19s
108500K .......... .......... .......... .......... .......... 41% 6.54M 19s
108550K .......... .......... .......... .......... .......... 41% 7.44M 19s
108600K .......... .......... .......... .......... .......... 41% 6.10M 19s
108650K .......... .......... .......... .......... .......... 41% 42.5M 19s
108700K .......... .......... .......... .......... .......... 41% 9.04M 19s
108750K .......... .......... .......... .......... .......... 41% 9.85M 19s
108800K .......... .......... .......... .......... .......... 41% 12.9M 19s
108850K .......... .......... .......... .......... .......... 41% 6.57M 19s
108900K .......... .......... .......... .......... .......... 41% 6.13M 19s
108950K .......... .......... .......... .......... .......... 41% 4.66M 19s
109000K .......... .......... .......... .......... .......... 41% 6.98M 19s
109050K .......... .......... .......... .......... .......... 41% 9.89M 19s
109100K .......... .......... .......... .......... .......... 41% 10.6M 19s
109150K .......... .......... .......... .......... .......... 41% 17.8M 19s
109200K .......... .......... .......... .......... .......... 41% 9.76M 19s
109250K .......... .......... .......... .......... .......... 41% 16.1M 19s
109300K .......... .......... .......... .......... .......... 41% 10.6M 19s
109350K .......... .......... .......... .......... .......... 41% 16.7M 19s
109400K .......... .......... .......... .......... .......... 41% 6.50M 19s
109450K .......... .......... .......... .......... .......... 41% 22.2M 19s
109500K .......... .......... .......... .......... .......... 41% 9.16M 19s
109550K .......... .......... .......... .......... .......... 41% 9.64M 19s
109600K .......... .......... .......... .......... .......... 41% 6.81M 19s
109650K .......... .......... .......... .......... .......... 41% 4.88M 19s
109700K .......... .......... .......... .......... .......... 41% 3.31M 19s
109750K .......... .......... .......... .......... .......... 41% 4.19M 19s
109800K .......... .......... .......... .......... .......... 41% 4.33M 19s
109850K .......... .......... .......... .......... .......... 41% 5.42M 19s
109900K .......... .......... .......... .......... .......... 41% 8.12M 19s
109950K .......... .......... .......... .......... .......... 41% 7.22M 19s
110000K .......... .......... .......... .......... .......... 41% 5.33M 19s
110050K .......... .......... .......... .......... .......... 41% 12.6M 19s
110100K .......... .......... .......... .......... .......... 42% 8.63M 19s
110150K .......... .......... .......... .......... .......... 42% 11.4M 19s
110200K .......... .......... .......... .......... .......... 42% 6.25M 19s
110250K .......... .......... .......... .......... .......... 42% 10.7M 19s
110300K .......... .......... .......... .......... .......... 42% 10.1M 19s
110350K .......... .......... .......... .......... .......... 42% 9.48M 19s
110400K .......... .......... .......... .......... .......... 42% 10.5M 19s
110450K .......... .......... .......... .......... .......... 42% 8.27M 19s
110500K .......... .......... .......... .......... .......... 42% 8.48M 19s
110550K .......... .......... .......... .......... .......... 42% 7.21M 19s
110600K .......... .......... .......... .......... .......... 42% 10.2M 19s
110650K .......... .......... .......... .......... .......... 42% 12.2M 19s
110700K .......... .......... .......... .......... .......... 42% 5.18M 19s
110750K .......... .......... .......... .......... .......... 42% 5.22M 19s
110800K .......... .......... .......... .......... .......... 42% 4.11M 19s
110850K .......... .......... .......... .......... .......... 42% 4.26M 19s
110900K .......... .......... .......... .......... .......... 42% 4.55M 19s
110950K .......... .......... .......... .......... .......... 42% 4.00M 19s
111000K .......... .......... .......... .......... .......... 42% 10.3M 19s
111050K .......... .......... .......... .......... .......... 42% 14.1M 19s
111100K .......... .......... .......... .......... .......... 42% 13.5M 19s
111150K .......... .......... .......... .......... .......... 42% 12.2M 19s
111200K .......... .......... .......... .......... .......... 42% 8.33M 19s
111250K .......... .......... .......... .......... .......... 42% 9.42M 19s
111300K .......... .......... .......... .......... .......... 42% 8.74M 19s
111350K .......... .......... .......... .......... .......... 42% 6.90M 19s
111400K .......... .......... .......... .......... .......... 42% 8.23M 19s
111450K .......... .......... .......... .......... .......... 42% 6.55M 19s
111500K .......... .......... .......... .......... .......... 42% 8.26M 19s
111550K .......... .......... .......... .......... .......... 42% 5.22M 19s
111600K .......... .......... .......... .......... .......... 42% 4.28M 19s
111650K .......... .......... .......... .......... .......... 42% 6.57M 19s
111700K .......... .......... .......... .......... .......... 42% 3.64M 19s
111750K .......... .......... .......... .......... .......... 42% 4.52M 19s
111800K .......... .......... .......... .......... .......... 42% 3.60M 19s
111850K .......... .......... .......... .......... .......... 42% 5.28M 19s
111900K .......... .......... .......... .......... .......... 42% 11.1M 19s
111950K .......... .......... .......... .......... .......... 42% 8.61M 19s
112000K .......... .......... .......... .......... .......... 42% 14.8M 19s
112050K .......... .......... .......... .......... .......... 42% 10.2M 19s
112100K .......... .......... .......... .......... .......... 42% 7.12M 19s
112150K .......... .......... .......... .......... .......... 42% 8.13M 19s
112200K .......... .......... .......... .......... .......... 42% 6.76M 19s
112250K .......... .......... .......... .......... .......... 42% 10.3M 19s
112300K .......... .......... .......... .......... .......... 42% 8.77M 19s
112350K .......... .......... .......... .......... .......... 42% 7.45M 19s
112400K .......... .......... .......... .......... .......... 42% 8.66M 19s
112450K .......... .......... .......... .......... .......... 42% 10.7M 19s
112500K .......... .......... .......... .......... .......... 42% 7.06M 19s
112550K .......... .......... .......... .......... .......... 42% 8.44M 19s
112600K .......... .......... .......... .......... .......... 42% 6.31M 19s
112650K .......... .......... .......... .......... .......... 42% 5.43M 19s
112700K .......... .......... .......... .......... .......... 43% 5.21M 19s
112750K .......... .......... .......... .......... .......... 43% 7.06M 19s
112800K .......... .......... .......... .......... .......... 43% 7.37M 19s
112850K .......... .......... .......... .......... .......... 43% 11.3M 19s
112900K .......... .......... .......... .......... .......... 43% 38.5M 19s
112950K .......... .......... .......... .......... .......... 43% 19.2M 19s
113000K .......... .......... .......... .......... .......... 43% 30.1M 19s
113050K .......... .......... .......... .......... .......... 43% 14.5M 18s
113100K .......... .......... .......... .......... .......... 43% 23.3M 18s
113150K .......... .......... .......... .......... .......... 43% 20.3M 18s
113200K .......... .......... .......... .......... .......... 43% 27.8M 18s
113250K .......... .......... .......... .......... .......... 43% 26.5M 18s
113300K .......... .......... .......... .......... .......... 43% 18.1M 18s
113350K .......... .......... .......... .......... .......... 43% 13.3M 18s
113400K .......... .......... .......... .......... .......... 43% 26.2M 18s
113450K .......... .......... .......... .......... .......... 43% 10.3M 18s
113500K .......... .......... .......... .......... .......... 43% 9.38M 18s
113550K .......... .......... .......... .......... .......... 43% 10.6M 18s
113600K .......... .......... .......... .......... .......... 43% 10.0M 18s
113650K .......... .......... .......... .......... .......... 43% 9.93M 18s
113700K .......... .......... .......... .......... .......... 43% 8.82M 18s
113750K .......... .......... .......... .......... .......... 43% 12.1M 18s
113800K .......... .......... .......... .......... .......... 43% 11.1M 18s
113850K .......... .......... .......... .......... .......... 43% 10.8M 18s
113900K .......... .......... .......... .......... .......... 43% 15.1M 18s
113950K .......... .......... .......... .......... .......... 43% 25.1M 18s
114000K .......... .......... .......... .......... .......... 43% 25.7M 18s
114050K .......... .......... .......... .......... .......... 43% 26.6M 18s
114100K .......... .......... .......... .......... .......... 43% 13.6M 18s
114150K .......... .......... .......... .......... .......... 43% 25.1M 18s
114200K .......... .......... .......... .......... .......... 43% 19.6M 18s
114250K .......... .......... .......... .......... .......... 43% 14.5M 18s
114300K .......... .......... .......... .......... .......... 43% 10.8M 18s
114350K .......... .......... .......... .......... .......... 43% 17.6M 18s
114400K .......... .......... .......... .......... .......... 43% 7.59M 18s
114450K .......... .......... .......... .......... .......... 43% 13.5M 18s
114500K .......... .......... .......... .......... .......... 43% 8.55M 18s
114550K .......... .......... .......... .......... .......... 43% 8.04M 18s
114600K .......... .......... .......... .......... .......... 43% 6.53M 18s
114650K .......... .......... .......... .......... .......... 43% 5.06M 18s
114700K .......... .......... .......... .......... .......... 43% 4.88M 18s
114750K .......... .......... .......... .......... .......... 43% 5.03M 18s
114800K .......... .......... .......... .......... .......... 43% 5.10M 18s
114850K .......... .......... .......... .......... .......... 43% 4.39M 18s
114900K .......... .......... .......... .......... .......... 43% 5.44M 18s
114950K .......... .......... .......... .......... .......... 43% 3.36M 18s
115000K .......... .......... .......... .......... .......... 43% 4.57M 18s
115050K .......... .......... .......... .......... .......... 43% 10.0M 18s
115100K .......... .......... .......... .......... .......... 43% 10.1M 18s
115150K .......... .......... .......... .......... .......... 43% 32.4M 18s
115200K .......... .......... .......... .......... .......... 43% 20.8M 18s
115250K .......... .......... .......... .......... .......... 43% 16.1M 18s
115300K .......... .......... .......... .......... .......... 43% 22.4M 18s
115350K .......... .......... .......... .......... .......... 44% 16.3M 18s
115400K .......... .......... .......... .......... .......... 44% 11.5M 18s
115450K .......... .......... .......... .......... .......... 44% 19.2M 18s
115500K .......... .......... .......... .......... .......... 44% 12.9M 18s
115550K .......... .......... .......... .......... .......... 44% 18.0M 18s
115600K .......... .......... .......... .......... .......... 44% 14.8M 18s
115650K .......... .......... .......... .......... .......... 44% 12.1M 18s
115700K .......... .......... .......... .......... .......... 44% 9.40M 18s
115750K .......... .......... .......... .......... .......... 44% 9.00M 18s
115800K .......... .......... .......... .......... .......... 44% 10.7M 18s
115850K .......... .......... .......... .......... .......... 44% 8.35M 18s
115900K .......... .......... .......... .......... .......... 44% 4.66M 18s
115950K .......... .......... .......... .......... .......... 44% 4.45M 18s
116000K .......... .......... .......... .......... .......... 44% 4.46M 18s
116050K .......... .......... .......... .......... .......... 44% 3.61M 18s
116100K .......... .......... .......... .......... .......... 44% 3.98M 18s
116150K .......... .......... .......... .......... .......... 44% 4.08M 18s
116200K .......... .......... .......... .......... .......... 44% 4.01M 18s
116250K .......... .......... .......... .......... .......... 44% 14.7M 18s
116300K .......... .......... .......... .......... .......... 44% 13.2M 18s
116350K .......... .......... .......... .......... .......... 44% 9.58M 18s
116400K .......... .......... .......... .......... .......... 44% 8.37M 18s
116450K .......... .......... .......... .......... .......... 44% 7.24M 18s
116500K .......... .......... .......... .......... .......... 44% 6.31M 18s
116550K .......... .......... .......... .......... .......... 44% 6.56M 18s
116600K .......... .......... .......... .......... .......... 44% 5.11M 18s
116650K .......... .......... .......... .......... .......... 44% 6.69M 18s
116700K .......... .......... .......... .......... .......... 44% 4.79M 18s
116750K .......... .......... .......... .......... .......... 44% 8.32M 18s
116800K .......... .......... .......... .......... .......... 44% 21.1M 18s
116850K .......... .......... .......... .......... .......... 44% 6.96M 18s
116900K .......... .......... .......... .......... .......... 44% 10.7M 18s
116950K .......... .......... .......... .......... .......... 44% 5.82M 18s
117000K .......... .......... .......... .......... .......... 44% 7.07M 18s
117050K .......... .......... .......... .......... .......... 44% 8.96M 18s
117100K .......... .......... .......... .......... .......... 44% 5.79M 18s
117150K .......... .......... .......... .......... .......... 44% 7.54M 18s
117200K .......... .......... .......... .......... .......... 44% 6.39M 18s
117250K .......... .......... .......... .......... .......... 44% 15.6M 18s
117300K .......... .......... .......... .......... .......... 44% 11.6M 18s
117350K .......... .......... .......... .......... .......... 44% 8.86M 18s
117400K .......... .......... .......... .......... .......... 44% 8.37M 18s
117450K .......... .......... .......... .......... .......... 44% 8.11M 18s
117500K .......... .......... .......... .......... .......... 44% 8.96M 18s
117550K .......... .......... .......... .......... .......... 44% 13.4M 18s
117600K .......... .......... .......... .......... .......... 44% 7.10M 18s
117650K .......... .......... .......... .......... .......... 44% 7.56M 18s
117700K .......... .......... .......... .......... .......... 44% 5.23M 18s
117750K .......... .......... .......... .......... .......... 44% 8.82M 18s
117800K .......... .......... .......... .......... .......... 44% 6.60M 18s
117850K .......... .......... .......... .......... .......... 44% 9.56M 18s
117900K .......... .......... .......... .......... .......... 44% 15.1M 18s
117950K .......... .......... .......... .......... .......... 45% 15.8M 18s
118000K .......... .......... .......... .......... .......... 45% 15.8M 18s
118050K .......... .......... .......... .......... .......... 45% 16.7M 18s
118100K .......... .......... .......... .......... .......... 45% 14.5M 18s
118150K .......... .......... .......... .......... .......... 45% 13.5M 18s
118200K .......... .......... .......... .......... .......... 45% 17.7M 18s
118250K .......... .......... .......... .......... .......... 45% 14.9M 18s
118300K .......... .......... .......... .......... .......... 45% 14.1M 18s
118350K .......... .......... .......... .......... .......... 45% 11.2M 18s
118400K .......... .......... .......... .......... .......... 45% 8.65M 18s
118450K .......... .......... .......... .......... .......... 45% 4.14M 18s
118500K .......... .......... .......... .......... .......... 45% 5.91M 18s
118550K .......... .......... .......... .......... .......... 45% 7.03M 18s
118600K .......... .......... .......... .......... .......... 45% 12.1M 18s
118650K .......... .......... .......... .......... .......... 45% 23.7M 18s
118700K .......... .......... .......... .......... .......... 45% 12.1M 18s
118750K .......... .......... .......... .......... .......... 45% 33.2M 18s
118800K .......... .......... .......... .......... .......... 45% 19.5M 18s
118850K .......... .......... .......... .......... .......... 45% 9.12M 18s
118900K .......... .......... .......... .......... .......... 45% 11.2M 18s
118950K .......... .......... .......... .......... .......... 45% 8.28M 18s
119000K .......... .......... .......... .......... .......... 45% 10.8M 18s
119050K .......... .......... .......... .......... .......... 45% 12.0M 18s
119100K .......... .......... .......... .......... .......... 45% 11.0M 18s
119150K .......... .......... .......... .......... .......... 45% 10.7M 18s
119200K .......... .......... .......... .......... .......... 45% 8.85M 18s
119250K .......... .......... .......... .......... .......... 45% 9.60M 18s
119300K .......... .......... .......... .......... .......... 45% 9.70M 18s
119350K .......... .......... .......... .......... .......... 45% 5.93M 18s
119400K .......... .......... .......... .......... .......... 45% 9.50M 18s
119450K .......... .......... .......... .......... .......... 45% 7.69M 18s
119500K .......... .......... .......... .......... .......... 45% 6.70M 18s
119550K .......... .......... .......... .......... .......... 45% 1005K 18s
119600K .......... .......... .......... .......... .......... 45% 2.48M 18s
119650K .......... .......... .......... .......... .......... 45%  869K 18s
119700K .......... .......... .......... .......... .......... 45% 1.20M 18s
119750K .......... .......... .......... .......... .......... 45% 10.2M 18s
119800K .......... .......... .......... .......... .......... 45% 5.05M 18s
119850K .......... .......... .......... .......... .......... 45% 3.67M 18s
119900K .......... .......... .......... .......... .......... 45% 4.10M 18s
119950K .......... .......... .......... .......... .......... 45% 3.60M 18s
120000K .......... .......... .......... .......... .......... 45% 3.64M 18s
120050K .......... .......... .......... .......... .......... 45% 2.70M 18s
120100K .......... .......... .......... .......... .......... 45% 2.40M 18s
120150K .......... .......... .......... .......... .......... 45% 4.05M 18s
120200K .......... .......... .......... .......... .......... 45% 5.53M 18s
120250K .......... .......... .......... .......... .......... 45% 5.88M 18s
120300K .......... .......... .......... .......... .......... 45% 5.92M 18s
120350K .......... .......... .......... .......... .......... 45% 7.93M 18s
120400K .......... .......... .......... .......... .......... 45% 11.7M 18s
120450K .......... .......... .......... .......... .......... 45% 8.11M 18s
120500K .......... .......... .......... .......... .......... 45% 21.6M 18s
120550K .......... .......... .......... .......... .......... 45% 7.45M 18s
120600K .......... .......... .......... .......... .......... 46% 8.30M 18s
120650K .......... .......... .......... .......... .......... 46% 7.26M 18s
120700K .......... .......... .......... .......... .......... 46% 5.38M 18s
120750K .......... .......... .......... .......... .......... 46% 7.88M 18s
120800K .......... .......... .......... .......... .......... 46% 8.10M 18s
120850K .......... .......... .......... .......... .......... 46% 4.71M 18s
120900K .......... .......... .......... .......... .......... 46% 8.85M 18s
120950K .......... .......... .......... .......... .......... 46% 13.4M 18s
121000K .......... .......... .......... .......... .......... 46% 14.0M 18s
121050K .......... .......... .......... .......... .......... 46% 9.42M 18s
121100K .......... .......... .......... .......... .......... 46% 9.48M 18s
121150K .......... .......... .......... .......... .......... 46% 10.8M 18s
121200K .......... .......... .......... .......... .......... 46% 9.36M 18s
121250K .......... .......... .......... .......... .......... 46% 9.16M 18s
121300K .......... .......... .......... .......... .......... 46% 9.13M 18s
121350K .......... .......... .......... .......... .......... 46% 8.10M 18s
121400K .......... .......... .......... .......... .......... 46% 6.00M 18s
121450K .......... .......... .......... .......... .......... 46% 3.75M 18s
121500K .......... .......... .......... .......... .......... 46% 5.09M 18s
121550K .......... .......... .......... .......... .......... 46% 5.64M 18s
121600K .......... .......... .......... .......... .......... 46% 3.50M 18s
121650K .......... .......... .......... .......... .......... 46% 3.39M 18s
121700K .......... .......... .......... .......... .......... 46% 3.36M 18s
121750K .......... .......... .......... .......... .......... 46% 2.09M 18s
121800K .......... .......... .......... .......... .......... 46% 2.50M 18s
121850K .......... .......... .......... .......... .......... 46% 5.48M 18s
121900K .......... .......... .......... .......... .......... 46% 4.73M 18s
121950K .......... .......... .......... .......... .......... 46% 3.14M 18s
122000K .......... .......... .......... .......... .......... 46% 4.80M 18s
122050K .......... .......... .......... .......... .......... 46% 4.15M 18s
122100K .......... .......... .......... .......... .......... 46% 4.90M 18s
122150K .......... .......... .......... .......... .......... 46% 4.91M 18s
122200K .......... .......... .......... .......... .......... 46% 4.68M 18s
122250K .......... .......... .......... .......... .......... 46% 8.01M 18s
122300K .......... .......... .......... .......... .......... 46% 8.29M 18s
122350K .......... .......... .......... .......... .......... 46% 7.75M 18s
122400K .......... .......... .......... .......... .......... 46% 10.6M 18s
122450K .......... .......... .......... .......... .......... 46% 28.2M 18s
122500K .......... .......... .......... .......... .......... 46% 16.9M 18s
122550K .......... .......... .......... .......... .......... 46% 6.31M 18s
122600K .......... .......... .......... .......... .......... 46% 3.99M 18s
122650K .......... .......... .......... .......... .......... 46% 5.04M 18s
122700K .......... .......... .......... .......... .......... 46% 4.99M 18s
122750K .......... .......... .......... .......... .......... 46% 5.39M 18s
122800K .......... .......... .......... .......... .......... 46% 7.27M 18s
122850K .......... .......... .......... .......... .......... 46% 17.7M 18s
122900K .......... .......... .......... .......... .......... 46% 13.3M 18s
122950K .......... .......... .......... .......... .......... 46% 6.48M 18s
123000K .......... .......... .......... .......... .......... 46% 8.99M 18s
123050K .......... .......... .......... .......... .......... 46% 13.1M 17s
123100K .......... .......... .......... .......... .......... 46% 5.79M 17s
123150K .......... .......... .......... .......... .......... 46% 7.10M 17s
123200K .......... .......... .......... .......... .......... 47% 4.27M 17s
123250K .......... .......... .......... .......... .......... 47% 4.66M 17s
123300K .......... .......... .......... .......... .......... 47% 5.67M 17s
123350K .......... .......... .......... .......... .......... 47% 3.58M 17s
123400K .......... .......... .......... .......... .......... 47% 3.60M 17s
123450K .......... .......... .......... .......... .......... 47% 2.57M 17s
123500K .......... .......... .......... .......... .......... 47% 3.47M 17s
123550K .......... .......... .......... .......... .......... 47% 5.17M 17s
123600K .......... .......... .......... .......... .......... 47% 4.21M 17s
123650K .......... .......... .......... .......... .......... 47% 5.03M 17s
123700K .......... .......... .......... .......... .......... 47% 3.40M 17s
123750K .......... .......... .......... .......... .......... 47% 4.04M 17s
123800K .......... .......... .......... .......... .......... 47% 6.87M 17s
123850K .......... .......... .......... .......... .......... 47% 29.3M 17s
123900K .......... .......... .......... .......... .......... 47% 37.2M 17s
123950K .......... .......... .......... .......... .......... 47% 35.3M 17s
124000K .......... .......... .......... .......... .......... 47% 46.7M 17s
124050K .......... .......... .......... .......... .......... 47% 29.7M 17s
124100K .......... .......... .......... .......... .......... 47% 24.9M 17s
124150K .......... .......... .......... .......... .......... 47% 24.7M 17s
124200K .......... .......... .......... .......... .......... 47% 22.4M 17s
124250K .......... .......... .......... .......... .......... 47% 13.5M 17s
124300K .......... .......... .......... .......... .......... 47% 28.7M 17s
124350K .......... .......... .......... .......... .......... 47% 11.2M 17s
124400K .......... .......... .......... .......... .......... 47% 40.2M 17s
124450K .......... .......... .......... .......... .......... 47% 15.8M 17s
124500K .......... .......... .......... .......... .......... 47% 12.5M 17s
124550K .......... .......... .......... .......... .......... 47% 14.0M 17s
124600K .......... .......... .......... .......... .......... 47% 7.40M 17s
124650K .......... .......... .......... .......... .......... 47% 7.60M 17s
124700K .......... .......... .......... .......... .......... 47% 5.11M 17s
124750K .......... .......... .......... .......... .......... 47% 3.89M 17s
124800K .......... .......... .......... .......... .......... 47% 4.48M 17s
124850K .......... .......... .......... .......... .......... 47% 6.18M 17s
124900K .......... .......... .......... .......... .......... 47% 8.34M 17s
124950K .......... .......... .......... .......... .......... 47% 6.34M 17s
125000K .......... .......... .......... .......... .......... 47% 7.47M 17s
125050K .......... .......... .......... .......... .......... 47% 10.5M 17s
125100K .......... .......... .......... .......... .......... 47% 19.3M 17s
125150K .......... .......... .......... .......... .......... 47% 18.3M 17s
125200K .......... .......... .......... .......... .......... 47% 21.9M 17s
125250K .......... .......... .......... .......... .......... 47% 19.6M 17s
125300K .......... .......... .......... .......... .......... 47% 20.7M 17s
125350K .......... .......... .......... .......... .......... 47% 21.5M 17s
125400K .......... .......... .......... .......... .......... 47% 18.3M 17s
125450K .......... .......... .......... .......... .......... 47% 12.6M 17s
125500K .......... .......... .......... .......... .......... 47% 13.8M 17s
125550K .......... .......... .......... .......... .......... 47% 9.24M 17s
125600K .......... .......... .......... .......... .......... 47% 8.84M 17s
125650K .......... .......... .......... .......... .......... 47% 10.2M 17s
125700K .......... .......... .......... .......... .......... 47% 7.49M 17s
125750K .......... .......... .......... .......... .......... 47% 6.17M 17s
125800K .......... .......... .......... .......... .......... 47% 8.43M 17s
125850K .......... .......... .......... .......... .......... 48% 7.38M 17s
125900K .......... .......... .......... .......... .......... 48% 4.84M 17s
125950K .......... .......... .......... .......... .......... 48% 3.89M 17s
126000K .......... .......... .......... .......... .......... 48% 3.63M 17s
126050K .......... .......... .......... .......... .......... 48% 4.55M 17s
126100K .......... .......... .......... .......... .......... 48% 4.30M 17s
126150K .......... .......... .......... .......... .......... 48% 4.30M 17s
126200K .......... .......... .......... .......... .......... 48% 4.41M 17s
126250K .......... .......... .......... .......... .......... 48% 5.49M 17s
126300K .......... .......... .......... .......... .......... 48% 6.98M 17s
126350K .......... .......... .......... .......... .......... 48% 4.98M 17s
126400K .......... .......... .......... .......... .......... 48% 5.23M 17s
126450K .......... .......... .......... .......... .......... 48% 5.85M 17s
126500K .......... .......... .......... .......... .......... 48% 17.7M 17s
126550K .......... .......... .......... .......... .......... 48% 17.5M 17s
126600K .......... .......... .......... .......... .......... 48% 36.9M 17s
126650K .......... .......... .......... .......... .......... 48% 21.4M 17s
126700K .......... .......... .......... .......... .......... 48% 16.2M 17s
126750K .......... .......... .......... .......... .......... 48% 11.3M 17s
126800K .......... .......... .......... .......... .......... 48% 16.6M 17s
126850K .......... .......... .......... .......... .......... 48% 10.4M 17s
126900K .......... .......... .......... .......... .......... 48% 8.39M 17s
126950K .......... .......... .......... .......... .......... 48% 6.75M 17s
127000K .......... .......... .......... .......... .......... 48% 7.89M 17s
127050K .......... .......... .......... .......... .......... 48% 8.60M 17s
127100K .......... .......... .......... .......... .......... 48% 6.65M 17s
127150K .......... .......... .......... .......... .......... 48% 3.78M 17s
127200K .......... .......... .......... .......... .......... 48% 2.66M 17s
127250K .......... .......... .......... .......... .......... 48% 3.51M 17s
127300K .......... .......... .......... .......... .......... 48% 3.81M 17s
127350K .......... .......... .......... .......... .......... 48% 3.57M 17s
127400K .......... .......... .......... .......... .......... 48% 5.20M 17s
127450K .......... .......... .......... .......... .......... 48% 6.02M 17s
127500K .......... .......... .......... .......... .......... 48% 7.43M 17s
127550K .......... .......... .......... .......... .......... 48% 4.60M 17s
127600K .......... .......... .......... .......... .......... 48% 3.83M 17s
127650K .......... .......... .......... .......... .......... 48% 3.99M 17s
127700K .......... .......... .......... .......... .......... 48% 4.73M 17s
127750K .......... .......... .......... .......... .......... 48% 10.5M 17s
127800K .......... .......... .......... .......... .......... 48% 10.2M 17s
127850K .......... .......... .......... .......... .......... 48% 10.1M 17s
127900K .......... .......... .......... .......... .......... 48% 7.84M 17s
127950K .......... .......... .......... .......... .......... 48% 12.0M 17s
128000K .......... .......... .......... .......... .......... 48% 11.9M 17s
128050K .......... .......... .......... .......... .......... 48% 9.54M 17s
128100K .......... .......... .......... .......... .......... 48% 9.18M 17s
128150K .......... .......... .......... .......... .......... 48% 13.0M 17s
128200K .......... .......... .......... .......... .......... 48% 7.57M 17s
128250K .......... .......... .......... .......... .......... 48% 12.0M 17s
128300K .......... .......... .......... .......... .......... 48% 13.3M 17s
128350K .......... .......... .......... .......... .......... 48% 21.6M 17s
128400K .......... .......... .......... .......... .......... 48% 20.0M 17s
128450K .......... .......... .......... .......... .......... 49% 15.3M 17s
128500K .......... .......... .......... .......... .......... 49% 25.6M 17s
128550K .......... .......... .......... .......... .......... 49% 13.0M 17s
128600K .......... .......... .......... .......... .......... 49% 16.1M 17s
128650K .......... .......... .......... .......... .......... 49% 11.1M 17s
128700K .......... .......... .......... .......... .......... 49% 6.85M 17s
128750K .......... .......... .......... .......... .......... 49% 10.7M 17s
128800K .......... .......... .......... .......... .......... 49% 7.30M 17s
128850K .......... .......... .......... .......... .......... 49% 8.16M 17s
128900K .......... .......... .......... .......... .......... 49% 7.33M 17s
128950K .......... .......... .......... .......... .......... 49% 8.08M 17s
129000K .......... .......... .......... .......... .......... 49% 9.61M 17s
129050K .......... .......... .......... .......... .......... 49% 6.41M 17s
129100K .......... .......... .......... .......... .......... 49% 6.93M 17s
129150K .......... .......... .......... .......... .......... 49% 6.51M 17s
129200K .......... .......... .......... .......... .......... 49% 6.67M 17s
129250K .......... .......... .......... .......... .......... 49% 5.40M 17s
129300K .......... .......... .......... .......... .......... 49% 3.32M 17s
129350K .......... .......... .......... .......... .......... 49% 6.22M 17s
129400K .......... .......... .......... .......... .......... 49% 8.21M 17s
129450K .......... .......... .......... .......... .......... 49% 8.49M 17s
129500K .......... .......... .......... .......... .......... 49% 17.5M 17s
129550K .......... .......... .......... .......... .......... 49% 21.1M 17s
129600K .......... .......... .......... .......... .......... 49% 8.58M 17s
129650K .......... .......... .......... .......... .......... 49% 10.6M 17s
129700K .......... .......... .......... .......... .......... 49% 4.46M 17s
129750K .......... .......... .......... .......... .......... 49% 3.50M 17s
129800K .......... .......... .......... .......... .......... 49% 4.10M 17s
129850K .......... .......... .......... .......... .......... 49% 3.57M 17s
129900K .......... .......... .......... .......... .......... 49% 8.02M 17s
129950K .......... .......... .......... .......... .......... 49% 5.52M 17s
130000K .......... .......... .......... .......... .......... 49% 5.18M 17s
130050K .......... .......... .......... .......... .......... 49% 5.69M 17s
130100K .......... .......... .......... .......... .......... 49% 4.01M 17s
130150K .......... .......... .......... .......... .......... 49% 2.85M 17s
130200K .......... .......... .......... .......... .......... 49% 1.08M 17s
130250K .......... .......... .......... .......... .......... 49% 1.97M 17s
130300K .......... .......... .......... .......... .......... 49% 2.20M 17s
130350K .......... .......... .......... .......... .......... 49% 5.28M 17s
130400K .......... .......... .......... .......... .......... 49% 11.4M 17s
130450K .......... .......... .......... .......... .......... 49% 40.4M 17s
130500K .......... .......... .......... .......... .......... 49% 28.9M 17s
130550K .......... .......... .......... .......... .......... 49% 20.4M 17s
130600K .......... .......... .......... .......... .......... 49% 24.5M 17s
130650K .......... .......... .......... .......... .......... 49% 20.9M 17s
130700K .......... .......... .......... .......... .......... 49% 15.9M 17s
130750K .......... .......... .......... .......... .......... 49% 29.8M 17s
130800K .......... .......... .......... .......... .......... 49% 18.5M 17s
130850K .......... .......... .......... .......... .......... 49% 20.4M 17s
130900K .......... .......... .......... .......... .......... 49% 18.8M 17s
130950K .......... .......... .......... .......... .......... 49% 15.0M 17s
131000K .......... .......... .......... .......... .......... 49% 15.8M 17s
131050K .......... .......... .......... .......... .......... 50% 18.3M 17s
131100K .......... .......... .......... .......... .......... 50% 14.0M 17s
131150K .......... .......... .......... .......... .......... 50% 17.3M 17s
131200K .......... .......... .......... .......... .......... 50% 15.7M 17s
131250K .......... .......... .......... .......... .......... 50% 15.2M 17s
131300K .......... .......... .......... .......... .......... 50% 16.3M 17s
131350K .......... .......... .......... .......... .......... 50% 6.06M 17s
131400K .......... .......... .......... .......... .......... 50% 13.1M 17s
131450K .......... .......... .......... .......... .......... 50% 13.2M 17s
131500K .......... .......... .......... .......... .......... 50% 12.6M 17s
131550K .......... .......... .......... .......... .......... 50% 10.9M 17s
131600K .......... .......... .......... .......... .......... 50% 7.88M 17s
131650K .......... .......... .......... .......... .......... 50% 5.71M 17s
131700K .......... .......... .......... .......... .......... 50% 4.44M 17s
131750K .......... .......... .......... .......... .......... 50% 2.98M 17s
131800K .......... .......... .......... .......... .......... 50% 3.37M 17s
131850K .......... .......... .......... .......... .......... 50% 2.47M 17s
131900K .......... .......... .......... .......... .......... 50% 2.76M 17s
131950K .......... .......... .......... .......... .......... 50% 2.83M 17s
132000K .......... .......... .......... .......... .......... 50% 1.74M 17s
132050K .......... .......... .......... .......... .......... 50% 1.63M 17s
132100K .......... .......... .......... .......... .......... 50% 1.67M 17s
132150K .......... .......... .......... .......... .......... 50% 2.88M 17s
132200K .......... .......... .......... .......... .......... 50% 11.8M 17s
132250K .......... .......... .......... .......... .......... 50% 10.6M 17s
132300K .......... .......... .......... .......... .......... 50% 8.63M 17s
132350K .......... .......... .......... .......... .......... 50% 8.13M 17s
132400K .......... .......... .......... .......... .......... 50% 6.20M 17s
132450K .......... .......... .......... .......... .......... 50% 7.03M 17s
132500K .......... .......... .......... .......... .......... 50% 8.55M 17s
132550K .......... .......... .......... .......... .......... 50% 6.30M 17s
132600K .......... .......... .......... .......... .......... 50% 5.72M 17s
132650K .......... .......... .......... .......... .......... 50% 9.19M 17s
132700K .......... .......... .......... .......... .......... 50% 7.14M 17s
132750K .......... .......... .......... .......... .......... 50% 9.14M 17s
132800K .......... .......... .......... .......... .......... 50% 9.36M 17s
132850K .......... .......... .......... .......... .......... 50% 6.60M 16s
132900K .......... .......... .......... .......... .......... 50% 6.97M 16s
132950K .......... .......... .......... .......... .......... 50% 4.97M 16s
133000K .......... .......... .......... .......... .......... 50% 4.04M 16s
133050K .......... .......... .......... .......... .......... 50% 3.50M 16s
133100K .......... .......... .......... .......... .......... 50% 4.16M 16s
133150K .......... .......... .......... .......... .......... 50% 13.3M 16s
133200K .......... .......... .......... .......... .......... 50% 9.34M 16s
133250K .......... .......... .......... .......... .......... 50% 11.0M 16s
133300K .......... .......... .......... .......... .......... 50% 8.43M 16s
133350K .......... .......... .......... .......... .......... 50% 8.36M 16s
133400K .......... .......... .......... .......... .......... 50% 9.14M 16s
133450K .......... .......... .......... .......... .......... 50% 8.38M 16s
133500K .......... .......... .......... .......... .......... 50% 7.11M 16s
133550K .......... .......... .......... .......... .......... 50% 7.59M 16s
133600K .......... .......... .......... .......... .......... 50% 5.62M 16s
133650K .......... .......... .......... .......... .......... 50% 5.58M 16s
133700K .......... .......... .......... .......... .......... 51% 3.64M 16s
133750K .......... .......... .......... .......... .......... 51% 3.77M 16s
133800K .......... .......... .......... .......... .......... 51% 3.23M 16s
133850K .......... .......... .......... .......... .......... 51% 3.58M 16s
133900K .......... .......... .......... .......... .......... 51% 4.08M 16s
133950K .......... .......... .......... .......... .......... 51% 3.04M 16s
134000K .......... .......... .......... .......... .......... 51% 2.79M 16s
134050K .......... .......... .......... .......... .......... 51% 2.12M 16s
134100K .......... .......... .......... .......... .......... 51% 1.53M 16s
134150K .......... .......... .......... .......... .......... 51% 2.51M 16s
134200K .......... .......... .......... .......... .......... 51% 7.18M 16s
134250K .......... .......... .......... .......... .......... 51% 10.2M 16s
134300K .......... .......... .......... .......... .......... 51% 7.84M 16s
134350K .......... .......... .......... .......... .......... 51% 7.47M 16s
134400K .......... .......... .......... .......... .......... 51% 6.39M 16s
134450K .......... .......... .......... .......... .......... 51% 4.97M 16s
134500K .......... .......... .......... .......... .......... 51% 5.98M 16s
134550K .......... .......... .......... .......... .......... 51% 4.63M 16s
134600K .......... .......... .......... .......... .......... 51% 2.73M 16s
134650K .......... .......... .......... .......... .......... 51% 3.57M 16s
134700K .......... .......... .......... .......... .......... 51% 3.06M 16s
134750K .......... .......... .......... .......... .......... 51% 7.92M 16s
134800K .......... .......... .......... .......... .......... 51% 6.62M 16s
134850K .......... .......... .......... .......... .......... 51% 4.78M 16s
134900K .......... .......... .......... .......... .......... 51% 5.97M 16s
134950K .......... .......... .......... .......... .......... 51% 4.36M 16s
135000K .......... .......... .......... .......... .......... 51% 5.16M 16s
135050K .......... .......... .......... .......... .......... 51% 4.17M 16s
135100K .......... .......... .......... .......... .......... 51% 1.47M 16s
135150K .......... .......... .......... .......... .......... 51% 1.74M 16s
135200K .......... .......... .......... .......... .......... 51% 4.82M 16s
135250K .......... .......... .......... .......... .......... 51% 2.40M 16s
135300K .......... .......... .......... .......... .......... 51% 2.01M 16s
135350K .......... .......... .......... .......... .......... 51% 2.01M 16s
135400K .......... .......... .......... .......... .......... 51% 4.30M 16s
135450K .......... .......... .......... .......... .......... 51% 10.2M 16s
135500K .......... .......... .......... .......... .......... 51% 32.9M 16s
135550K .......... .......... .......... .......... .......... 51% 16.1M 16s
135600K .......... .......... .......... .......... .......... 51% 18.7M 16s
135650K .......... .......... .......... .......... .......... 51% 21.3M 16s
135700K .......... .......... .......... .......... .......... 51% 17.4M 16s
135750K .......... .......... .......... .......... .......... 51% 23.8M 16s
135800K .......... .......... .......... .......... .......... 51% 18.3M 16s
135850K .......... .......... .......... .......... .......... 51% 14.8M 16s
135900K .......... .......... .......... .......... .......... 51% 19.5M 16s
135950K .......... .......... .......... .......... .......... 51% 12.0M 16s
136000K .......... .......... .......... .......... .......... 51% 8.46M 16s
136050K .......... .......... .......... .......... .......... 51% 7.35M 16s
136100K .......... .......... .......... .......... .......... 51% 11.3M 16s
136150K .......... .......... .......... .......... .......... 51% 9.10M 16s
136200K .......... .......... .......... .......... .......... 51% 6.51M 16s
136250K .......... .......... .......... .......... .......... 51% 5.25M 16s
136300K .......... .......... .......... .......... .......... 52% 6.74M 16s
136350K .......... .......... .......... .......... .......... 52% 9.63M 16s
136400K .......... .......... .......... .......... .......... 52% 6.73M 16s
136450K .......... .......... .......... .......... .......... 52% 5.83M 16s
136500K .......... .......... .......... .......... .......... 52% 6.23M 16s
136550K .......... .......... .......... .......... .......... 52% 7.23M 16s
136600K .......... .......... .......... .......... .......... 52% 4.14M 16s
136650K .......... .......... .......... .......... .......... 52% 4.36M 16s
136700K .......... .......... .......... .......... .......... 52% 3.96M 16s
136750K .......... .......... .......... .......... .......... 52% 3.80M 16s
136800K .......... .......... .......... .......... .......... 52% 4.97M 16s
136850K .......... .......... .......... .......... .......... 52% 5.87M 16s
136900K .......... .......... .......... .......... .......... 52% 9.86M 16s
136950K .......... .......... .......... .......... .......... 52% 7.64M 16s
137000K .......... .......... .......... .......... .......... 52% 10.3M 16s
137050K .......... .......... .......... .......... .......... 52% 8.06M 16s
137100K .......... .......... .......... .......... .......... 52% 8.53M 16s
137150K .......... .......... .......... .......... .......... 52% 7.40M 16s
137200K .......... .......... .......... .......... .......... 52% 17.8M 16s
137250K .......... .......... .......... .......... .......... 52% 12.4M 16s
137300K .......... .......... .......... .......... .......... 52% 15.3M 16s
137350K .......... .......... .......... .......... .......... 52% 13.2M 16s
137400K .......... .......... .......... .......... .......... 52% 14.3M 16s
137450K .......... .......... .......... .......... .......... 52% 7.93M 16s
137500K .......... .......... .......... .......... .......... 52% 9.23M 16s
137550K .......... .......... .......... .......... .......... 52% 6.21M 16s
137600K .......... .......... .......... .......... .......... 52% 5.89M 16s
137650K .......... .......... .......... .......... .......... 52% 7.52M 16s
137700K .......... .......... .......... .......... .......... 52% 5.62M 16s
137750K .......... .......... .......... .......... .......... 52% 6.19M 16s
137800K .......... .......... .......... .......... .......... 52% 6.73M 16s
137850K .......... .......... .......... .......... .......... 52% 5.96M 16s
137900K .......... .......... .......... .......... .......... 52% 6.44M 16s
137950K .......... .......... .......... .......... .......... 52% 6.21M 16s
138000K .......... .......... .......... .......... .......... 52% 7.22M 16s
138050K .......... .......... .......... .......... .......... 52% 6.27M 16s
138100K .......... .......... .......... .......... .......... 52% 5.35M 16s
138150K .......... .......... .......... .......... .......... 52% 12.3M 16s
138200K .......... .......... .......... .......... .......... 52% 17.0M 16s
138250K .......... .......... .......... .......... .......... 52% 21.7M 16s
138300K .......... .......... .......... .......... .......... 52% 14.8M 16s
138350K .......... .......... .......... .......... .......... 52% 12.6M 16s
138400K .......... .......... .......... .......... .......... 52% 9.76M 16s
138450K .......... .......... .......... .......... .......... 52% 31.2M 16s
138500K .......... .......... .......... .......... .......... 52% 9.61M 16s
138550K .......... .......... .......... .......... .......... 52% 16.9M 16s
138600K .......... .......... .......... .......... .......... 52% 10.2M 16s
138650K .......... .......... .......... .......... .......... 52% 7.59M 16s
138700K .......... .......... .......... .......... .......... 52% 3.58M 16s
138750K .......... .......... .......... .......... .......... 52% 2.25M 16s
138800K .......... .......... .......... .......... .......... 52% 4.01M 16s
138850K .......... .......... .......... .......... .......... 52%  830K 16s
138900K .......... .......... .......... .......... .......... 52% 1.92M 16s
138950K .......... .......... .......... .......... .......... 53% 2.92M 16s
139000K .......... .......... .......... .......... .......... 53% 9.82M 16s
139050K .......... .......... .......... .......... .......... 53% 6.80M 16s
139100K .......... .......... .......... .......... .......... 53% 6.47M 16s
139150K .......... .......... .......... .......... .......... 53% 4.79M 16s
139200K .......... .......... .......... .......... .......... 53% 4.18M 16s
139250K .......... .......... .......... .......... .......... 53% 3.19M 16s
139300K .......... .......... .......... .......... .......... 53% 3.25M 16s
139350K .......... .......... .......... .......... .......... 53% 3.37M 16s
139400K .......... .......... .......... .......... .......... 53% 7.18M 16s
139450K .......... .......... .......... .......... .......... 53% 7.19M 16s
139500K .......... .......... .......... .......... .......... 53% 7.74M 16s
139550K .......... .......... .......... .......... .......... 53% 10.5M 16s
139600K .......... .......... .......... .......... .......... 53% 8.07M 16s
139650K .......... .......... .......... .......... .......... 53% 7.98M 16s
139700K .......... .......... .......... .......... .......... 53% 6.02M 16s
139750K .......... .......... .......... .......... .......... 53% 5.52M 16s
139800K .......... .......... .......... .......... .......... 53% 5.05M 16s
139850K .......... .......... .......... .......... .......... 53% 4.30M 16s
139900K .......... .......... .......... .......... .......... 53% 5.07M 16s
139950K .......... .......... .......... .......... .......... 53% 7.88M 16s
140000K .......... .......... .......... .......... .......... 53% 13.4M 16s
140050K .......... .......... .......... .......... .......... 53% 12.9M 16s
140100K .......... .......... .......... .......... .......... 53% 9.68M 16s
140150K .......... .......... .......... .......... .......... 53% 11.9M 16s
140200K .......... .......... .......... .......... .......... 53% 12.1M 16s
140250K .......... .......... .......... .......... .......... 53% 12.9M 16s
140300K .......... .......... .......... .......... .......... 53% 15.0M 16s
140350K .......... .......... .......... .......... .......... 53% 11.3M 16s
140400K .......... .......... .......... .......... .......... 53% 16.8M 16s
140450K .......... .......... .......... .......... .......... 53% 13.1M 16s
140500K .......... .......... .......... .......... .......... 53% 12.8M 16s
140550K .......... .......... .......... .......... .......... 53% 17.6M 16s
140600K .......... .......... .......... .......... .......... 53% 10.5M 16s
140650K .......... .......... .......... .......... .......... 53% 13.5M 16s
140700K .......... .......... .......... .......... .......... 53% 14.0M 16s
140750K .......... .......... .......... .......... .......... 53% 11.3M 16s
140800K .......... .......... .......... .......... .......... 53% 10.2M 16s
140850K .......... .......... .......... .......... .......... 53% 11.3M 16s
140900K .......... .......... .......... .......... .......... 53% 12.5M 16s
140950K .......... .......... .......... .......... .......... 53% 8.13M 16s
141000K .......... .......... .......... .......... .......... 53% 8.58M 16s
141050K .......... .......... .......... .......... .......... 53% 9.53M 16s
141100K .......... .......... .......... .......... .......... 53% 5.97M 16s
141150K .......... .......... .......... .......... .......... 53% 8.23M 16s
141200K .......... .......... .......... .......... .......... 53% 6.64M 16s
141250K .......... .......... .......... .......... .......... 53% 4.52M 16s
141300K .......... .......... .......... .......... .......... 53% 5.97M 16s
141350K .......... .......... .......... .......... .......... 53% 4.22M 16s
141400K .......... .......... .......... .......... .......... 53% 5.32M 16s
141450K .......... .......... .......... .......... .......... 53% 5.52M 16s
141500K .......... .......... .......... .......... .......... 53% 14.4M 16s
141550K .......... .......... .......... .......... .......... 54% 14.4M 16s
141600K .......... .......... .......... .......... .......... 54% 13.0M 16s
141650K .......... .......... .......... .......... .......... 54% 14.3M 16s
141700K .......... .......... .......... .......... .......... 54% 14.3M 16s
141750K .......... .......... .......... .......... .......... 54% 13.3M 16s
141800K .......... .......... .......... .......... .......... 54% 15.5M 16s
141850K .......... .......... .......... .......... .......... 54% 15.8M 16s
141900K .......... .......... .......... .......... .......... 54% 11.2M 16s
141950K .......... .......... .......... .......... .......... 54% 9.84M 16s
142000K .......... .......... .......... .......... .......... 54% 18.1M 16s
142050K .......... .......... .......... .......... .......... 54% 14.2M 16s
142100K .......... .......... .......... .......... .......... 54% 7.93M 16s
142150K .......... .......... .......... .......... .......... 54% 7.55M 16s
142200K .......... .......... .......... .......... .......... 54% 7.30M 16s
142250K .......... .......... .......... .......... .......... 54% 9.72M 16s
142300K .......... .......... .......... .......... .......... 54% 9.05M 16s
142350K .......... .......... .......... .......... .......... 54% 6.29M 16s
142400K .......... .......... .......... .......... .......... 54% 7.50M 16s
142450K .......... .......... .......... .......... .......... 54% 10.4M 16s
142500K .......... .......... .......... .......... .......... 54% 6.71M 16s
142550K .......... .......... .......... .......... .......... 54% 41.9M 16s
142600K .......... .......... .......... .......... .......... 54% 6.62M 16s
142650K .......... .......... .......... .......... .......... 54% 6.94M 16s
142700K .......... .......... .......... .......... .......... 54% 8.18M 16s
142750K .......... .......... .......... .......... .......... 54% 8.36M 16s
142800K .......... .......... .......... .......... .......... 54% 9.93M 16s
142850K .......... .......... .......... .......... .......... 54% 7.70M 16s
142900K .......... .......... .......... .......... .......... 54% 10.9M 16s
142950K .......... .......... .......... .......... .......... 54% 10.7M 15s
143000K .......... .......... .......... .......... .......... 54% 17.0M 15s
143050K .......... .......... .......... .......... .......... 54% 24.2M 15s
143100K .......... .......... .......... .......... .......... 54% 18.2M 15s
143150K .......... .......... .......... .......... .......... 54% 20.9M 15s
143200K .......... .......... .......... .......... .......... 54% 25.2M 15s
143250K .......... .......... .......... .......... .......... 54% 23.9M 15s
143300K .......... .......... .......... .......... .......... 54% 9.09M 15s
143350K .......... .......... .......... .......... .......... 54% 63.0M 15s
143400K .......... .......... .......... .......... .......... 54% 15.5M 15s
143450K .......... .......... .......... .......... .......... 54% 12.1M 15s
143500K .......... .......... .......... .......... .......... 54% 10.5M 15s
143550K .......... .......... .......... .......... .......... 54% 7.36M 15s
143600K .......... .......... .......... .......... .......... 54% 6.82M 15s
143650K .......... .......... .......... .......... .......... 54% 5.22M 15s
143700K .......... .......... .......... .......... .......... 54% 3.82M 15s
143750K .......... .......... .......... .......... .......... 54% 4.14M 15s
143800K .......... .......... .......... .......... .......... 54% 6.54M 15s
143850K .......... .......... .......... .......... .......... 54% 4.74M 15s
143900K .......... .......... .......... .......... .......... 54% 6.46M 15s
143950K .......... .......... .......... .......... .......... 54% 3.13M 15s
144000K .......... .......... .......... .......... .......... 54% 1.04M 15s
144050K .......... .......... .......... .......... .......... 54% 2.75M 15s
144100K .......... .......... .......... .......... .......... 54% 2.10M 15s
144150K .......... .......... .......... .......... .......... 54% 2.56M 15s
144200K .......... .......... .......... .......... .......... 55% 2.32M 15s
144250K .......... .......... .......... .......... .......... 55% 11.0M 15s
144300K .......... .......... .......... .......... .......... 55% 7.86M 15s
144350K .......... .......... .......... .......... .......... 55% 7.02M 15s
144400K .......... .......... .......... .......... .......... 55% 7.80M 15s
144450K .......... .......... .......... .......... .......... 55% 6.69M 15s
144500K .......... .......... .......... .......... .......... 55% 9.07M 15s
144550K .......... .......... .......... .......... .......... 55% 5.77M 15s
144600K .......... .......... .......... .......... .......... 55% 6.67M 15s
144650K .......... .......... .......... .......... .......... 55% 5.73M 15s
144700K .......... .......... .......... .......... .......... 55% 4.39M 15s
144750K .......... .......... .......... .......... .......... 55% 4.45M 15s
144800K .......... .......... .......... .......... .......... 55% 6.01M 15s
144850K .......... .......... .......... .......... .......... 55% 4.60M 15s
144900K .......... .......... .......... .......... .......... 55% 14.0M 15s
144950K .......... .......... .......... .......... .......... 55% 10.9M 15s
145000K .......... .......... .......... .......... .......... 55% 8.73M 15s
145050K .......... .......... .......... .......... .......... 55% 9.00M 15s
145100K .......... .......... .......... .......... .......... 55% 8.13M 15s
145150K .......... .......... .......... .......... .......... 55% 9.42M 15s
145200K .......... .......... .......... .......... .......... 55% 7.56M 15s
145250K .......... .......... .......... .......... .......... 55% 10.4M 15s
145300K .......... .......... .......... .......... .......... 55% 8.25M 15s
145350K .......... .......... .......... .......... .......... 55% 6.06M 15s
145400K .......... .......... .......... .......... .......... 55% 6.44M 15s
145450K .......... .......... .......... .......... .......... 55% 4.71M 15s
145500K .......... .......... .......... .......... .......... 55% 4.24M 15s
145550K .......... .......... .......... .......... .......... 55% 4.07M 15s
145600K .......... .......... .......... .......... .......... 55% 3.26M 15s
145650K .......... .......... .......... .......... .......... 55% 7.43M 15s
145700K .......... .......... .......... .......... .......... 55% 6.79M 15s
145750K .......... .......... .......... .......... .......... 55% 6.78M 15s
145800K .......... .......... .......... .......... .......... 55% 5.88M 15s
145850K .......... .......... .......... .......... .......... 55% 6.09M 15s
145900K .......... .......... .......... .......... .......... 55% 6.19M 15s
145950K .......... .......... .......... .......... .......... 55% 4.75M 15s
146000K .......... .......... .......... .......... .......... 55% 5.07M 15s
146050K .......... .......... .......... .......... .......... 55% 5.48M 15s
146100K .......... .......... .......... .......... .......... 55% 4.20M 15s
146150K .......... .......... .......... .......... .......... 55% 3.95M 15s
146200K .......... .......... .......... .......... .......... 55% 4.01M 15s
146250K .......... .......... .......... .......... .......... 55% 7.00M 15s
146300K .......... .......... .......... .......... .......... 55% 15.9M 15s
146350K .......... .......... .......... .......... .......... 55% 16.7M 15s
146400K .......... .......... .......... .......... .......... 55% 16.4M 15s
146450K .......... .......... .......... .......... .......... 55% 8.11M 15s
146500K .......... .......... .......... .......... .......... 55% 8.40M 15s
146550K .......... .......... .......... .......... .......... 55% 7.98M 15s
146600K .......... .......... .......... .......... .......... 55% 6.45M 15s
146650K .......... .......... .......... .......... .......... 55% 6.29M 15s
146700K .......... .......... .......... .......... .......... 55% 3.33M 15s
146750K .......... .......... .......... .......... .......... 55% 3.46M 15s
146800K .......... .......... .......... .......... .......... 56% 2.16M 15s
146850K .......... .......... .......... .......... .......... 56% 1.65M 15s
146900K .......... .......... .......... .......... .......... 56% 5.22M 15s
146950K .......... .......... .......... .......... .......... 56% 4.64M 15s
147000K .......... .......... .......... .......... .......... 56% 5.80M 15s
147050K .......... .......... .......... .......... .......... 56% 5.97M 15s
147100K .......... .......... .......... .......... .......... 56% 9.76M 15s
147150K .......... .......... .......... .......... .......... 56% 9.31M 15s
147200K .......... .......... .......... .......... .......... 56% 8.17M 15s
147250K .......... .......... .......... .......... .......... 56% 11.4M 15s
147300K .......... .......... .......... .......... .......... 56% 9.94M 15s
147350K .......... .......... .......... .......... .......... 56% 8.38M 15s
147400K .......... .......... .......... .......... .......... 56% 8.03M 15s
147450K .......... .......... .......... .......... .......... 56% 7.46M 15s
147500K .......... .......... .......... .......... .......... 56% 11.1M 15s
147550K .......... .......... .......... .......... .......... 56% 8.82M 15s
147600K .......... .......... .......... .......... .......... 56% 6.81M 15s
147650K .......... .......... .......... .......... .......... 56% 6.76M 15s
147700K .......... .......... .......... .......... .......... 56% 4.28M 15s
147750K .......... .......... .......... .......... .......... 56% 4.60M 15s
147800K .......... .......... .......... .......... .......... 56% 5.21M 15s
147850K .......... .......... .......... .......... .......... 56% 3.61M 15s
147900K .......... .......... .......... .......... .......... 56% 3.01M 15s
147950K .......... .......... .......... .......... .......... 56% 3.36M 15s
148000K .......... .......... .......... .......... .......... 56% 4.96M 15s
148050K .......... .......... .......... .......... .......... 56% 3.21M 15s
148100K .......... .......... .......... .......... .......... 56% 3.51M 15s
148150K .......... .......... .......... .......... .......... 56% 4.31M 15s
148200K .......... .......... .......... .......... .......... 56% 5.14M 15s
148250K .......... .......... .......... .......... .......... 56% 10.5M 15s
148300K .......... .......... .......... .......... .......... 56% 19.6M 15s
148350K .......... .......... .......... .......... .......... 56% 11.3M 15s
148400K .......... .......... .......... .......... .......... 56% 10.7M 15s
148450K .......... .......... .......... .......... .......... 56% 11.3M 15s
148500K .......... .......... .......... .......... .......... 56% 13.2M 15s
148550K .......... .......... .......... .......... .......... 56% 13.2M 15s
148600K .......... .......... .......... .......... .......... 56% 7.57M 15s
148650K .......... .......... .......... .......... .......... 56% 6.77M 15s
148700K .......... .......... .......... .......... .......... 56% 6.02M 15s
148750K .......... .......... .......... .......... .......... 56% 5.95M 15s
148800K .......... .......... .......... .......... .......... 56% 6.42M 15s
148850K .......... .......... .......... .......... .......... 56% 5.04M 15s
148900K .......... .......... .......... .......... .......... 56% 5.78M 15s
148950K .......... .......... .......... .......... .......... 56% 13.0M 15s
149000K .......... .......... .......... .......... .......... 56% 12.3M 15s
149050K .......... .......... .......... .......... .......... 56% 8.43M 15s
149100K .......... .......... .......... .......... .......... 56% 4.56M 15s
149150K .......... .......... .......... .......... .......... 56% 5.79M 15s
149200K .......... .......... .......... .......... .......... 56% 4.75M 15s
149250K .......... .......... .......... .......... .......... 56% 5.13M 15s
149300K .......... .......... .......... .......... .......... 56% 5.21M 15s
149350K .......... .......... .......... .......... .......... 56% 2.87M 15s
149400K .......... .......... .......... .......... .......... 57% 3.06M 15s
149450K .......... .......... .......... .......... .......... 57% 6.04M 15s
149500K .......... .......... .......... .......... .......... 57% 34.0M 15s
149550K .......... .......... .......... .......... .......... 57% 14.6M 15s
149600K .......... .......... .......... .......... .......... 57% 13.8M 15s
149650K .......... .......... .......... .......... .......... 57% 19.7M 15s
149700K .......... .......... .......... .......... .......... 57% 11.9M 15s
149750K .......... .......... .......... .......... .......... 57% 10.7M 15s
149800K .......... .......... .......... .......... .......... 57% 9.33M 15s
149850K .......... .......... .......... .......... .......... 57% 7.69M 15s
149900K .......... .......... .......... .......... .......... 57% 8.13M 15s
149950K .......... .......... .......... .......... .......... 57% 6.86M 15s
150000K .......... .......... .......... .......... .......... 57% 8.82M 15s
150050K .......... .......... .......... .......... .......... 57% 6.88M 15s
150100K .......... .......... .......... .......... .......... 57% 5.66M 15s
150150K .......... .......... .......... .......... .......... 57% 10.7M 15s
150200K .......... .......... .......... .......... .......... 57% 9.65M 15s
150250K .......... .......... .......... .......... .......... 57% 11.7M 15s
150300K .......... .......... .......... .......... .......... 57% 11.9M 15s
150350K .......... .......... .......... .......... .......... 57% 9.83M 15s
150400K .......... .......... .......... .......... .......... 57% 13.8M 15s
150450K .......... .......... .......... .......... .......... 57% 10.2M 15s
150500K .......... .......... .......... .......... .......... 57% 11.6M 15s
150550K .......... .......... .......... .......... .......... 57% 24.5M 15s
150600K .......... .......... .......... .......... .......... 57% 14.6M 15s
150650K .......... .......... .......... .......... .......... 57% 42.2M 15s
150700K .......... .......... .......... .......... .......... 57% 15.1M 15s
150750K .......... .......... .......... .......... .......... 57% 14.8M 15s
150800K .......... .......... .......... .......... .......... 57% 9.17M 15s
150850K .......... .......... .......... .......... .......... 57% 45.0M 15s
150900K .......... .......... .......... .......... .......... 57% 11.1M 15s
150950K .......... .......... .......... .......... .......... 57% 7.86M 15s
151000K .......... .......... .......... .......... .......... 57% 8.52M 15s
151050K .......... .......... .......... .......... .......... 57% 10.6M 15s
151100K .......... .......... .......... .......... .......... 57% 6.01M 15s
151150K .......... .......... .......... .......... .......... 57% 10.4M 15s
151200K .......... .......... .......... .......... .......... 57% 4.94M 15s
151250K .......... .......... .......... .......... .......... 57% 6.94M 15s
151300K .......... .......... .......... .......... .......... 57% 6.90M 15s
151350K .......... .......... .......... .......... .......... 57% 4.79M 15s
151400K .......... .......... .......... .......... .......... 57% 6.69M 15s
151450K .......... .......... .......... .......... .......... 57% 6.07M 15s
151500K .......... .......... .......... .......... .......... 57% 6.39M 15s
151550K .......... .......... .......... .......... .......... 57% 5.95M 15s
151600K .......... .......... .......... .......... .......... 57% 5.72M 15s
151650K .......... .......... .......... .......... .......... 57% 8.68M 15s
151700K .......... .......... .......... .......... .......... 57% 7.01M 15s
151750K .......... .......... .......... .......... .......... 57% 14.3M 15s
151800K .......... .......... .......... .......... .......... 57% 13.9M 15s
151850K .......... .......... .......... .......... .......... 57% 7.36M 15s
151900K .......... .......... .......... .......... .......... 57% 7.30M 14s
151950K .......... .......... .......... .......... .......... 57% 7.86M 14s
152000K .......... .......... .......... .......... .......... 57% 9.24M 14s
152050K .......... .......... .......... .......... .......... 58% 6.36M 14s
152100K .......... .......... .......... .......... .......... 58% 7.29M 14s
152150K .......... .......... .......... .......... .......... 58% 5.11M 14s
152200K .......... .......... .......... .......... .......... 58% 4.86M 14s
152250K .......... .......... .......... .......... .......... 58% 13.6M 14s
152300K .......... .......... .......... .......... .......... 58% 8.74M 14s
152350K .......... .......... .......... .......... .......... 58% 13.2M 14s
152400K .......... .......... .......... .......... .......... 58% 13.0M 14s
152450K .......... .......... .......... .......... .......... 58% 21.4M 14s
152500K .......... .......... .......... .......... .......... 58%  101M 14s
152550K .......... .......... .......... .......... .......... 58% 29.7M 14s
152600K .......... .......... .......... .......... .......... 58% 48.9M 14s
152650K .......... .......... .......... .......... .......... 58% 35.8M 14s
152700K .......... .......... .......... .......... .......... 58% 37.2M 14s
152750K .......... .......... .......... .......... .......... 58% 63.2M 14s
152800K .......... .......... .......... .......... .......... 58% 36.7M 14s
152850K .......... .......... .......... .......... .......... 58% 24.9M 14s
152900K .......... .......... .......... .......... .......... 58% 23.9M 14s
152950K .......... .......... .......... .......... .......... 58% 9.81M 14s
153000K .......... .......... .......... .......... .......... 58% 28.5M 14s
153050K .......... .......... .......... .......... .......... 58% 6.45M 14s
153100K .......... .......... .......... .......... .......... 58% 14.4M 14s
153150K .......... .......... .......... .......... .......... 58% 6.98M 14s
153200K .......... .......... .......... .......... .......... 58% 7.95M 14s
153250K .......... .......... .......... .......... .......... 58% 6.05M 14s
153300K .......... .......... .......... .......... .......... 58% 7.91M 14s
153350K .......... .......... .......... .......... .......... 58% 5.87M 14s
153400K .......... .......... .......... .......... .......... 58% 8.65M 14s
153450K .......... .......... .......... .......... .......... 58% 6.87M 14s
153500K .......... .......... .......... .......... .......... 58% 7.42M 14s
153550K .......... .......... .......... .......... .......... 58% 9.99M 14s
153600K .......... .......... .......... .......... .......... 58% 7.61M 14s
153650K .......... .......... .......... .......... .......... 58% 8.03M 14s
153700K .......... .......... .......... .......... .......... 58% 8.82M 14s
153750K .......... .......... .......... .......... .......... 58% 8.85M 14s
153800K .......... .......... .......... .......... .......... 58% 9.59M 14s
153850K .......... .......... .......... .......... .......... 58% 6.49M 14s
153900K .......... .......... .......... .......... .......... 58% 11.2M 14s
153950K .......... .......... .......... .......... .......... 58% 6.96M 14s
154000K .......... .......... .......... .......... .......... 58% 10.3M 14s
154050K .......... .......... .......... .......... .......... 58% 6.19M 14s
154100K .......... .......... .......... .......... .......... 58% 10.8M 14s
154150K .......... .......... .......... .......... .......... 58% 6.47M 14s
154200K .......... .......... .......... .......... .......... 58% 11.2M 14s
154250K .......... .......... .......... .......... .......... 58% 7.85M 14s
154300K .......... .......... .......... .......... .......... 58% 12.7M 14s
154350K .......... .......... .......... .......... .......... 58% 6.01M 14s
154400K .......... .......... .......... .......... .......... 58% 7.23M 14s
154450K .......... .......... .......... .......... .......... 58% 7.53M 14s
154500K .......... .......... .......... .......... .......... 58% 6.84M 14s
154550K .......... .......... .......... .......... .......... 58% 8.06M 14s
154600K .......... .......... .......... .......... .......... 58% 7.07M 14s
154650K .......... .......... .......... .......... .......... 59% 6.65M 14s
154700K .......... .......... .......... .......... .......... 59% 5.28M 14s
154750K .......... .......... .......... .......... .......... 59% 5.58M 14s
154800K .......... .......... .......... .......... .......... 59% 4.59M 14s
154850K .......... .......... .......... .......... .......... 59% 6.18M 14s
154900K .......... .......... .......... .......... .......... 59% 6.08M 14s
154950K .......... .......... .......... .......... .......... 59% 4.29M 14s
155000K .......... .......... .......... .......... .......... 59% 4.59M 14s
155050K .......... .......... .......... .......... .......... 59% 3.61M 14s
155100K .......... .......... .......... .......... .......... 59% 1.26M 14s
155150K .......... .......... .......... .......... .......... 59% 2.67M 14s
155200K .......... .......... .......... .......... .......... 59%  201M 14s
155250K .......... .......... .......... .......... .......... 59% 27.1M 14s
155300K .......... .......... .......... .......... .......... 59% 8.32M 14s
155350K .......... .......... .......... .......... .......... 59% 7.04M 14s
155400K .......... .......... .......... .......... .......... 59% 5.88M 14s
155450K .......... .......... .......... .......... .......... 59% 4.21M 14s
155500K .......... .......... .......... .......... .......... 59% 5.15M 14s
155550K .......... .......... .......... .......... .......... 59% 6.56M 14s
155600K .......... .......... .......... .......... .......... 59% 16.8M 14s
155650K .......... .......... .......... .......... .......... 59% 15.2M 14s
155700K .......... .......... .......... .......... .......... 59% 11.3M 14s
155750K .......... .......... .......... .......... .......... 59% 19.8M 14s
155800K .......... .......... .......... .......... .......... 59% 13.8M 14s
155850K .......... .......... .......... .......... .......... 59% 10.1M 14s
155900K .......... .......... .......... .......... .......... 59% 13.0M 14s
155950K .......... .......... .......... .......... .......... 59% 10.5M 14s
156000K .......... .......... .......... .......... .......... 59% 9.16M 14s
156050K .......... .......... .......... .......... .......... 59% 5.19M 14s
156100K .......... .......... .......... .......... .......... 59% 4.51M 14s
156150K .......... .......... .......... .......... .......... 59% 6.88M 14s
156200K .......... .......... .......... .......... .......... 59% 4.89M 14s
156250K .......... .......... .......... .......... .......... 59% 10.3M 14s
156300K .......... .......... .......... .......... .......... 59% 14.8M 14s
156350K .......... .......... .......... .......... .......... 59% 29.7M 14s
156400K .......... .......... .......... .......... .......... 59% 15.0M 14s
156450K .......... .......... .......... .......... .......... 59% 9.37M 14s
156500K .......... .......... .......... .......... .......... 59% 28.7M 14s
156550K .......... .......... .......... .......... .......... 59% 14.3M 14s
156600K .......... .......... .......... .......... .......... 59% 10.6M 14s
156650K .......... .......... .......... .......... .......... 59% 13.9M 14s
156700K .......... .......... .......... .......... .......... 59% 12.8M 14s
156750K .......... .......... .......... .......... .......... 59% 12.6M 14s
156800K .......... .......... .......... .......... .......... 59% 13.2M 14s
156850K .......... .......... .......... .......... .......... 59% 9.08M 14s
156900K .......... .......... .......... .......... .......... 59% 14.3M 14s
156950K .......... .......... .......... .......... .......... 59% 8.54M 14s
157000K .......... .......... .......... .......... .......... 59% 17.5M 14s
157050K .......... .......... .......... .......... .......... 59% 9.57M 14s
157100K .......... .......... .......... .......... .......... 59% 7.51M 14s
157150K .......... .......... .......... .......... .......... 59% 9.71M 14s
157200K .......... .......... .......... .......... .......... 59% 6.55M 14s
157250K .......... .......... .......... .......... .......... 59% 10.6M 14s
157300K .......... .......... .......... .......... .......... 60% 6.92M 14s
157350K .......... .......... .......... .......... .......... 60% 7.04M 14s
157400K .......... .......... .......... .......... .......... 60% 8.43M 14s
157450K .......... .......... .......... .......... .......... 60% 15.9M 14s
157500K .......... .......... .......... .......... .......... 60% 13.7M 14s
157550K .......... .......... .......... .......... .......... 60% 10.8M 14s
157600K .......... .......... .......... .......... .......... 60% 8.97M 14s
157650K .......... .......... .......... .......... .......... 60% 8.81M 14s
157700K .......... .......... .......... .......... .......... 60% 5.66M 14s
157750K .......... .......... .......... .......... .......... 60% 5.22M 14s
157800K .......... .......... .......... .......... .......... 60% 3.41M 14s
157850K .......... .......... .......... .......... .......... 60% 5.12M 14s
157900K .......... .......... .......... .......... .......... 60% 4.72M 14s
157950K .......... .......... .......... .......... .......... 60% 4.89M 14s
158000K .......... .......... .......... .......... .......... 60% 6.88M 14s
158050K .......... .......... .......... .......... .......... 60% 3.35M 14s
158100K .......... .......... .......... .......... .......... 60% 3.19M 14s
158150K .......... .......... .......... .......... .......... 60% 3.78M 14s
158200K .......... .......... .......... .......... .......... 60% 8.45M 14s
158250K .......... .......... .......... .......... .......... 60% 12.7M 14s
158300K .......... .......... .......... .......... .......... 60% 12.1M 14s
158350K .......... .......... .......... .......... .......... 60% 10.1M 14s
158400K .......... .......... .......... .......... .......... 60% 13.5M 14s
158450K .......... .......... .......... .......... .......... 60% 11.8M 14s
158500K .......... .......... .......... .......... .......... 60% 10.7M 14s
158550K .......... .......... .......... .......... .......... 60% 13.2M 14s
158600K .......... .......... .......... .......... .......... 60% 14.5M 14s
158650K .......... .......... .......... .......... .......... 60% 22.0M 14s
158700K .......... .......... .......... .......... .......... 60% 20.3M 14s
158750K .......... .......... .......... .......... .......... 60% 26.2M 14s
158800K .......... .......... .......... .......... .......... 60% 19.4M 14s
158850K .......... .......... .......... .......... .......... 60% 21.4M 14s
158900K .......... .......... .......... .......... .......... 60% 13.4M 14s
158950K .......... .......... .......... .......... .......... 60% 27.7M 14s
159000K .......... .......... .......... .......... .......... 60% 8.70M 14s
159050K .......... .......... .......... .......... .......... 60%  126M 13s
159100K .......... .......... .......... .......... .......... 60% 10.3M 13s
159150K .......... .......... .......... .......... .......... 60% 7.97M 13s
159200K .......... .......... .......... .......... .......... 60% 5.26M 13s
159250K .......... .......... .......... .......... .......... 60% 8.10M 13s
159300K .......... .......... .......... .......... .......... 60% 7.32M 13s
159350K .......... .......... .......... .......... .......... 60% 5.39M 13s
159400K .......... .......... .......... .......... .......... 60% 5.60M 13s
159450K .......... .......... .......... .......... .......... 60% 4.22M 13s
159500K .......... .......... .......... .......... .......... 60% 4.48M 13s
159550K .......... .......... .......... .......... .......... 60% 2.75M 13s
159600K .......... .......... .......... .......... .......... 60% 2.63M 13s
159650K .......... .......... .......... .......... .......... 60% 2.55M 13s
159700K .......... .......... .......... .......... .......... 60% 8.54M 13s
159750K .......... .......... .......... .......... .......... 60% 20.2M 13s
159800K .......... .......... .......... .......... .......... 60% 43.5M 13s
159850K .......... .......... .......... .......... .......... 60% 25.2M 13s
159900K .......... .......... .......... .......... .......... 61% 35.8M 13s
159950K .......... .......... .......... .......... .......... 61% 15.7M 13s
160000K .......... .......... .......... .......... .......... 61%  122M 13s
160050K .......... .......... .......... .......... .......... 61% 27.5M 13s
160100K .......... .......... .......... .......... .......... 61% 22.1M 13s
160150K .......... .......... .......... .......... .......... 61% 31.9M 13s
160200K .......... .......... .......... .......... .......... 61% 17.7M 13s
160250K .......... .......... .......... .......... .......... 61% 23.4M 13s
160300K .......... .......... .......... .......... .......... 61% 14.4M 13s
160350K .......... .......... .......... .......... .......... 61% 14.5M 13s
160400K .......... .......... .......... .......... .......... 61% 12.9M 13s
160450K .......... .......... .......... .......... .......... 61% 11.7M 13s
160500K .......... .......... .......... .......... .......... 61% 15.6M 13s
160550K .......... .......... .......... .......... .......... 61% 17.5M 13s
160600K .......... .......... .......... .......... .......... 61% 9.83M 13s
160650K .......... .......... .......... .......... .......... 61% 12.8M 13s
160700K .......... .......... .......... .......... .......... 61% 9.50M 13s
160750K .......... .......... .......... .......... .......... 61% 9.71M 13s
160800K .......... .......... .......... .......... .......... 61% 10.1M 13s
160850K .......... .......... .......... .......... .......... 61% 9.25M 13s
160900K .......... .......... .......... .......... .......... 61% 8.96M 13s
160950K .......... .......... .......... .......... .......... 61% 7.41M 13s
161000K .......... .......... .......... .......... .......... 61% 8.75M 13s
161050K .......... .......... .......... .......... .......... 61% 8.76M 13s
161100K .......... .......... .......... .......... .......... 61% 7.25M 13s
161150K .......... .......... .......... .......... .......... 61% 7.79M 13s
161200K .......... .......... .......... .......... .......... 61% 7.00M 13s
161250K .......... .......... .......... .......... .......... 61% 7.54M 13s
161300K .......... .......... .......... .......... .......... 61% 4.81M 13s
161350K .......... .......... .......... .......... .......... 61% 4.39M 13s
161400K .......... .......... .......... .......... .......... 61% 4.15M 13s
161450K .......... .......... .......... .......... .......... 61% 3.69M 13s
161500K .......... .......... .......... .......... .......... 61% 6.52M 13s
161550K .......... .......... .......... .......... .......... 61% 8.85M 13s
161600K .......... .......... .......... .......... .......... 61% 6.21M 13s
161650K .......... .......... .......... .......... .......... 61% 10.5M 13s
161700K .......... .......... .......... .......... .......... 61% 5.09M 13s
161750K .......... .......... .......... .......... .......... 61% 6.15M 13s
161800K .......... .......... .......... .......... .......... 61% 7.02M 13s
161850K .......... .......... .......... .......... .......... 61% 4.60M 13s
161900K .......... .......... .......... .......... .......... 61% 10.3M 13s
161950K .......... .......... .......... .......... .......... 61% 10.4M 13s
162000K .......... .......... .......... .......... .......... 61% 28.9M 13s
162050K .......... .......... .......... .......... .......... 61% 16.7M 13s
162100K .......... .......... .......... .......... .......... 61% 13.9M 13s
162150K .......... .......... .......... .......... .......... 61% 14.7M 13s
162200K .......... .......... .......... .......... .......... 61% 30.4M 13s
162250K .......... .......... .......... .......... .......... 61% 19.2M 13s
162300K .......... .......... .......... .......... .......... 61% 14.2M 13s
162350K .......... .......... .......... .......... .......... 61% 17.1M 13s
162400K .......... .......... .......... .......... .......... 61% 20.1M 13s
162450K .......... .......... .......... .......... .......... 61% 16.4M 13s
162500K .......... .......... .......... .......... .......... 61% 15.1M 13s
162550K .......... .......... .......... .......... .......... 62% 20.7M 13s
162600K .......... .......... .......... .......... .......... 62% 13.0M 13s
162650K .......... .......... .......... .......... .......... 62% 25.8M 13s
162700K .......... .......... .......... .......... .......... 62% 16.4M 13s
162750K .......... .......... .......... .......... .......... 62% 20.6M 13s
162800K .......... .......... .......... .......... .......... 62% 12.8M 13s
162850K .......... .......... .......... .......... .......... 62% 11.2M 13s
162900K .......... .......... .......... .......... .......... 62% 14.9M 13s
162950K .......... .......... .......... .......... .......... 62% 7.61M 13s
163000K .......... .......... .......... .......... .......... 62% 9.01M 13s
163050K .......... .......... .......... .......... .......... 62% 7.01M 13s
163100K .......... .......... .......... .......... .......... 62% 5.21M 13s
163150K .......... .......... .......... .......... .......... 62% 5.00M 13s
163200K .......... .......... .......... .......... .......... 62% 5.66M 13s
163250K .......... .......... .......... .......... .......... 62% 4.76M 13s
163300K .......... .......... .......... .......... .......... 62% 4.29M 13s
163350K .......... .......... .......... .......... .......... 62% 2.39M 13s
163400K .......... .......... .......... .......... .......... 62% 2.94M 13s
163450K .......... .......... .......... .......... .......... 62% 3.32M 13s
163500K .......... .......... .......... .......... .......... 62% 4.29M 13s
163550K .......... .......... .......... .......... .......... 62% 7.87M 13s
163600K .......... .......... .......... .......... .......... 62% 12.3M 13s
163650K .......... .......... .......... .......... .......... 62%  147M 13s
163700K .......... .......... .......... .......... .......... 62% 13.9M 13s
163750K .......... .......... .......... .......... .......... 62% 24.5M 13s
163800K .......... .......... .......... .......... .......... 62% 14.8M 13s
163850K .......... .......... .......... .......... .......... 62% 15.6M 13s
163900K .......... .......... .......... .......... .......... 62% 26.1M 13s
163950K .......... .......... .......... .......... .......... 62% 11.6M 13s
164000K .......... .......... .......... .......... .......... 62% 45.0M 13s
164050K .......... .......... .......... .......... .......... 62% 12.9M 13s
164100K .......... .......... .......... .......... .......... 62% 12.4M 13s
164150K .......... .......... .......... .......... .......... 62% 9.91M 13s
164200K .......... .......... .......... .......... .......... 62% 7.70M 13s
164250K .......... .......... .......... .......... .......... 62% 6.55M 13s
164300K .......... .......... .......... .......... .......... 62% 6.94M 13s
164350K .......... .......... .......... .......... .......... 62% 5.25M 13s
164400K .......... .......... .......... .......... .......... 62% 4.49M 13s
164450K .......... .......... .......... .......... .......... 62% 3.62M 13s
164500K .......... .......... .......... .......... .......... 62% 3.80M 13s
164550K .......... .......... .......... .......... .......... 62% 2.50M 13s
164600K .......... .......... .......... .......... .......... 62% 2.59M 13s
164650K .......... .......... .......... .......... .......... 62% 10.2M 13s
164700K .......... .......... .......... .......... .......... 62% 11.9M 13s
164750K .......... .......... .......... .......... .......... 62% 9.30M 13s
164800K .......... .......... .......... .......... .......... 62% 6.70M 13s
164850K .......... .......... .......... .......... .......... 62% 7.70M 13s
164900K .......... .......... .......... .......... .......... 62% 7.84M 13s
164950K .......... .......... .......... .......... .......... 62% 4.25M 13s
165000K .......... .......... .......... .......... .......... 62% 5.50M 13s
165050K .......... .......... .......... .......... .......... 62% 4.06M 13s
165100K .......... .......... .......... .......... .......... 62% 6.56M 13s
165150K .......... .......... .......... .......... .......... 63% 11.5M 13s
165200K .......... .......... .......... .......... .......... 63% 8.94M 13s
165250K .......... .......... .......... .......... .......... 63% 11.5M 13s
165300K .......... .......... .......... .......... .......... 63% 9.87M 13s
165350K .......... .......... .......... .......... .......... 63% 11.2M 13s
165400K .......... .......... .......... .......... .......... 63% 10.6M 13s
165450K .......... .......... .......... .......... .......... 63% 7.70M 13s
165500K .......... .......... .......... .......... .......... 63% 7.57M 13s
165550K .......... .......... .......... .......... .......... 63% 9.80M 13s
165600K .......... .......... .......... .......... .......... 63% 8.77M 13s
165650K .......... .......... .......... .......... .......... 63% 10.5M 13s
165700K .......... .......... .......... .......... .......... 63% 6.99M 13s
165750K .......... .......... .......... .......... .......... 63% 7.69M 13s
165800K .......... .......... .......... .......... .......... 63% 8.21M 13s
165850K .......... .......... .......... .......... .......... 63% 6.12M 13s
165900K .......... .......... .......... .......... .......... 63% 7.32M 13s
165950K .......... .......... .......... .......... .......... 63% 5.67M 13s
166000K .......... .......... .......... .......... .......... 63% 4.78M 13s
166050K .......... .......... .......... .......... .......... 63% 7.04M 13s
166100K .......... .......... .......... .......... .......... 63% 20.3M 13s
166150K .......... .......... .......... .......... .......... 63% 44.3M 13s
166200K .......... .......... .......... .......... .......... 63% 38.3M 13s
166250K .......... .......... .......... .......... .......... 63% 22.3M 13s
166300K .......... .......... .......... .......... .......... 63% 39.4M 13s
166350K .......... .......... .......... .......... .......... 63% 98.0M 13s
166400K .......... .......... .......... .......... .......... 63% 18.2M 13s
166450K .......... .......... .......... .......... .......... 63% 99.9M 12s
166500K .......... .......... .......... .......... .......... 63% 72.0M 12s
166550K .......... .......... .......... .......... .......... 63% 20.4M 12s
166600K .......... .......... .......... .......... .......... 63% 37.0M 12s
166650K .......... .......... .......... .......... .......... 63% 60.0M 12s
166700K .......... .......... .......... .......... .......... 63% 35.7M 12s
166750K .......... .......... .......... .......... .......... 63% 71.8M 12s
166800K .......... .......... .......... .......... .......... 63% 15.8M 12s
166850K .......... .......... .......... .......... .......... 63% 37.4M 12s
166900K .......... .......... .......... .......... .......... 63% 30.1M 12s
166950K .......... .......... .......... .......... .......... 63% 25.6M 12s
167000K .......... .......... .......... .......... .......... 63% 25.8M 12s
167050K .......... .......... .......... .......... .......... 63% 13.3M 12s
167100K .......... .......... .......... .......... .......... 63% 33.0M 12s
167150K .......... .......... .......... .......... .......... 63% 24.5M 12s
167200K .......... .......... .......... .......... .......... 63% 13.7M 12s
167250K .......... .......... .......... .......... .......... 63% 30.3M 12s
167300K .......... .......... .......... .......... .......... 63% 15.8M 12s
167350K .......... .......... .......... .......... .......... 63% 8.72M 12s
167400K .......... .......... .......... .......... .......... 63% 16.8M 12s
167450K .......... .......... .......... .......... .......... 63%  228K 12s
167500K .......... .......... .......... .......... .......... 63% 4.54M 12s
167550K .......... .......... .......... .......... .......... 63% 11.0M 12s
167600K .......... .......... .......... .......... .......... 63% 11.9M 12s
167650K .......... .......... .......... .......... .......... 63% 13.3M 12s
167700K .......... .......... .......... .......... .......... 63% 12.2M 12s
167750K .......... .......... .......... .......... .......... 63% 9.12M 12s
167800K .......... .......... .......... .......... .......... 64% 12.1M 12s
167850K .......... .......... .......... .......... .......... 64% 10.8M 12s
167900K .......... .......... .......... .......... .......... 64% 14.4M 12s
167950K .......... .......... .......... .......... .......... 64% 12.6M 12s
168000K .......... .......... .......... .......... .......... 64% 13.2M 12s
168050K .......... .......... .......... .......... .......... 64% 18.4M 12s
168100K .......... .......... .......... .......... .......... 64% 8.36M 12s
168150K .......... .......... .......... .......... .......... 64% 8.94M 12s
168200K .......... .......... .......... .......... .......... 64% 6.66M 12s
168250K .......... .......... .......... .......... .......... 64% 9.27M 12s
168300K .......... .......... .......... .......... .......... 64% 8.60M 12s
168350K .......... .......... .......... .......... .......... 64% 7.38M 12s
168400K .......... .......... .......... .......... .......... 64% 6.45M 12s
168450K .......... .......... .......... .......... .......... 64% 3.95M 12s
168500K .......... .......... .......... .......... .......... 64% 10.7M 12s
168550K .......... .......... .......... .......... .......... 64% 7.26M 12s
168600K .......... .......... .......... .......... .......... 64% 5.16M 12s
168650K .......... .......... .......... .......... .......... 64% 9.79M 12s
168700K .......... .......... .......... .......... .......... 64% 7.06M 12s
168750K .......... .......... .......... .......... .......... 64% 7.41M 12s
168800K .......... .......... .......... .......... .......... 64% 11.4M 12s
168850K .......... .......... .......... .......... .......... 64% 11.6M 12s
168900K .......... .......... .......... .......... .......... 64% 14.7M 12s
168950K .......... .......... .......... .......... .......... 64% 9.40M 12s
169000K .......... .......... .......... .......... .......... 64% 9.26M 12s
169050K .......... .......... .......... .......... .......... 64% 11.9M 12s
169100K .......... .......... .......... .......... .......... 64% 4.86M 12s
169150K .......... .......... .......... .......... .......... 64% 6.65M 12s
169200K .......... .......... .......... .......... .......... 64% 6.01M 12s
169250K .......... .......... .......... .......... .......... 64% 10.6M 12s
169300K .......... .......... .......... .......... .......... 64% 6.57M 12s
169350K .......... .......... .......... .......... .......... 64% 7.35M 12s
169400K .......... .......... .......... .......... .......... 64% 19.8M 12s
169450K .......... .......... .......... .......... .......... 64% 22.7M 12s
169500K .......... .......... .......... .......... .......... 64% 13.7M 12s
169550K .......... .......... .......... .......... .......... 64% 24.5M 12s
169600K .......... .......... .......... .......... .......... 64% 15.6M 12s
169650K .......... .......... .......... .......... .......... 64% 9.06M 12s
169700K .......... .......... .......... .......... .......... 64% 7.99M 12s
169750K .......... .......... .......... .......... .......... 64% 7.53M 12s
169800K .......... .......... .......... .......... .......... 64% 8.30M 12s
169850K .......... .......... .......... .......... .......... 64% 6.58M 12s
169900K .......... .......... .......... .......... .......... 64% 6.63M 12s
169950K .......... .......... .......... .......... .......... 64% 5.63M 12s
170000K .......... .......... .......... .......... .......... 64% 12.7M 12s
170050K .......... .......... .......... .......... .......... 64% 7.28M 12s
170100K .......... .......... .......... .......... .......... 64% 5.70M 12s
170150K .......... .......... .......... .......... .......... 64% 6.15M 12s
170200K .......... .......... .......... .......... .......... 64% 4.52M 12s
170250K .......... .......... .......... .......... .......... 64% 7.19M 12s
170300K .......... .......... .......... .......... .......... 64% 14.4M 12s
170350K .......... .......... .......... .......... .......... 64% 11.3M 12s
170400K .......... .......... .......... .......... .......... 65% 14.1M 12s
170450K .......... .......... .......... .......... .......... 65% 10.0M 12s
170500K .......... .......... .......... .......... .......... 65% 13.0M 12s
170550K .......... .......... .......... .......... .......... 65% 11.7M 12s
170600K .......... .......... .......... .......... .......... 65% 8.14M 12s
170650K .......... .......... .......... .......... .......... 65% 8.43M 12s
170700K .......... .......... .......... .......... .......... 65% 5.53M 12s
170750K .......... .......... .......... .......... .......... 65% 7.42M 12s
170800K .......... .......... .......... .......... .......... 65% 8.33M 12s
170850K .......... .......... .......... .......... .......... 65% 7.08M 12s
170900K .......... .......... .......... .......... .......... 65% 7.39M 12s
170950K .......... .......... .......... .......... .......... 65% 7.50M 12s
171000K .......... .......... .......... .......... .......... 65% 69.2M 12s
171050K .......... .......... .......... .......... .......... 65% 13.7M 12s
171100K .......... .......... .......... .......... .......... 65% 10.2M 12s
171150K .......... .......... .......... .......... .......... 65% 16.6M 12s
171200K .......... .......... .......... .......... .......... 65% 14.9M 12s
171250K .......... .......... .......... .......... .......... 65% 16.2M 12s
171300K .......... .......... .......... .......... .......... 65% 15.5M 12s
171350K .......... .......... .......... .......... .......... 65% 9.15M 12s
171400K .......... .......... .......... .......... .......... 65% 15.0M 12s
171450K .......... .......... .......... .......... .......... 65% 13.3M 12s
171500K .......... .......... .......... .......... .......... 65% 14.6M 12s
171550K .......... .......... .......... .......... .......... 65% 10.8M 12s
171600K .......... .......... .......... .......... .......... 65% 77.1M 12s
171650K .......... .......... .......... .......... .......... 65% 21.2M 12s
171700K .......... .......... .......... .......... .......... 65% 13.0M 12s
171750K .......... .......... .......... .......... .......... 65% 9.51M 12s
171800K .......... .......... .......... .......... .......... 65% 23.0M 12s
171850K .......... .......... .......... .......... .......... 65% 10.8M 12s
171900K .......... .......... .......... .......... .......... 65% 10.2M 12s
171950K .......... .......... .......... .......... .......... 65% 7.19M 12s
172000K .......... .......... .......... .......... .......... 65% 7.17M 12s
172050K .......... .......... .......... .......... .......... 65% 7.93M 12s
172100K .......... .......... .......... .......... .......... 65% 5.70M 12s
172150K .......... .......... .......... .......... .......... 65% 6.68M 12s
172200K .......... .......... .......... .......... .......... 65% 6.33M 12s
172250K .......... .......... .......... .......... .......... 65% 34.2M 12s
172300K .......... .......... .......... .......... .......... 65% 32.5M 12s
172350K .......... .......... .......... .......... .......... 65% 14.6M 12s
172400K .......... .......... .......... .......... .......... 65% 13.2M 12s
172450K .......... .......... .......... .......... .......... 65% 12.6M 12s
172500K .......... .......... .......... .......... .......... 65% 10.2M 12s
172550K .......... .......... .......... .......... .......... 65% 7.88M 12s
172600K .......... .......... .......... .......... .......... 65% 13.1M 12s
172650K .......... .......... .......... .......... .......... 65% 13.1M 12s
172700K .......... .......... .......... .......... .......... 65% 13.8M 12s
172750K .......... .......... .......... .......... .......... 65% 11.0M 12s
172800K .......... .......... .......... .......... .......... 65% 15.2M 12s
172850K .......... .......... .......... .......... .......... 65% 8.28M 12s
172900K .......... .......... .......... .......... .......... 65% 15.3M 12s
172950K .......... .......... .......... .......... .......... 65% 7.69M 12s
173000K .......... .......... .......... .......... .......... 66% 8.24M 12s
173050K .......... .......... .......... .......... .......... 66% 11.3M 12s
173100K .......... .......... .......... .......... .......... 66% 10.1M 12s
173150K .......... .......... .......... .......... .......... 66% 18.1M 12s
173200K .......... .......... .......... .......... .......... 66% 10.5M 12s
173250K .......... .......... .......... .......... .......... 66% 16.2M 12s
173300K .......... .......... .......... .......... .......... 66% 10.1M 12s
173350K .......... .......... .......... .......... .......... 66% 9.99M 12s
173400K .......... .......... .......... .......... .......... 66% 8.21M 12s
173450K .......... .......... .......... .......... .......... 66% 6.30M 12s
173500K .......... .......... .......... .......... .......... 66% 7.01M 12s
173550K .......... .......... .......... .......... .......... 66% 5.28M 12s
173600K .......... .......... .......... .......... .......... 66% 4.84M 12s
173650K .......... .......... .......... .......... .......... 66% 5.95M 12s
173700K .......... .......... .......... .......... .......... 66% 23.6M 12s
173750K .......... .......... .......... .......... .......... 66% 11.9M 12s
173800K .......... .......... .......... .......... .......... 66% 13.4M 12s
173850K .......... .......... .......... .......... .......... 66% 9.31M 12s
173900K .......... .......... .......... .......... .......... 66% 12.9M 12s
173950K .......... .......... .......... .......... .......... 66% 8.00M 11s
174000K .......... .......... .......... .......... .......... 66% 8.61M 11s
174050K .......... .......... .......... .......... .......... 66% 4.96M 11s
174100K .......... .......... .......... .......... .......... 66% 4.31M 11s
174150K .......... .......... .......... .......... .......... 66% 5.38M 11s
174200K .......... .......... .......... .......... .......... 66% 9.45M 11s
174250K .......... .......... .......... .......... .......... 66% 11.2M 11s
174300K .......... .......... .......... .......... .......... 66% 14.1M 11s
174350K .......... .......... .......... .......... .......... 66% 9.78M 11s
174400K .......... .......... .......... .......... .......... 66% 11.7M 11s
174450K .......... .......... .......... .......... .......... 66% 6.75M 11s
174500K .......... .......... .......... .......... .......... 66% 6.93M 11s
174550K .......... .......... .......... .......... .......... 66% 3.83M 11s
174600K .......... .......... .......... .......... .......... 66% 2.94M 11s
174650K .......... .......... .......... .......... .......... 66% 6.73M 11s
174700K .......... .......... .......... .......... .......... 66% 8.83M 11s
174750K .......... .......... .......... .......... .......... 66% 11.3M 11s
174800K .......... .......... .......... .......... .......... 66% 10.1M 11s
174850K .......... .......... .......... .......... .......... 66% 12.5M 11s
174900K .......... .......... .......... .......... .......... 66% 9.15M 11s
174950K .......... .......... .......... .......... .......... 66% 4.92M 11s
175000K .......... .......... .......... .......... .......... 66% 10.1M 11s
175050K .......... .......... .......... .......... .......... 66% 19.2M 11s
175100K .......... .......... .......... .......... .......... 66% 26.7M 11s
175150K .......... .......... .......... .......... .......... 66% 22.5M 11s
175200K .......... .......... .......... .......... .......... 66% 12.3M 11s
175250K .......... .......... .......... .......... .......... 66% 16.9M 11s
175300K .......... .......... .......... .......... .......... 66% 26.2M 11s
175350K .......... .......... .......... .......... .......... 66% 24.5M 11s
175400K .......... .......... .......... .......... .......... 66% 38.0M 11s
175450K .......... .......... .......... .......... .......... 66% 6.13M 11s
175500K .......... .......... .......... .......... .......... 66% 6.76M 11s
175550K .......... .......... .......... .......... .......... 66% 6.46M 11s
175600K .......... .......... .......... .......... .......... 66% 3.50M 11s
175650K .......... .......... .......... .......... .......... 67% 4.86M 11s
175700K .......... .......... .......... .......... .......... 67% 7.57M 11s
175750K .......... .......... .......... .......... .......... 67% 6.63M 11s
175800K .......... .......... .......... .......... .......... 67% 6.29M 11s
175850K .......... .......... .......... .......... .......... 67% 3.96M 11s
175900K .......... .......... .......... .......... .......... 67% 3.62M 11s
175950K .......... .......... .......... .......... .......... 67% 4.47M 11s
176000K .......... .......... .......... .......... .......... 67% 21.7M 11s
176050K .......... .......... .......... .......... .......... 67% 18.9M 11s
176100K .......... .......... .......... .......... .......... 67% 17.9M 11s
176150K .......... .......... .......... .......... .......... 67% 38.6M 11s
176200K .......... .......... .......... .......... .......... 67% 14.8M 11s
176250K .......... .......... .......... .......... .......... 67% 16.1M 11s
176300K .......... .......... .......... .......... .......... 67% 11.0M 11s
176350K .......... .......... .......... .......... .......... 67% 9.61M 11s
176400K .......... .......... .......... .......... .......... 67% 9.43M 11s
176450K .......... .......... .......... .......... .......... 67% 7.23M 11s
176500K .......... .......... .......... .......... .......... 67% 8.57M 11s
176550K .......... .......... .......... .......... .......... 67% 8.73M 11s
176600K .......... .......... .......... .......... .......... 67% 9.40M 11s
176650K .......... .......... .......... .......... .......... 67% 19.5M 11s
176700K .......... .......... .......... .......... .......... 67% 15.1M 11s
176750K .......... .......... .......... .......... .......... 67% 37.5M 11s
176800K .......... .......... .......... .......... .......... 67% 14.8M 11s
176850K .......... .......... .......... .......... .......... 67% 18.6M 11s
176900K .......... .......... .......... .......... .......... 67% 12.6M 11s
176950K .......... .......... .......... .......... .......... 67% 10.1M 11s
177000K .......... .......... .......... .......... .......... 67% 13.1M 11s
177050K .......... .......... .......... .......... .......... 67% 10.3M 11s
177100K .......... .......... .......... .......... .......... 67% 10.1M 11s
177150K .......... .......... .......... .......... .......... 67% 10.9M 11s
177200K .......... .......... .......... .......... .......... 67% 7.71M 11s
177250K .......... .......... .......... .......... .......... 67% 13.2M 11s
177300K .......... .......... .......... .......... .......... 67% 17.3M 11s
177350K .......... .......... .......... .......... .......... 67% 11.3M 11s
177400K .......... .......... .......... .......... .......... 67% 14.6M 11s
177450K .......... .......... .......... .......... .......... 67% 9.80M 11s
177500K .......... .......... .......... .......... .......... 67% 10.8M 11s
177550K .......... .......... .......... .......... .......... 67% 10.7M 11s
177600K .......... .......... .......... .......... .......... 67% 10.8M 11s
177650K .......... .......... .......... .......... .......... 67% 11.6M 11s
177700K .......... .......... .......... .......... .......... 67% 8.60M 11s
177750K .......... .......... .......... .......... .......... 67% 8.27M 11s
177800K .......... .......... .......... .......... .......... 67% 9.42M 11s
177850K .......... .......... .......... .......... .......... 67% 15.6M 11s
177900K .......... .......... .......... .......... .......... 67% 13.6M 11s
177950K .......... .......... .......... .......... .......... 67% 11.9M 11s
178000K .......... .......... .......... .......... .......... 67% 19.5M 11s
178050K .......... .......... .......... .......... .......... 67% 16.8M 11s
178100K .......... .......... .......... .......... .......... 67% 12.9M 11s
178150K .......... .......... .......... .......... .......... 67% 16.2M 11s
178200K .......... .......... .......... .......... .......... 67% 10.2M 11s
178250K .......... .......... .......... .......... .......... 68% 11.4M 11s
178300K .......... .......... .......... .......... .......... 68% 11.2M 11s
178350K .......... .......... .......... .......... .......... 68% 8.40M 11s
178400K .......... .......... .......... .......... .......... 68% 7.97M 11s
178450K .......... .......... .......... .......... .......... 68% 6.68M 11s
178500K .......... .......... .......... .......... .......... 68% 7.95M 11s
178550K .......... .......... .......... .......... .......... 68% 9.79M 11s
178600K .......... .......... .......... .......... .......... 68% 9.10M 11s
178650K .......... .......... .......... .......... .......... 68% 9.90M 11s
178700K .......... .......... .......... .......... .......... 68% 6.81M 11s
178750K .......... .......... .......... .......... .......... 68% 8.04M 11s
178800K .......... .......... .......... .......... .......... 68% 10.4M 11s
178850K .......... .......... .......... .......... .......... 68% 16.6M 11s
178900K .......... .......... .......... .......... .......... 68% 22.9M 11s
178950K .......... .......... .......... .......... .......... 68% 18.5M 11s
179000K .......... .......... .......... .......... .......... 68% 17.5M 11s
179050K .......... .......... .......... .......... .......... 68% 22.7M 11s
179100K .......... .......... .......... .......... .......... 68% 7.38M 11s
179150K .......... .......... .......... .......... .......... 68% 20.5M 11s
179200K .......... .......... .......... .......... .......... 68% 10.8M 11s
179250K .......... .......... .......... .......... .......... 68% 11.5M 11s
179300K .......... .......... .......... .......... .......... 68% 12.0M 11s
179350K .......... .......... .......... .......... .......... 68% 8.13M 11s
179400K .......... .......... .......... .......... .......... 68% 9.10M 11s
179450K .......... .......... .......... .......... .......... 68% 10.2M 11s
179500K .......... .......... .......... .......... .......... 68% 5.95M 11s
179550K .......... .......... .......... .......... .......... 68% 7.31M 11s
179600K .......... .......... .......... .......... .......... 68% 7.85M 11s
179650K .......... .......... .......... .......... .......... 68% 4.46M 11s
179700K .......... .......... .......... .......... .......... 68% 4.49M 11s
179750K .......... .......... .......... .......... .......... 68% 3.47M 11s
179800K .......... .......... .......... .......... .......... 68% 1.98M 11s
179850K .......... .......... .......... .......... .......... 68% 1.77M 11s
179900K .......... .......... .......... .......... .......... 68% 3.77M 11s
179950K .......... .......... .......... .......... .......... 68% 10.3M 11s
180000K .......... .......... .......... .......... .......... 68% 10.6M 11s
180050K .......... .......... .......... .......... .......... 68% 16.1M 11s
180100K .......... .......... .......... .......... .......... 68% 10.5M 11s
180150K .......... .......... .......... .......... .......... 68% 6.81M 11s
180200K .......... .......... .......... .......... .......... 68% 7.84M 11s
180250K .......... .......... .......... .......... .......... 68% 6.70M 11s
180300K .......... .......... .......... .......... .......... 68% 7.53M 11s
180350K .......... .......... .......... .......... .......... 68% 5.01M 11s
180400K .......... .......... .......... .......... .......... 68% 6.62M 11s
180450K .......... .......... .......... .......... .......... 68% 5.27M 11s
180500K .......... .......... .......... .......... .......... 68% 5.97M 11s
180550K .......... .......... .......... .......... .......... 68% 5.04M 11s
180600K .......... .......... .......... .......... .......... 68% 2.19M 11s
180650K .......... .......... .......... .......... .......... 68% 1.87M 11s
180700K .......... .......... .......... .......... .......... 68% 7.70M 11s
180750K .......... .......... .......... .......... .......... 68% 22.2M 11s
180800K .......... .......... .......... .......... .......... 68% 15.6M 11s
180850K .......... .......... .......... .......... .......... 68% 16.9M 11s
180900K .......... .......... .......... .......... .......... 69% 25.4M 11s
180950K .......... .......... .......... .......... .......... 69% 22.1M 11s
181000K .......... .......... .......... .......... .......... 69% 18.8M 11s
181050K .......... .......... .......... .......... .......... 69% 27.1M 11s
181100K .......... .......... .......... .......... .......... 69% 16.4M 11s
181150K .......... .......... .......... .......... .......... 69% 25.0M 11s
181200K .......... .......... .......... .......... .......... 69% 18.6M 11s
181250K .......... .......... .......... .......... .......... 69% 20.7M 11s
181300K .......... .......... .......... .......... .......... 69% 14.5M 10s
181350K .......... .......... .......... .......... .......... 69% 20.0M 10s
181400K .......... .......... .......... .......... .......... 69% 15.0M 10s
181450K .......... .......... .......... .......... .......... 69% 8.73M 10s
181500K .......... .......... .......... .......... .......... 69% 22.4M 10s
181550K .......... .......... .......... .......... .......... 69% 12.7M 10s
181600K .......... .......... .......... .......... .......... 69% 8.34M 10s
181650K .......... .......... .......... .......... .......... 69% 8.93M 10s
181700K .......... .......... .......... .......... .......... 69% 9.03M 10s
181750K .......... .......... .......... .......... .......... 69% 10.0M 10s
181800K .......... .......... .......... .......... .......... 69% 9.09M 10s
181850K .......... .......... .......... .......... .......... 69% 9.29M 10s
181900K .......... .......... .......... .......... .......... 69% 9.53M 10s
181950K .......... .......... .......... .......... .......... 69% 7.60M 10s
182000K .......... .......... .......... .......... .......... 69% 6.64M 10s
182050K .......... .......... .......... .......... .......... 69% 8.01M 10s
182100K .......... .......... .......... .......... .......... 69% 6.66M 10s
182150K .......... .......... .......... .......... .......... 69% 6.49M 10s
182200K .......... .......... .......... .......... .......... 69% 5.65M 10s
182250K .......... .......... .......... .......... .......... 69% 7.02M 10s
182300K .......... .......... .......... .......... .......... 69% 6.53M 10s
182350K .......... .......... .......... .......... .......... 69%  226K 10s
182400K .......... .......... .......... .......... .......... 69% 6.87M 10s
182450K .......... .......... .......... .......... .......... 69% 6.33M 10s
182500K .......... .......... .......... .......... .......... 69% 9.82M 10s
182550K .......... .......... .......... .......... .......... 69% 6.45M 10s
182600K .......... .......... .......... .......... .......... 69% 4.81M 10s
182650K .......... .......... .......... .......... .......... 69% 3.58M 10s
182700K .......... .......... .......... .......... .......... 69% 3.09M 10s
182750K .......... .......... .......... .......... .......... 69%  546K 10s
182800K .......... .......... .......... .......... .......... 69% 2.38M 10s
182850K .......... .......... .......... .......... .......... 69% 1.82M 10s
182900K .......... .......... .......... .......... .......... 69% 7.64M 10s
182950K .......... .......... .......... .......... .......... 69% 14.6M 10s
183000K .......... .......... .......... .......... .......... 69% 25.5M 10s
183050K .......... .......... .......... .......... .......... 69% 13.4M 10s
183100K .......... .......... .......... .......... .......... 69% 9.72M 10s
183150K .......... .......... .......... .......... .......... 69% 11.9M 10s
183200K .......... .......... .......... .......... .......... 69% 7.78M 10s
183250K .......... .......... .......... .......... .......... 69% 11.3M 10s
183300K .......... .......... .......... .......... .......... 69% 10.3M 10s
183350K .......... .......... .......... .......... .......... 69% 5.22M 10s
183400K .......... .......... .......... .......... .......... 69% 8.44M 10s
183450K .......... .......... .......... .......... .......... 69% 7.04M 10s
183500K .......... .......... .......... .......... .......... 70% 6.10M 10s
183550K .......... .......... .......... .......... .......... 70% 7.66M 10s
183600K .......... .......... .......... .......... .......... 70% 7.14M 10s
183650K .......... .......... .......... .......... .......... 70% 9.84M 10s
183700K .......... .......... .......... .......... .......... 70% 6.33M 10s
183750K .......... .......... .......... .......... .......... 70% 7.58M 10s
183800K .......... .......... .......... .......... .......... 70% 5.62M 10s
183850K .......... .......... .......... .......... .......... 70% 5.44M 10s
183900K .......... .......... .......... .......... .......... 70% 6.13M 10s
183950K .......... .......... .......... .......... .......... 70% 4.57M 10s
184000K .......... .......... .......... .......... .......... 70% 9.04M 10s
184050K .......... .......... .......... .......... .......... 70% 8.77M 10s
184100K .......... .......... .......... .......... .......... 70% 6.43M 10s
184150K .......... .......... .......... .......... .......... 70% 6.94M 10s
184200K .......... .......... .......... .......... .......... 70% 5.65M 10s
184250K .......... .......... .......... .......... .......... 70% 6.24M 10s
184300K .......... .......... .......... .......... .......... 70% 5.52M 10s
184350K .......... .......... .......... .......... .......... 70% 4.79M 10s
184400K .......... .......... .......... .......... .......... 70% 4.19M 10s
184450K .......... .......... .......... .......... .......... 70% 4.26M 10s
184500K .......... .......... .......... .......... .......... 70% 4.34M 10s
184550K .......... .......... .......... .......... .......... 70% 3.98M 10s
184600K .......... .......... .......... .......... .......... 70% 4.36M 10s
184650K .......... .......... .......... .......... .......... 70% 4.44M 10s
184700K .......... .......... .......... .......... .......... 70% 14.1M 10s
184750K .......... .......... .......... .......... .......... 70% 15.0M 10s
184800K .......... .......... .......... .......... .......... 70% 17.3M 10s
184850K .......... .......... .......... .......... .......... 70% 11.8M 10s
184900K .......... .......... .......... .......... .......... 70% 8.90M 10s
184950K .......... .......... .......... .......... .......... 70% 14.6M 10s
185000K .......... .......... .......... .......... .......... 70% 7.94M 10s
185050K .......... .......... .......... .......... .......... 70% 8.07M 10s
185100K .......... .......... .......... .......... .......... 70% 7.00M 10s
185150K .......... .......... .......... .......... .......... 70% 7.10M 10s
185200K .......... .......... .......... .......... .......... 70% 6.00M 10s
185250K .......... .......... .......... .......... .......... 70% 5.63M 10s
185300K .......... .......... .......... .......... .......... 70% 10.4M 10s
185350K .......... .......... .......... .......... .......... 70% 6.69M 10s
185400K .......... .......... .......... .......... .......... 70% 8.70M 10s
185450K .......... .......... .......... .......... .......... 70% 7.17M 10s
185500K .......... .......... .......... .......... .......... 70% 10.4M 10s
185550K .......... .......... .......... .......... .......... 70% 8.77M 10s
185600K .......... .......... .......... .......... .......... 70% 8.44M 10s
185650K .......... .......... .......... .......... .......... 70% 7.86M 10s
185700K .......... .......... .......... .......... .......... 70% 5.19M 10s
185750K .......... .......... .......... .......... .......... 70% 7.46M 10s
185800K .......... .......... .......... .......... .......... 70% 6.17M 10s
185850K .......... .......... .......... .......... .......... 70% 7.54M 10s
185900K .......... .......... .......... .......... .......... 70% 19.6M 10s
185950K .......... .......... .......... .......... .......... 70% 19.9M 10s
186000K .......... .......... .......... .......... .......... 70% 17.4M 10s
186050K .......... .......... .......... .......... .......... 70% 15.5M 10s
186100K .......... .......... .......... .......... .......... 70% 11.3M 10s
186150K .......... .......... .......... .......... .......... 71% 7.63M 10s
186200K .......... .......... .......... .......... .......... 71% 8.60M 10s
186250K .......... .......... .......... .......... .......... 71% 8.49M 10s
186300K .......... .......... .......... .......... .......... 71% 6.40M 10s
186350K .......... .......... .......... .......... .......... 71% 7.50M 10s
186400K .......... .......... .......... .......... .......... 71% 8.32M 10s
186450K .......... .......... .......... .......... .......... 71% 7.33M 10s
186500K .......... .......... .......... .......... .......... 71% 9.84M 10s
186550K .......... .......... .......... .......... .......... 71% 6.58M 10s
186600K .......... .......... .......... .......... .......... 71% 6.33M 10s
186650K .......... .......... .......... .......... .......... 71% 8.15M 10s
186700K .......... .......... .......... .......... .......... 71% 9.56M 10s
186750K .......... .......... .......... .......... .......... 71% 10.6M 10s
186800K .......... .......... .......... .......... .......... 71% 12.2M 10s
186850K .......... .......... .......... .......... .......... 71% 7.00M 10s
186900K .......... .......... .......... .......... .......... 71% 8.70M 10s
186950K .......... .......... .......... .......... .......... 71% 5.70M 10s
187000K .......... .......... .......... .......... .......... 71% 7.13M 10s
187050K .......... .......... .......... .......... .......... 71% 7.66M 10s
187100K .......... .......... .......... .......... .......... 71% 8.86M 10s
187150K .......... .......... .......... .......... .......... 71% 14.1M 10s
187200K .......... .......... .......... .......... .......... 71% 22.4M 10s
187250K .......... .......... .......... .......... .......... 71% 20.7M 10s
187300K .......... .......... .......... .......... .......... 71% 21.1M 10s
187350K .......... .......... .......... .......... .......... 71% 14.5M 10s
187400K .......... .......... .......... .......... .......... 71% 17.7M 10s
187450K .......... .......... .......... .......... .......... 71% 21.9M 10s
187500K .......... .......... .......... .......... .......... 71% 17.5M 10s
187550K .......... .......... .......... .......... .......... 71% 13.6M 10s
187600K .......... .......... .......... .......... .......... 71% 29.7M 10s
187650K .......... .......... .......... .......... .......... 71% 13.6M 10s
187700K .......... .......... .......... .......... .......... 71% 13.4M 10s
187750K .......... .......... .......... .......... .......... 71% 9.72M 10s
187800K .......... .......... .......... .......... .......... 71% 13.4M 10s
187850K .......... .......... .......... .......... .......... 71% 10.0M 10s
187900K .......... .......... .......... .......... .......... 71% 12.5M 10s
187950K .......... .......... .......... .......... .......... 71% 8.13M 10s
188000K .......... .......... .......... .......... .......... 71% 6.62M 10s
188050K .......... .......... .......... .......... .......... 71% 11.0M 10s
188100K .......... .......... .......... .......... .......... 71% 6.81M 10s
188150K .......... .......... .......... .......... .......... 71% 8.40M 10s
188200K .......... .......... .......... .......... .......... 71% 8.77M 10s
188250K .......... .......... .......... .......... .......... 71% 9.68M 10s
188300K .......... .......... .......... .......... .......... 71% 7.78M 10s
188350K .......... .......... .......... .......... .......... 71% 7.58M 10s
188400K .......... .......... .......... .......... .......... 71% 10.4M 10s
188450K .......... .......... .......... .......... .......... 71% 7.52M 10s
188500K .......... .......... .......... .......... .......... 71% 10.1M 10s
188550K .......... .......... .......... .......... .......... 71% 10.4M 10s
188600K .......... .......... .......... .......... .......... 71% 7.02M 10s
188650K .......... .......... .......... .......... .......... 71% 20.1M 10s
188700K .......... .......... .......... .......... .......... 71% 32.9M 10s
188750K .......... .......... .......... .......... .......... 72% 32.8M 10s
188800K .......... .......... .......... .......... .......... 72% 35.0M 10s
188850K .......... .......... .......... .......... .......... 72% 28.1M 10s
188900K .......... .......... .......... .......... .......... 72% 18.3M 10s
188950K .......... .......... .......... .......... .......... 72% 56.5M 10s
189000K .......... .......... .......... .......... .......... 72% 23.7M 10s
189050K .......... .......... .......... .......... .......... 72% 20.1M 10s
189100K .......... .......... .......... .......... .......... 72% 19.0M 10s
189150K .......... .......... .......... .......... .......... 72% 26.3M 10s
189200K .......... .......... .......... .......... .......... 72% 11.9M 10s
189250K .......... .......... .......... .......... .......... 72% 13.1M 10s
189300K .......... .......... .......... .......... .......... 72% 14.9M 10s
189350K .......... .......... .......... .......... .......... 72% 10.7M 10s
189400K .......... .......... .......... .......... .......... 72% 11.8M 10s
189450K .......... .......... .......... .......... .......... 72% 15.9M 10s
189500K .......... .......... .......... .......... .......... 72% 9.87M 10s
189550K .......... .......... .......... .......... .......... 72% 15.7M 10s
189600K .......... .......... .......... .......... .......... 72% 6.05M 9s
189650K .......... .......... .......... .......... .......... 72%  182M 9s
189700K .......... .......... .......... .......... .......... 72% 20.7M 9s
189750K .......... .......... .......... .......... .......... 72% 11.5M 9s
189800K .......... .......... .......... .......... .......... 72% 15.9M 9s
189850K .......... .......... .......... .......... .......... 72% 12.4M 9s
189900K .......... .......... .......... .......... .......... 72% 12.6M 9s
189950K .......... .......... .......... .......... .......... 72% 12.7M 9s
190000K .......... .......... .......... .......... .......... 72% 20.6M 9s
190050K .......... .......... .......... .......... .......... 72% 20.6M 9s
190100K .......... .......... .......... .......... .......... 72% 15.4M 9s
190150K .......... .......... .......... .......... .......... 72% 21.2M 9s
190200K .......... .......... .......... .......... .......... 72% 11.1M 9s
190250K .......... .......... .......... .......... .......... 72% 15.6M 9s
190300K .......... .......... .......... .......... .......... 72% 17.2M 9s
190350K .......... .......... .......... .......... .......... 72% 13.9M 9s
190400K .......... .......... .......... .......... .......... 72% 15.1M 9s
190450K .......... .......... .......... .......... .......... 72% 11.2M 9s
190500K .......... .......... .......... .......... .......... 72% 11.8M 9s
190550K .......... .......... .......... .......... .......... 72% 10.9M 9s
190600K .......... .......... .......... .......... .......... 72% 8.94M 9s
190650K .......... .......... .......... .......... .......... 72% 13.0M 9s
190700K .......... .......... .......... .......... .......... 72% 11.2M 9s
190750K .......... .......... .......... .......... .......... 72% 10.5M 9s
190800K .......... .......... .......... .......... .......... 72% 10.2M 9s
190850K .......... .......... .......... .......... .......... 72% 12.6M 9s
190900K .......... .......... .......... .......... .......... 72% 16.3M 9s
190950K .......... .......... .......... .......... .......... 72% 12.7M 9s
191000K .......... .......... .......... .......... .......... 72% 11.5M 9s
191050K .......... .......... .......... .......... .......... 72% 13.3M 9s
191100K .......... .......... .......... .......... .......... 72% 8.54M 9s
191150K .......... .......... .......... .......... .......... 72% 8.03M 9s
191200K .......... .......... .......... .......... .......... 72% 10.8M 9s
191250K .......... .......... .......... .......... .......... 72% 19.7M 9s
191300K .......... .......... .......... .......... .......... 72% 18.9M 9s
191350K .......... .......... .......... .......... .......... 73% 15.5M 9s
191400K .......... .......... .......... .......... .......... 73% 20.6M 9s
191450K .......... .......... .......... .......... .......... 73% 16.4M 9s
191500K .......... .......... .......... .......... .......... 73% 21.7M 9s
191550K .......... .......... .......... .......... .......... 73% 18.8M 9s
191600K .......... .......... .......... .......... .......... 73% 18.1M 9s
191650K .......... .......... .......... .......... .......... 73% 18.9M 9s
191700K .......... .......... .......... .......... .......... 73% 18.0M 9s
191750K .......... .......... .......... .......... .......... 73% 12.8M 9s
191800K .......... .......... .......... .......... .......... 73% 15.5M 9s
191850K .......... .......... .......... .......... .......... 73% 12.2M 9s
191900K .......... .......... .......... .......... .......... 73% 11.8M 9s
191950K .......... .......... .......... .......... .......... 73% 13.4M 9s
192000K .......... .......... .......... .......... .......... 73% 13.3M 9s
192050K .......... .......... .......... .......... .......... 73% 11.1M 9s
192100K .......... .......... .......... .......... .......... 73% 19.8M 9s
192150K .......... .......... .......... .......... .......... 73% 20.7M 9s
192200K .......... .......... .......... .......... .......... 73% 16.1M 9s
192250K .......... .......... .......... .......... .......... 73% 15.8M 9s
192300K .......... .......... .......... .......... .......... 73% 10.9M 9s
192350K .......... .......... .......... .......... .......... 73% 9.70M 9s
192400K .......... .......... .......... .......... .......... 73% 13.0M 9s
192450K .......... .......... .......... .......... .......... 73% 8.47M 9s
192500K .......... .......... .......... .......... .......... 73% 15.4M 9s
192550K .......... .......... .......... .......... .......... 73% 20.8M 9s
192600K .......... .......... .......... .......... .......... 73% 12.8M 9s
192650K .......... .......... .......... .......... .......... 73% 13.6M 9s
192700K .......... .......... .......... .......... .......... 73% 10.7M 9s
192750K .......... .......... .......... .......... .......... 73% 15.5M 9s
192800K .......... .......... .......... .......... .......... 73% 12.8M 9s
192850K .......... .......... .......... .......... .......... 73% 11.2M 9s
192900K .......... .......... .......... .......... .......... 73% 9.67M 9s
192950K .......... .......... .......... .......... .......... 73% 6.07M 9s
193000K .......... .......... .......... .......... .......... 73% 9.04M 9s
193050K .......... .......... .......... .......... .......... 73% 9.30M 9s
193100K .......... .......... .......... .......... .......... 73% 13.9M 9s
193150K .......... .......... .......... .......... .......... 73% 9.55M 9s
193200K .......... .......... .......... .......... .......... 73% 11.4M 9s
193250K .......... .......... .......... .......... .......... 73% 10.0M 9s
193300K .......... .......... .......... .......... .......... 73% 17.1M 9s
193350K .......... .......... .......... .......... .......... 73% 13.3M 9s
193400K .......... .......... .......... .......... .......... 73% 18.7M 9s
193450K .......... .......... .......... .......... .......... 73% 13.5M 9s
193500K .......... .......... .......... .......... .......... 73% 14.6M 9s
193550K .......... .......... .......... .......... .......... 73% 9.36M 9s
193600K .......... .......... .......... .......... .......... 73% 10.9M 9s
193650K .......... .......... .......... .......... .......... 73% 8.86M 9s
193700K .......... .......... .......... .......... .......... 73% 7.35M 9s
193750K .......... .......... .......... .......... .......... 73% 8.74M 9s
193800K .......... .......... .......... .......... .......... 73% 10.3M 9s
193850K .......... .......... .......... .......... .......... 73% 6.68M 9s
193900K .......... .......... .......... .......... .......... 73% 8.96M 9s
193950K .......... .......... .......... .......... .......... 73% 9.14M 9s
194000K .......... .......... .......... .......... .......... 74% 10.7M 9s
194050K .......... .......... .......... .......... .......... 74% 9.93M 9s
194100K .......... .......... .......... .......... .......... 74% 10.5M 9s
194150K .......... .......... .......... .......... .......... 74% 9.60M 9s
194200K .......... .......... .......... .......... .......... 74% 13.3M 9s
194250K .......... .......... .......... .......... .......... 74% 12.3M 9s
194300K .......... .......... .......... .......... .......... 74% 8.35M 9s
194350K .......... .......... .......... .......... .......... 74% 6.13M 9s
194400K .......... .......... .......... .......... .......... 74% 8.84M 9s
194450K .......... .......... .......... .......... .......... 74% 7.91M 9s
194500K .......... .......... .......... .......... .......... 74% 10.9M 9s
194550K .......... .......... .......... .......... .......... 74% 9.21M 9s
194600K .......... .......... .......... .......... .......... 74% 8.40M 9s
194650K .......... .......... .......... .......... .......... 74% 10.4M 9s
194700K .......... .......... .......... .......... .......... 74% 10.3M 9s
194750K .......... .......... .......... .......... .......... 74% 9.48M 9s
194800K .......... .......... .......... .......... .......... 74% 10.6M 9s
194850K .......... .......... .......... .......... .......... 74% 10.6M 9s
194900K .......... .......... .......... .......... .......... 74% 31.9M 9s
194950K .......... .......... .......... .......... .......... 74% 38.0M 9s
195000K .......... .......... .......... .......... .......... 74% 28.3M 9s
195050K .......... .......... .......... .......... .......... 74% 24.3M 9s
195100K .......... .......... .......... .......... .......... 74% 20.1M 9s
195150K .......... .......... .......... .......... .......... 74% 27.0M 9s
195200K .......... .......... .......... .......... .......... 74% 23.0M 9s
195250K .......... .......... .......... .......... .......... 74% 22.3M 9s
195300K .......... .......... .......... .......... .......... 74% 24.2M 9s
195350K .......... .......... .......... .......... .......... 74% 16.3M 9s
195400K .......... .......... .......... .......... .......... 74% 21.9M 9s
195450K .......... .......... .......... .......... .......... 74% 18.6M 9s
195500K .......... .......... .......... .......... .......... 74% 14.5M 9s
195550K .......... .......... .......... .......... .......... 74% 12.6M 9s
195600K .......... .......... .......... .......... .......... 74% 11.3M 9s
195650K .......... .......... .......... .......... .......... 74% 16.2M 9s
195700K .......... .......... .......... .......... .......... 74% 17.2M 9s
195750K .......... .......... .......... .......... .......... 74% 15.0M 9s
195800K .......... .......... .......... .......... .......... 74% 23.1M 9s
195850K .......... .......... .......... .......... .......... 74% 16.7M 9s
195900K .......... .......... .......... .......... .......... 74% 16.2M 9s
195950K .......... .......... .......... .......... .......... 74% 11.2M 9s
196000K .......... .......... .......... .......... .......... 74% 8.63M 9s
196050K .......... .......... .......... .......... .......... 74% 6.63M 9s
196100K .......... .......... .......... .......... .......... 74% 4.99M 9s
196150K .......... .......... .......... .......... .......... 74% 5.30M 9s
196200K .......... .......... .......... .......... .......... 74% 3.81M 9s
196250K .......... .......... .......... .......... .......... 74% 3.73M 9s
196300K .......... .......... .......... .......... .......... 74% 3.63M 9s
196350K .......... .......... .......... .......... .......... 74% 1.10M 9s
196400K .......... .......... .......... .......... .......... 74% 3.37M 9s
196450K .......... .......... .......... .......... .......... 74% 3.98M 9s
196500K .......... .......... .......... .......... .......... 74% 4.45M 9s
196550K .......... .......... .......... .......... .......... 74% 3.63M 9s
196600K .......... .......... .......... .......... .......... 75% 4.79M 8s
196650K .......... .......... .......... .......... .......... 75% 20.9M 8s
196700K .......... .......... .......... .......... .......... 75% 23.5M 8s
196750K .......... .......... .......... .......... .......... 75% 29.1M 8s
196800K .......... .......... .......... .......... .......... 75% 51.6M 8s
196850K .......... .......... .......... .......... .......... 75% 24.7M 8s
196900K .......... .......... .......... .......... .......... 75% 23.0M 8s
196950K .......... .......... .......... .......... .......... 75% 21.8M 8s
197000K .......... .......... .......... .......... .......... 75% 16.3M 8s
197050K .......... .......... .......... .......... .......... 75% 30.8M 8s
197100K .......... .......... .......... .......... .......... 75% 21.0M 8s
197150K .......... .......... .......... .......... .......... 75% 18.8M 8s
197200K .......... .......... .......... .......... .......... 75% 9.87M 8s
197250K .......... .......... .......... .......... .......... 75% 16.2M 8s
197300K .......... .......... .......... .......... .......... 75% 14.9M 8s
197350K .......... .......... .......... .......... .......... 75% 8.81M 8s
197400K .......... .......... .......... .......... .......... 75% 8.96M 8s
197450K .......... .......... .......... .......... .......... 75% 5.88M 8s
197500K .......... .......... .......... .......... .......... 75% 6.14M 8s
197550K .......... .......... .......... .......... .......... 75% 6.85M 8s
197600K .......... .......... .......... .......... .......... 75% 4.01M 8s
197650K .......... .......... .......... .......... .......... 75% 6.45M 8s
197700K .......... .......... .......... .......... .......... 75% 5.61M 8s
197750K .......... .......... .......... .......... .......... 75% 8.27M 8s
197800K .......... .......... .......... .......... .......... 75% 17.7M 8s
197850K .......... .......... .......... .......... .......... 75% 26.3M 8s
197900K .......... .......... .......... .......... .......... 75% 20.5M 8s
197950K .......... .......... .......... .......... .......... 75% 22.2M 8s
198000K .......... .......... .......... .......... .......... 75% 38.7M 8s
198050K .......... .......... .......... .......... .......... 75% 15.4M 8s
198100K .......... .......... .......... .......... .......... 75% 17.5M 8s
198150K .......... .......... .......... .......... .......... 75% 18.6M 8s
198200K .......... .......... .......... .......... .......... 75% 14.1M 8s
198250K .......... .......... .......... .......... .......... 75% 17.7M 8s
198300K .......... .......... .......... .......... .......... 75% 18.3M 8s
198350K .......... .......... .......... .......... .......... 75% 14.7M 8s
198400K .......... .......... .......... .......... .......... 75% 10.8M 8s
198450K .......... .......... .......... .......... .......... 75% 10.1M 8s
198500K .......... .......... .......... .......... .......... 75% 11.4M 8s
198550K .......... .......... .......... .......... .......... 75% 11.6M 8s
198600K .......... .......... .......... .......... .......... 75% 11.1M 8s
198650K .......... .......... .......... .......... .......... 75% 11.8M 8s
198700K .......... .......... .......... .......... .......... 75% 8.76M 8s
198750K .......... .......... .......... .......... .......... 75% 12.8M 8s
198800K .......... .......... .......... .......... .......... 75% 15.9M 8s
198850K .......... .......... .......... .......... .......... 75% 14.2M 8s
198900K .......... .......... .......... .......... .......... 75% 20.9M 8s
198950K .......... .......... .......... .......... .......... 75% 15.3M 8s
199000K .......... .......... .......... .......... .......... 75% 10.9M 8s
199050K .......... .......... .......... .......... .......... 75% 10.0M 8s
199100K .......... .......... .......... .......... .......... 75% 5.02M 8s
199150K .......... .......... .......... .......... .......... 75% 5.01M 8s
199200K .......... .......... .......... .......... .......... 75% 8.51M 8s
199250K .......... .......... .......... .......... .......... 76% 12.0M 8s
199300K .......... .......... .......... .......... .......... 76% 12.2M 8s
199350K .......... .......... .......... .......... .......... 76% 9.38M 8s
199400K .......... .......... .......... .......... .......... 76% 2.60M 8s
199450K .......... .......... .......... .......... .......... 76% 9.73M 8s
199500K .......... .......... .......... .......... .......... 76% 10.9M 8s
199550K .......... .......... .......... .......... .......... 76% 13.0M 8s
199600K .......... .......... .......... .......... .......... 76% 9.67M 8s
199650K .......... .......... .......... .......... .......... 76% 11.3M 8s
199700K .......... .......... .......... .......... .......... 76% 8.23M 8s
199750K .......... .......... .......... .......... .......... 76% 13.7M 8s
199800K .......... .......... .......... .......... .......... 76% 15.0M 8s
199850K .......... .......... .......... .......... .......... 76% 9.87M 8s
199900K .......... .......... .......... .......... .......... 76% 10.2M 8s
199950K .......... .......... .......... .......... .......... 76% 9.88M 8s
200000K .......... .......... .......... .......... .......... 76% 10.3M 8s
200050K .......... .......... .......... .......... .......... 76% 11.0M 8s
200100K .......... .......... .......... .......... .......... 76% 10.2M 8s
200150K .......... .......... .......... .......... .......... 76% 12.5M 8s
200200K .......... .......... .......... .......... .......... 76% 29.7M 8s
200250K .......... .......... .......... .......... .......... 76% 22.3M 8s
200300K .......... .......... .......... .......... .......... 76% 15.4M 8s
200350K .......... .......... .......... .......... .......... 76% 16.6M 8s
200400K .......... .......... .......... .......... .......... 76% 9.80M 8s
200450K .......... .......... .......... .......... .......... 76% 12.8M 8s
200500K .......... .......... .......... .......... .......... 76% 13.9M 8s
200550K .......... .......... .......... .......... .......... 76% 16.3M 8s
200600K .......... .......... .......... .......... .......... 76% 12.5M 8s
200650K .......... .......... .......... .......... .......... 76% 13.6M 8s
200700K .......... .......... .......... .......... .......... 76% 7.00M 8s
200750K .......... .......... .......... .......... .......... 76% 5.23M 8s
200800K .......... .......... .......... .......... .......... 76% 7.28M 8s
200850K .......... .......... .......... .......... .......... 76% 6.84M 8s
200900K .......... .......... .......... .......... .......... 76% 8.27M 8s
200950K .......... .......... .......... .......... .......... 76% 6.05M 8s
201000K .......... .......... .......... .......... .......... 76% 6.39M 8s
201050K .......... .......... .......... .......... .......... 76% 8.16M 8s
201100K .......... .......... .......... .......... .......... 76% 5.95M 8s
201150K .......... .......... .......... .......... .......... 76% 9.13M 8s
201200K .......... .......... .......... .......... .......... 76% 5.72M 8s
201250K .......... .......... .......... .......... .......... 76% 6.60M 8s
201300K .......... .......... .......... .......... .......... 76% 6.76M 8s
201350K .......... .......... .......... .......... .......... 76% 6.91M 8s
201400K .......... .......... .......... .......... .......... 76% 18.1M 8s
201450K .......... .......... .......... .......... .......... 76% 18.8M 8s
201500K .......... .......... .......... .......... .......... 76% 59.3M 8s
201550K .......... .......... .......... .......... .......... 76% 14.6M 8s
201600K .......... .......... .......... .......... .......... 76% 10.2M 8s
201650K .......... .......... .......... .......... .......... 76% 9.45M 8s
201700K .......... .......... .......... .......... .......... 76% 13.7M 8s
201750K .......... .......... .......... .......... .......... 76% 9.62M 8s
201800K .......... .......... .......... .......... .......... 76% 11.0M 8s
201850K .......... .......... .......... .......... .......... 77% 8.21M 8s
201900K .......... .......... .......... .......... .......... 77% 9.53M 8s
201950K .......... .......... .......... .......... .......... 77% 6.12M 8s
202000K .......... .......... .......... .......... .......... 77% 8.15M 8s
202050K .......... .......... .......... .......... .......... 77% 6.86M 8s
202100K .......... .......... .......... .......... .......... 77% 6.73M 8s
202150K .......... .......... .......... .......... .......... 77% 6.49M 8s
202200K .......... .......... .......... .......... .......... 77% 4.12M 8s
202250K .......... .......... .......... .......... .......... 77% 4.35M 8s
202300K .......... .......... .......... .......... .......... 77% 4.57M 8s
202350K .......... .......... .......... .......... .......... 77% 3.19M 8s
202400K .......... .......... .......... .......... .......... 77% 4.02M 8s
202450K .......... .......... .......... .......... .......... 77% 5.15M 8s
202500K .......... .......... .......... .......... .......... 77% 14.7M 8s
202550K .......... .......... .......... .......... .......... 77% 27.9M 8s
202600K .......... .......... .......... .......... .......... 77% 16.2M 8s
202650K .......... .......... .......... .......... .......... 77% 16.3M 8s
202700K .......... .......... .......... .......... .......... 77% 24.2M 8s
202750K .......... .......... .......... .......... .......... 77% 28.5M 8s
202800K .......... .......... .......... .......... .......... 77% 35.7M 8s
202850K .......... .......... .......... .......... .......... 77% 19.7M 8s
202900K .......... .......... .......... .......... .......... 77% 23.9M 8s
202950K .......... .......... .......... .......... .......... 77% 33.6M 8s
203000K .......... .......... .......... .......... .......... 77% 20.6M 8s
203050K .......... .......... .......... .......... .......... 77% 28.3M 8s
203100K .......... .......... .......... .......... .......... 77% 9.48M 8s
203150K .......... .......... .......... .......... .......... 77% 57.0M 8s
203200K .......... .......... .......... .......... .......... 77% 13.5M 8s
203250K .......... .......... .......... .......... .......... 77% 10.9M 8s
203300K .......... .......... .......... .......... .......... 77% 10.5M 8s
203350K .......... .......... .......... .......... .......... 77% 7.45M 8s
203400K .......... .......... .......... .......... .......... 77% 9.02M 8s
203450K .......... .......... .......... .......... .......... 77% 7.94M 8s
203500K .......... .......... .......... .......... .......... 77% 7.25M 8s
203550K .......... .......... .......... .......... .......... 77% 6.75M 8s
203600K .......... .......... .......... .......... .......... 77% 6.84M 8s
203650K .......... .......... .......... .......... .......... 77% 13.8M 8s
203700K .......... .......... .......... .......... .......... 77% 9.40M 8s
203750K .......... .......... .......... .......... .......... 77% 46.5M 8s
203800K .......... .......... .......... .......... .......... 77% 14.2M 7s
203850K .......... .......... .......... .......... .......... 77% 15.8M 7s
203900K .......... .......... .......... .......... .......... 77% 13.8M 7s
203950K .......... .......... .......... .......... .......... 77% 9.83M 7s
204000K .......... .......... .......... .......... .......... 77% 15.1M 7s
204050K .......... .......... .......... .......... .......... 77% 11.0M 7s
204100K .......... .......... .......... .......... .......... 77% 8.04M 7s
204150K .......... .......... .......... .......... .......... 77% 14.1M 7s
204200K .......... .......... .......... .......... .......... 77% 9.43M 7s
204250K .......... .......... .......... .......... .......... 77% 9.06M 7s
204300K .......... .......... .......... .......... .......... 77% 8.71M 7s
204350K .......... .......... .......... .......... .......... 77% 9.21M 7s
204400K .......... .......... .......... .......... .......... 77% 11.0M 7s
204450K .......... .......... .......... .......... .......... 77% 11.9M 7s
204500K .......... .......... .......... .......... .......... 78% 13.7M 7s
204550K .......... .......... .......... .......... .......... 78% 13.0M 7s
204600K .......... .......... .......... .......... .......... 78% 10.6M 7s
204650K .......... .......... .......... .......... .......... 78% 13.5M 7s
204700K .......... .......... .......... .......... .......... 78% 10.7M 7s
204750K .......... .......... .......... .......... .......... 78% 7.82M 7s
204800K .......... .......... .......... .......... .......... 78% 5.92M 7s
204850K .......... .......... .......... .......... .......... 78% 5.11M 7s
204900K .......... .......... .......... .......... .......... 78% 4.36M 7s
204950K .......... .......... .......... .......... .......... 78% 3.20M 7s
205000K .......... .......... .......... .......... .......... 78% 5.92M 7s
205050K .......... .......... .......... .......... .......... 78% 6.00M 7s
205100K .......... .......... .......... .......... .......... 78% 5.66M 7s
205150K .......... .......... .......... .......... .......... 78% 4.89M 7s
205200K .......... .......... .......... .......... .......... 78% 4.84M 7s
205250K .......... .......... .......... .......... .......... 78% 6.08M 7s
205300K .......... .......... .......... .......... .......... 78% 6.12M 7s
205350K .......... .......... .......... .......... .......... 78% 5.78M 7s
205400K .......... .......... .......... .......... .......... 78% 8.73M 7s
205450K .......... .......... .......... .......... .......... 78% 8.89M 7s
205500K .......... .......... .......... .......... .......... 78% 8.26M 7s
205550K .......... .......... .......... .......... .......... 78% 8.97M 7s
205600K .......... .......... .......... .......... .......... 78% 6.96M 7s
205650K .......... .......... .......... .......... .......... 78% 9.34M 7s
205700K .......... .......... .......... .......... .......... 78% 9.58M 7s
205750K .......... .......... .......... .......... .......... 78% 27.4M 7s
205800K .......... .......... .......... .......... .......... 78% 18.3M 7s
205850K .......... .......... .......... .......... .......... 78% 17.2M 7s
205900K .......... .......... .......... .......... .......... 78% 15.9M 7s
205950K .......... .......... .......... .......... .......... 78% 15.3M 7s
206000K .......... .......... .......... .......... .......... 78% 14.8M 7s
206050K .......... .......... .......... .......... .......... 78% 9.31M 7s
206100K .......... .......... .......... .......... .......... 78% 9.86M 7s
206150K .......... .......... .......... .......... .......... 78% 10.2M 7s
206200K .......... .......... .......... .......... .......... 78% 9.92M 7s
206250K .......... .......... .......... .......... .......... 78% 13.2M 7s
206300K .......... .......... .......... .......... .......... 78% 14.8M 7s
206350K .......... .......... .......... .......... .......... 78% 13.0M 7s
206400K .......... .......... .......... .......... .......... 78% 9.97M 7s
206450K .......... .......... .......... .......... .......... 78% 9.40M 7s
206500K .......... .......... .......... .......... .......... 78% 6.68M 7s
206550K .......... .......... .......... .......... .......... 78% 8.60M 7s
206600K .......... .......... .......... .......... .......... 78% 7.04M 7s
206650K .......... .......... .......... .......... .......... 78% 7.02M 7s
206700K .......... .......... .......... .......... .......... 78% 10.2M 7s
206750K .......... .......... .......... .......... .......... 78% 11.3M 7s
206800K .......... .......... .......... .......... .......... 78% 9.17M 7s
206850K .......... .......... .......... .......... .......... 78% 5.70M 7s
206900K .......... .......... .......... .......... .......... 78% 4.70M 7s
206950K .......... .......... .......... .......... .......... 78% 4.67M 7s
207000K .......... .......... .......... .......... .......... 78% 13.6M 7s
207050K .......... .......... .......... .......... .......... 78% 13.4M 7s
207100K .......... .......... .......... .......... .......... 79% 12.4M 7s
207150K .......... .......... .......... .......... .......... 79% 12.7M 7s
207200K .......... .......... .......... .......... .......... 79% 9.71M 7s
207250K .......... .......... .......... .......... .......... 79% 9.32M 7s
207300K .......... .......... .......... .......... .......... 79% 11.9M 7s
207350K .......... .......... .......... .......... .......... 79% 5.46M 7s
207400K .......... .......... .......... .......... .......... 79% 6.62M 7s
207450K .......... .......... .......... .......... .......... 79% 6.30M 7s
207500K .......... .......... .......... .......... .......... 79% 6.60M 7s
207550K .......... .......... .......... .......... .......... 79% 7.34M 7s
207600K .......... .......... .......... .......... .......... 79% 10.3M 7s
207650K .......... .......... .......... .......... .......... 79% 9.69M 7s
207700K .......... .......... .......... .......... .......... 79% 6.69M 7s
207750K .......... .......... .......... .......... .......... 79% 8.88M 7s
207800K .......... .......... .......... .......... .......... 79% 8.14M 7s
207850K .......... .......... .......... .......... .......... 79% 5.74M 7s
207900K .......... .......... .......... .......... .......... 79% 5.99M 7s
207950K .......... .......... .......... .......... .......... 79% 6.69M 7s
208000K .......... .......... .......... .......... .......... 79% 6.20M 7s
208050K .......... .......... .......... .......... .......... 79% 6.08M 7s
208100K .......... .......... .......... .......... .......... 79% 6.09M 7s
208150K .......... .......... .......... .......... .......... 79% 8.68M 7s
208200K .......... .......... .......... .......... .......... 79% 11.0M 7s
208250K .......... .......... .......... .......... .......... 79% 17.6M 7s
208300K .......... .......... .......... .......... .......... 79% 17.9M 7s
208350K .......... .......... .......... .......... .......... 79% 12.1M 7s
208400K .......... .......... .......... .......... .......... 79% 13.7M 7s
208450K .......... .......... .......... .......... .......... 79% 8.66M 7s
208500K .......... .......... .......... .......... .......... 79% 10.2M 7s
208550K .......... .......... .......... .......... .......... 79% 10.5M 7s
208600K .......... .......... .......... .......... .......... 79% 5.97M 7s
208650K .......... .......... .......... .......... .......... 79% 11.9M 7s
208700K .......... .......... .......... .......... .......... 79% 8.59M 7s
208750K .......... .......... .......... .......... .......... 79% 10.8M 7s
208800K .......... .......... .......... .......... .......... 79% 10.4M 7s
208850K .......... .......... .......... .......... .......... 79% 9.70M 7s
208900K .......... .......... .......... .......... .......... 79% 10.5M 7s
208950K .......... .......... .......... .......... .......... 79% 10.1M 7s
209000K .......... .......... .......... .......... .......... 79% 9.98M 7s
209050K .......... .......... .......... .......... .......... 79% 5.01M 7s
209100K .......... .......... .......... .......... .......... 79% 28.1M 7s
209150K .......... .......... .......... .......... .......... 79% 19.9M 7s
209200K .......... .......... .......... .......... .......... 79% 15.3M 7s
209250K .......... .......... .......... .......... .......... 79% 15.2M 7s
209300K .......... .......... .......... .......... .......... 79% 20.5M 7s
209350K .......... .......... .......... .......... .......... 79% 11.7M 7s
209400K .......... .......... .......... .......... .......... 79% 13.0M 7s
209450K .......... .......... .......... .......... .......... 79% 12.9M 7s
209500K .......... .......... .......... .......... .......... 79% 8.92M 7s
209550K .......... .......... .......... .......... .......... 79% 8.01M 7s
209600K .......... .......... .......... .......... .......... 79% 4.72M 7s
209650K .......... .......... .......... .......... .......... 79% 5.18M 7s
209700K .......... .......... .......... .......... .......... 79% 5.42M 7s
209750K .......... .......... .......... .......... .......... 80% 5.24M 7s
209800K .......... .......... .......... .......... .......... 80% 8.99M 7s
209850K .......... .......... .......... .......... .......... 80% 8.04M 7s
209900K .......... .......... .......... .......... .......... 80% 9.03M 7s
209950K .......... .......... .......... .......... .......... 80% 10.5M 7s
210000K .......... .......... .......... .......... .......... 80% 11.5M 7s
210050K .......... .......... .......... .......... .......... 80% 10.0M 7s
210100K .......... .......... .......... .......... .......... 80% 8.27M 7s
210150K .......... .......... .......... .......... .......... 80% 10.4M 7s
210200K .......... .......... .......... .......... .......... 80% 7.83M 7s
210250K .......... .......... .......... .......... .......... 80% 17.4M 7s
210300K .......... .......... .......... .......... .......... 80% 15.6M 7s
210350K .......... .......... .......... .......... .......... 80% 7.19M 7s
210400K .......... .......... .......... .......... .......... 80% 7.29M 7s
210450K .......... .......... .......... .......... .......... 80% 5.99M 7s
210500K .......... .......... .......... .......... .......... 80% 9.27M 7s
210550K .......... .......... .......... .......... .......... 80% 10.6M 7s
210600K .......... .......... .......... .......... .......... 80% 9.35M 7s
210650K .......... .......... .......... .......... .......... 80% 9.62M 7s
210700K .......... .......... .......... .......... .......... 80% 9.77M 7s
210750K .......... .......... .......... .......... .......... 80% 8.59M 7s
210800K .......... .......... .......... .......... .......... 80% 7.18M 7s
210850K .......... .......... .......... .......... .......... 80% 14.6M 7s
210900K .......... .......... .......... .......... .......... 80% 16.0M 7s
210950K .......... .......... .......... .......... .......... 80% 23.2M 7s
211000K .......... .......... .......... .......... .......... 80% 17.3M 7s
211050K .......... .......... .......... .......... .......... 80% 23.1M 7s
211100K .......... .......... .......... .......... .......... 80% 14.3M 7s
211150K .......... .......... .......... .......... .......... 80% 24.9M 7s
211200K .......... .......... .......... .......... .......... 80% 15.4M 7s
211250K .......... .......... .......... .......... .......... 80% 10.5M 7s
211300K .......... .......... .......... .......... .......... 80% 40.7M 6s
211350K .......... .......... .......... .......... .......... 80% 6.86M 6s
211400K .......... .......... .......... .......... .......... 80% 10.1M 6s
211450K .......... .......... .......... .......... .......... 80% 9.06M 6s
211500K .......... .......... .......... .......... .......... 80% 8.42M 6s
211550K .......... .......... .......... .......... .......... 80% 8.35M 6s
211600K .......... .......... .......... .......... .......... 80% 7.71M 6s
211650K .......... .......... .......... .......... .......... 80% 8.55M 6s
211700K .......... .......... .......... .......... .......... 80% 6.83M 6s
211750K .......... .......... .......... .......... .......... 80% 9.81M 6s
211800K .......... .......... .......... .......... .......... 80% 6.94M 6s
211850K .......... .......... .......... .......... .......... 80% 9.48M 6s
211900K .......... .......... .......... .......... .......... 80% 9.70M 6s
211950K .......... .......... .......... .......... .......... 80% 8.77M 6s
212000K .......... .......... .......... .......... .......... 80% 7.80M 6s
212050K .......... .......... .......... .......... .......... 80% 7.97M 6s
212100K .......... .......... .......... .......... .......... 80% 5.32M 6s
212150K .......... .......... .......... .......... .......... 80% 7.37M 6s
212200K .......... .......... .......... .......... .......... 80% 6.70M 6s
212250K .......... .......... .......... .......... .......... 80% 6.43M 6s
212300K .......... .......... .......... .......... .......... 80% 6.43M 6s
212350K .......... .......... .......... .......... .......... 81% 8.91M 6s
212400K .......... .......... .......... .......... .......... 81% 15.9M 6s
212450K .......... .......... .......... .......... .......... 81% 15.2M 6s
212500K .......... .......... .......... .......... .......... 81% 9.26M 6s
212550K .......... .......... .......... .......... .......... 81% 32.5M 6s
212600K .......... .......... .......... .......... .......... 81% 11.7M 6s
212650K .......... .......... .......... .......... .......... 81% 12.0M 6s
212700K .......... .......... .......... .......... .......... 81% 10.8M 6s
212750K .......... .......... .......... .......... .......... 81% 20.7M 6s
212800K .......... .......... .......... .......... .......... 81% 11.9M 6s
212850K .......... .......... .......... .......... .......... 81% 10.0M 6s
212900K .......... .......... .......... .......... .......... 81% 13.9M 6s
212950K .......... .......... .......... .......... .......... 81% 8.15M 6s
213000K .......... .......... .......... .......... .......... 81% 9.65M 6s
213050K .......... .......... .......... .......... .......... 81% 46.1M 6s
213100K .......... .......... .......... .......... .......... 81% 26.1M 6s
213150K .......... .......... .......... .......... .......... 81% 12.9M 6s
213200K .......... .......... .......... .......... .......... 81% 12.1M 6s
213250K .......... .......... .......... .......... .......... 81% 10.8M 6s
213300K .......... .......... .......... .......... .......... 81% 13.8M 6s
213350K .......... .......... .......... .......... .......... 81% 12.4M 6s
213400K .......... .......... .......... .......... .......... 81% 10.5M 6s
213450K .......... .......... .......... .......... .......... 81% 10.9M 6s
213500K .......... .......... .......... .......... .......... 81% 13.2M 6s
213550K .......... .......... .......... .......... .......... 81% 11.2M 6s
213600K .......... .......... .......... .......... .......... 81% 11.1M 6s
213650K .......... .......... .......... .......... .......... 81% 6.02M 6s
213700K .......... .......... .......... .......... .......... 81% 7.59M 6s
213750K .......... .......... .......... .......... .......... 81% 7.33M 6s
213800K .......... .......... .......... .......... .......... 81% 7.73M 6s
213850K .......... .......... .......... .......... .......... 81% 5.85M 6s
213900K .......... .......... .......... .......... .......... 81% 6.99M 6s
213950K .......... .......... .......... .......... .......... 81% 10.6M 6s
214000K .......... .......... .......... .......... .......... 81% 12.1M 6s
214050K .......... .......... .......... .......... .......... 81% 16.5M 6s
214100K .......... .......... .......... .......... .......... 81% 10.4M 6s
214150K .......... .......... .......... .......... .......... 81% 12.9M 6s
214200K .......... .......... .......... .......... .......... 81% 11.9M 6s
214250K .......... .......... .......... .......... .......... 81% 9.74M 6s
214300K .......... .......... .......... .......... .......... 81% 10.5M 6s
214350K .......... .......... .......... .......... .......... 81% 8.31M 6s
214400K .......... .......... .......... .......... .......... 81% 9.51M 6s
214450K .......... .......... .......... .......... .......... 81% 9.63M 6s
214500K .......... .......... .......... .......... .......... 81% 9.71M 6s
214550K .......... .......... .......... .......... .......... 81% 7.80M 6s
214600K .......... .......... .......... .......... .......... 81% 7.57M 6s
214650K .......... .......... .......... .......... .......... 81% 7.01M 6s
214700K .......... .......... .......... .......... .......... 81% 5.70M 6s
214750K .......... .......... .......... .......... .......... 81% 6.28M 6s
214800K .......... .......... .......... .......... .......... 81% 6.55M 6s
214850K .......... .......... .......... .......... .......... 81% 4.01M 6s
214900K .......... .......... .......... .......... .......... 81% 4.97M 6s
214950K .......... .......... .......... .......... .......... 82% 4.76M 6s
215000K .......... .......... .......... .......... .......... 82% 5.50M 6s
215050K .......... .......... .......... .......... .......... 82% 5.13M 6s
215100K .......... .......... .......... .......... .......... 82% 11.7M 6s
215150K .......... .......... .......... .......... .......... 82% 9.43M 6s
215200K .......... .......... .......... .......... .......... 82% 10.1M 6s
215250K .......... .......... .......... .......... .......... 82% 10.2M 6s
215300K .......... .......... .......... .......... .......... 82% 10.5M 6s
215350K .......... .......... .......... .......... .......... 82% 6.32M 6s
215400K .......... .......... .......... .......... .......... 82% 9.11M 6s
215450K .......... .......... .......... .......... .......... 82% 8.78M 6s
215500K .......... .......... .......... .......... .......... 82% 13.1M 6s
215550K .......... .......... .......... .......... .......... 82% 10.5M 6s
215600K .......... .......... .......... .......... .......... 82% 26.0M 6s
215650K .......... .......... .......... .......... .......... 82% 22.7M 6s
215700K .......... .......... .......... .......... .......... 82% 12.2M 6s
215750K .......... .......... .......... .......... .......... 82% 8.48M 6s
215800K .......... .......... .......... .......... .......... 82% 87.7M 6s
215850K .......... .......... .......... .......... .......... 82% 15.7M 6s
215900K .......... .......... .......... .......... .......... 82% 9.13M 6s
215950K .......... .......... .......... .......... .......... 82% 17.8M 6s
216000K .......... .......... .......... .......... .......... 82% 11.7M 6s
216050K .......... .......... .......... .......... .......... 82% 13.0M 6s
216100K .......... .......... .......... .......... .......... 82% 10.0M 6s
216150K .......... .......... .......... .......... .......... 82% 12.4M 6s
216200K .......... .......... .......... .......... .......... 82% 11.0M 6s
216250K .......... .......... .......... .......... .......... 82% 12.4M 6s
216300K .......... .......... .......... .......... .......... 82% 10.4M 6s
216350K .......... .......... .......... .......... .......... 82% 12.1M 6s
216400K .......... .......... .......... .......... .......... 82% 13.1M 6s
216450K .......... .......... .......... .......... .......... 82% 10.3M 6s
216500K .......... .......... .......... .......... .......... 82% 9.13M 6s
216550K .......... .......... .......... .......... .......... 82% 19.3M 6s
216600K .......... .......... .......... .......... .......... 82% 14.2M 6s
216650K .......... .......... .......... .......... .......... 82% 13.7M 6s
216700K .......... .......... .......... .......... .......... 82% 8.18M 6s
216750K .......... .......... .......... .......... .......... 82% 9.67M 6s
216800K .......... .......... .......... .......... .......... 82% 9.70M 6s
216850K .......... .......... .......... .......... .......... 82% 7.07M 6s
216900K .......... .......... .......... .......... .......... 82% 7.45M 6s
216950K .......... .......... .......... .......... .......... 82% 4.68M 6s
217000K .......... .......... .......... .......... .......... 82% 4.84M 6s
217050K .......... .......... .......... .......... .......... 82% 3.80M 6s
217100K .......... .......... .......... .......... .......... 82% 2.58M 6s
217150K .......... .......... .......... .......... .......... 82% 3.18M 6s
217200K .......... .......... .......... .......... .......... 82%  214K 6s
217250K .......... .......... .......... .......... .......... 82% 11.8M 6s
217300K .......... .......... .......... .......... .......... 82% 16.1M 6s
217350K .......... .......... .......... .......... .......... 82% 15.3M 6s
217400K .......... .......... .......... .......... .......... 82% 16.0M 6s
217450K .......... .......... .......... .......... .......... 82% 13.6M 6s
217500K .......... .......... .......... .......... .......... 82% 16.3M 6s
217550K .......... .......... .......... .......... .......... 82% 13.3M 6s
217600K .......... .......... .......... .......... .......... 83% 17.6M 6s
217650K .......... .......... .......... .......... .......... 83% 16.5M 6s
217700K .......... .......... .......... .......... .......... 83% 9.02M 6s
217750K .......... .......... .......... .......... .......... 83% 9.76M 6s
217800K .......... .......... .......... .......... .......... 83% 11.2M 6s
217850K .......... .......... .......... .......... .......... 83% 8.73M 6s
217900K .......... .......... .......... .......... .......... 83% 10.7M 6s
217950K .......... .......... .......... .......... .......... 83% 8.19M 6s
218000K .......... .......... .......... .......... .......... 83% 10.0M 6s
218050K .......... .......... .......... .......... .......... 83% 7.02M 6s
218100K .......... .......... .......... .......... .......... 83% 12.8M 6s
218150K .......... .......... .......... .......... .......... 83% 7.99M 6s
218200K .......... .......... .......... .......... .......... 83% 8.08M 6s
218250K .......... .......... .......... .......... .......... 83% 8.77M 6s
218300K .......... .......... .......... .......... .......... 83% 6.29M 6s
218350K .......... .......... .......... .......... .......... 83% 4.10M 6s
218400K .......... .......... .......... .......... .......... 83% 9.12M 6s
218450K .......... .......... .......... .......... .......... 83% 13.4M 6s
218500K .......... .......... .......... .......... .......... 83% 8.55M 6s
218550K .......... .......... .......... .......... .......... 83% 27.3M 6s
218600K .......... .......... .......... .......... .......... 83% 12.5M 6s
218650K .......... .......... .......... .......... .......... 83% 8.32M 6s
218700K .......... .......... .......... .......... .......... 83% 14.3M 6s
218750K .......... .......... .......... .......... .......... 83% 7.78M 6s
218800K .......... .......... .......... .......... .......... 83% 6.94M 6s
218850K .......... .......... .......... .......... .......... 83% 7.89M 6s
218900K .......... .......... .......... .......... .......... 83% 9.83M 6s
218950K .......... .......... .......... .......... .......... 83% 8.52M 6s
219000K .......... .......... .......... .......... .......... 83% 11.4M 6s
219050K .......... .......... .......... .......... .......... 83% 7.86M 6s
219100K .......... .......... .......... .......... .......... 83% 5.75M 6s
219150K .......... .......... .......... .......... .......... 83% 6.46M 6s
219200K .......... .......... .......... .......... .......... 83% 5.25M 6s
219250K .......... .......... .......... .......... .......... 83% 5.28M 5s
219300K .......... .......... .......... .......... .......... 83% 6.32M 5s
219350K .......... .......... .......... .......... .......... 83% 4.70M 5s
219400K .......... .......... .......... .......... .......... 83% 7.41M 5s
219450K .......... .......... .......... .......... .......... 83% 5.99M 5s
219500K .......... .......... .......... .......... .......... 83% 8.24M 5s
219550K .......... .......... .......... .......... .......... 83% 4.30M 5s
219600K .......... .......... .......... .......... .......... 83% 4.01M 5s
219650K .......... .......... .......... .......... .......... 83% 4.21M 5s
219700K .......... .......... .......... .......... .......... 83% 6.80M 5s
219750K .......... .......... .......... .......... .......... 83% 11.5M 5s
219800K .......... .......... .......... .......... .......... 83% 9.24M 5s
219850K .......... .......... .......... .......... .......... 83% 5.96M 5s
219900K .......... .......... .......... .......... .......... 83% 7.92M 5s
219950K .......... .......... .......... .......... .......... 83% 5.83M 5s
220000K .......... .......... .......... .......... .......... 83% 6.36M 5s
220050K .......... .......... .......... .......... .......... 83% 8.20M 5s
220100K .......... .......... .......... .......... .......... 83% 4.39M 5s
220150K .......... .......... .......... .......... .......... 83% 5.23M 5s
220200K .......... .......... .......... .......... .......... 84% 3.53M 5s
220250K .......... .......... .......... .......... .......... 84% 5.95M 5s
220300K .......... .......... .......... .......... .......... 84% 3.68M 5s
220350K .......... .......... .......... .......... .......... 84% 3.45M 5s
220400K .......... .......... .......... .......... .......... 84% 4.52M 5s
220450K .......... .......... .......... .......... .......... 84% 4.69M 5s
220500K .......... .......... .......... .......... .......... 84% 5.85M 5s
220550K .......... .......... .......... .......... .......... 84% 4.05M 5s
220600K .......... .......... .......... .......... .......... 84% 3.27M 5s
220650K .......... .......... .......... .......... .......... 84% 3.94M 5s
220700K .......... .......... .......... .......... .......... 84% 5.33M 5s
220750K .......... .......... .......... .......... .......... 84% 11.0M 5s
220800K .......... .......... .......... .......... .......... 84% 5.97M 5s
220850K .......... .......... .......... .......... .......... 84% 4.68M 5s
220900K .......... .......... .......... .......... .......... 84% 3.83M 5s
220950K .......... .......... .......... .......... .......... 84% 3.15M 5s
221000K .......... .......... .......... .......... .......... 84% 5.07M 5s
221050K .......... .......... .......... .......... .......... 84% 7.37M 5s
221100K .......... .......... .......... .......... .......... 84% 9.52M 5s
221150K .......... .......... .......... .......... .......... 84% 8.44M 5s
221200K .......... .......... .......... .......... .......... 84% 5.99M 5s
221250K .......... .......... .......... .......... .......... 84% 7.75M 5s
221300K .......... .......... .......... .......... .......... 84% 6.03M 5s
221350K .......... .......... .......... .......... .......... 84% 7.57M 5s
221400K .......... .......... .......... .......... .......... 84% 7.79M 5s
221450K .......... .......... .......... .......... .......... 84% 6.35M 5s
221500K .......... .......... .......... .......... .......... 84% 5.31M 5s
221550K .......... .......... .......... .......... .......... 84% 6.97M 5s
221600K .......... .......... .......... .......... .......... 84% 5.80M 5s
221650K .......... .......... .......... .......... .......... 84% 5.33M 5s
221700K .......... .......... .......... .......... .......... 84% 6.37M 5s
221750K .......... .......... .......... .......... .......... 84% 7.86M 5s
221800K .......... .......... .......... .......... .......... 84% 8.95M 5s
221850K .......... .......... .......... .......... .......... 84% 4.55M 5s
221900K .......... .......... .......... .......... .......... 84% 5.55M 5s
221950K .......... .......... .......... .......... .......... 84% 4.24M 5s
222000K .......... .......... .......... .......... .......... 84% 6.76M 5s
222050K .......... .......... .......... .......... .......... 84% 13.0M 5s
222100K .......... .......... .......... .......... .......... 84% 19.2M 5s
222150K .......... .......... .......... .......... .......... 84% 23.6M 5s
222200K .......... .......... .......... .......... .......... 84% 14.2M 5s
222250K .......... .......... .......... .......... .......... 84%  131M 5s
222300K .......... .......... .......... .......... .......... 84% 22.2M 5s
222350K .......... .......... .......... .......... .......... 84% 23.4M 5s
222400K .......... .......... .......... .......... .......... 84% 16.8M 5s
222450K .......... .......... .......... .......... .......... 84% 30.2M 5s
222500K .......... .......... .......... .......... .......... 84% 19.0M 5s
222550K .......... .......... .......... .......... .......... 84% 22.3M 5s
222600K .......... .......... .......... .......... .......... 84% 12.8M 5s
222650K .......... .......... .......... .......... .......... 84% 12.1M 5s
222700K .......... .......... .......... .......... .......... 84% 18.7M 5s
222750K .......... .......... .......... .......... .......... 84% 13.4M 5s
222800K .......... .......... .......... .......... .......... 84% 12.7M 5s
222850K .......... .......... .......... .......... .......... 85% 15.3M 5s
222900K .......... .......... .......... .......... .......... 85% 18.6M 5s
222950K .......... .......... .......... .......... .......... 85% 13.0M 5s
223000K .......... .......... .......... .......... .......... 85% 10.2M 5s
223050K .......... .......... .......... .......... .......... 85% 7.78M 5s
223100K .......... .......... .......... .......... .......... 85% 6.32M 5s
223150K .......... .......... .......... .......... .......... 85% 7.87M 5s
223200K .......... .......... .......... .......... .......... 85% 8.23M 5s
223250K .......... .......... .......... .......... .......... 85% 7.70M 5s
223300K .......... .......... .......... .......... .......... 85% 5.31M 5s
223350K .......... .......... .......... .......... .......... 85% 6.11M 5s
223400K .......... .......... .......... .......... .......... 85% 5.47M 5s
223450K .......... .......... .......... .......... .......... 85% 4.55M 5s
223500K .......... .......... .......... .......... .......... 85% 12.3M 5s
223550K .......... .......... .......... .......... .......... 85% 9.06M 5s
223600K .......... .......... .......... .......... .......... 85% 8.09M 5s
223650K .......... .......... .......... .......... .......... 85% 6.93M 5s
223700K .......... .......... .......... .......... .......... 85% 14.0M 5s
223750K .......... .......... .......... .......... .......... 85% 15.2M 5s
223800K .......... .......... .......... .......... .......... 85% 7.72M 5s
223850K .......... .......... .......... .......... .......... 85% 11.8M 5s
223900K .......... .......... .......... .......... .......... 85% 7.93M 5s
223950K .......... .......... .......... .......... .......... 85% 9.24M 5s
224000K .......... .......... .......... .......... .......... 85% 8.63M 5s
224050K .......... .......... .......... .......... .......... 85% 9.20M 5s
224100K .......... .......... .......... .......... .......... 85% 8.31M 5s
224150K .......... .......... .......... .......... .......... 85% 10.2M 5s
224200K .......... .......... .......... .......... .......... 85% 6.35M 5s
224250K .......... .......... .......... .......... .......... 85% 6.74M 5s
224300K .......... .......... .......... .......... .......... 85% 8.12M 5s
224350K .......... .......... .......... .......... .......... 85% 7.54M 5s
224400K .......... .......... .......... .......... .......... 85% 8.34M 5s
224450K .......... .......... .......... .......... .......... 85% 6.98M 5s
224500K .......... .......... .......... .......... .......... 85% 8.92M 5s
224550K .......... .......... .......... .......... .......... 85% 10.2M 5s
224600K .......... .......... .......... .......... .......... 85% 10.9M 5s
224650K .......... .......... .......... .......... .......... 85% 12.1M 5s
224700K .......... .......... .......... .......... .......... 85% 11.9M 5s
224750K .......... .......... .......... .......... .......... 85% 13.6M 5s
224800K .......... .......... .......... .......... .......... 85% 13.0M 5s
224850K .......... .......... .......... .......... .......... 85% 11.8M 5s
224900K .......... .......... .......... .......... .......... 85% 14.6M 5s
224950K .......... .......... .......... .......... .......... 85% 11.3M 5s
225000K .......... .......... .......... .......... .......... 85% 20.0M 5s
225050K .......... .......... .......... .......... .......... 85% 26.9M 5s
225100K .......... .......... .......... .......... .......... 85% 38.3M 5s
225150K .......... .......... .......... .......... .......... 85% 17.5M 5s
225200K .......... .......... .......... .......... .......... 85% 90.6M 5s
225250K .......... .......... .......... .......... .......... 85% 50.0M 5s
225300K .......... .......... .......... .......... .......... 85% 57.9M 5s
225350K .......... .......... .......... .......... .......... 85% 16.5M 5s
225400K .......... .......... .......... .......... .......... 85% 36.4M 5s
225450K .......... .......... .......... .......... .......... 86% 11.5M 5s
225500K .......... .......... .......... .......... .......... 86% 14.9M 5s
225550K .......... .......... .......... .......... .......... 86% 15.0M 5s
225600K .......... .......... .......... .......... .......... 86% 12.8M 5s
225650K .......... .......... .......... .......... .......... 86% 12.3M 5s
225700K .......... .......... .......... .......... .......... 86% 8.88M 5s
225750K .......... .......... .......... .......... .......... 86% 10.5M 5s
225800K .......... .......... .......... .......... .......... 86% 10.0M 5s
225850K .......... .......... .......... .......... .......... 86% 9.41M 5s
225900K .......... .......... .......... .......... .......... 86% 12.9M 5s
225950K .......... .......... .......... .......... .......... 86% 9.90M 5s
226000K .......... .......... .......... .......... .......... 86% 15.4M 5s
226050K .......... .......... .......... .......... .......... 86% 18.2M 5s
226100K .......... .......... .......... .......... .......... 86% 16.1M 5s
226150K .......... .......... .......... .......... .......... 86% 15.8M 5s
226200K .......... .......... .......... .......... .......... 86% 19.8M 5s
226250K .......... .......... .......... .......... .......... 86% 14.6M 5s
226300K .......... .......... .......... .......... .......... 86% 8.88M 5s
226350K .......... .......... .......... .......... .......... 86% 36.5M 5s
226400K .......... .......... .......... .......... .......... 86% 12.2M 5s
226450K .......... .......... .......... .......... .......... 86% 12.5M 5s
226500K .......... .......... .......... .......... .......... 86% 13.8M 5s
226550K .......... .......... .......... .......... .......... 86% 22.5M 5s
226600K .......... .......... .......... .......... .......... 86% 16.1M 5s
226650K .......... .......... .......... .......... .......... 86% 12.3M 5s
226700K .......... .......... .......... .......... .......... 86% 8.82M 5s
226750K .......... .......... .......... .......... .......... 86% 10.6M 5s
226800K .......... .......... .......... .......... .......... 86% 9.06M 5s
226850K .......... .......... .......... .......... .......... 86% 7.76M 5s
226900K .......... .......... .......... .......... .......... 86% 9.28M 5s
226950K .......... .......... .......... .......... .......... 86% 8.49M 4s
227000K .......... .......... .......... .......... .......... 86% 7.00M 4s
227050K .......... .......... .......... .......... .......... 86% 8.13M 4s
227100K .......... .......... .......... .......... .......... 86% 5.92M 4s
227150K .......... .......... .......... .......... .......... 86% 11.0M 4s
227200K .......... .......... .......... .......... .......... 86% 8.66M 4s
227250K .......... .......... .......... .......... .......... 86% 10.8M 4s
227300K .......... .......... .......... .......... .......... 86% 11.8M 4s
227350K .......... .......... .......... .......... .......... 86% 7.18M 4s
227400K .......... .......... .......... .......... .......... 86% 10.4M 4s
227450K .......... .......... .......... .......... .......... 86% 6.01M 4s
227500K .......... .......... .......... .......... .......... 86% 7.10M 4s
227550K .......... .......... .......... .......... .......... 86% 7.15M 4s
227600K .......... .......... .......... .......... .......... 86% 8.17M 4s
227650K .......... .......... .......... .......... .......... 86% 46.0M 4s
227700K .......... .......... .......... .......... .......... 86% 20.6M 4s
227750K .......... .......... .......... .......... .......... 86% 42.2M 4s
227800K .......... .......... .......... .......... .......... 86% 34.3M 4s
227850K .......... .......... .......... .......... .......... 86% 17.6M 4s
227900K .......... .......... .......... .......... .......... 86% 22.1M 4s
227950K .......... .......... .......... .......... .......... 86% 19.7M 4s
228000K .......... .......... .......... .......... .......... 86% 17.6M 4s
228050K .......... .......... .......... .......... .......... 86% 16.0M 4s
228100K .......... .......... .......... .......... .......... 87% 16.3M 4s
228150K .......... .......... .......... .......... .......... 87% 15.0M 4s
228200K .......... .......... .......... .......... .......... 87% 11.8M 4s
228250K .......... .......... .......... .......... .......... 87% 10.4M 4s
228300K .......... .......... .......... .......... .......... 87% 30.6M 4s
228350K .......... .......... .......... .......... .......... 87% 11.5M 4s
228400K .......... .......... .......... .......... .......... 87% 8.33M 4s
228450K .......... .......... .......... .......... .......... 87% 8.25M 4s
228500K .......... .......... .......... .......... .......... 87% 7.23M 4s
228550K .......... .......... .......... .......... .......... 87% 9.48M 4s
228600K .......... .......... .......... .......... .......... 87% 8.76M 4s
228650K .......... .......... .......... .......... .......... 87% 7.28M 4s
228700K .......... .......... .......... .......... .......... 87% 13.5M 4s
228750K .......... .......... .......... .......... .......... 87% 10.3M 4s
228800K .......... .......... .......... .......... .......... 87% 11.5M 4s
228850K .......... .......... .......... .......... .......... 87% 6.87M 4s
228900K .......... .......... .......... .......... .......... 87% 5.87M 4s
228950K .......... .......... .......... .......... .......... 87% 6.30M 4s
229000K .......... .......... .......... .......... .......... 87% 3.82M 4s
229050K .......... .......... .......... .......... .......... 87% 3.51M 4s
229100K .......... .......... .......... .......... .......... 87% 3.63M 4s
229150K .......... .......... .......... .......... .......... 87% 2.92M 4s
229200K .......... .......... .......... .......... .......... 87% 2.45M 4s
229250K .......... .......... .......... .......... .......... 87% 5.25M 4s
229300K .......... .......... .......... .......... .......... 87% 10.9M 4s
229350K .......... .......... .......... .......... .......... 87% 10.5M 4s
229400K .......... .......... .......... .......... .......... 87% 12.7M 4s
229450K .......... .......... .......... .......... .......... 87% 9.59M 4s
229500K .......... .......... .......... .......... .......... 87% 11.6M 4s
229550K .......... .......... .......... .......... .......... 87% 10.9M 4s
229600K .......... .......... .......... .......... .......... 87% 9.06M 4s
229650K .......... .......... .......... .......... .......... 87% 9.28M 4s
229700K .......... .......... .......... .......... .......... 87% 26.3M 4s
229750K .......... .......... .......... .......... .......... 87% 19.9M 4s
229800K .......... .......... .......... .......... .......... 87% 10.2M 4s
229850K .......... .......... .......... .......... .......... 87% 13.2M 4s
229900K .......... .......... .......... .......... .......... 87% 12.7M 4s
229950K .......... .......... .......... .......... .......... 87% 9.70M 4s
230000K .......... .......... .......... .......... .......... 87% 13.1M 4s
230050K .......... .......... .......... .......... .......... 87% 9.17M 4s
230100K .......... .......... .......... .......... .......... 87% 9.64M 4s
230150K .......... .......... .......... .......... .......... 87% 8.06M 4s
230200K .......... .......... .......... .......... .......... 87% 6.43M 4s
230250K .......... .......... .......... .......... .......... 87% 9.73M 4s
230300K .......... .......... .......... .......... .......... 87% 7.72M 4s
230350K .......... .......... .......... .......... .......... 87% 6.53M 4s
230400K .......... .......... .......... .......... .......... 87% 7.24M 4s
230450K .......... .......... .......... .......... .......... 87% 4.79M 4s
230500K .......... .......... .......... .......... .......... 87% 4.98M 4s
230550K .......... .......... .......... .......... .......... 87% 5.10M 4s
230600K .......... .......... .......... .......... .......... 87% 5.98M 4s
230650K .......... .......... .......... .......... .......... 87% 10.0M 4s
230700K .......... .......... .......... .......... .......... 88% 8.99M 4s
230750K .......... .......... .......... .......... .......... 88% 8.31M 4s
230800K .......... .......... .......... .......... .......... 88% 8.41M 4s
230850K .......... .......... .......... .......... .......... 88% 18.9M 4s
230900K .......... .......... .......... .......... .......... 88% 14.0M 4s
230950K .......... .......... .......... .......... .......... 88% 28.5M 4s
231000K .......... .......... .......... .......... .......... 88% 20.5M 4s
231050K .......... .......... .......... .......... .......... 88% 19.4M 4s
231100K .......... .......... .......... .......... .......... 88% 12.6M 4s
231150K .......... .......... .......... .......... .......... 88% 14.9M 4s
231200K .......... .......... .......... .......... .......... 88% 15.5M 4s
231250K .......... .......... .......... .......... .......... 88% 15.7M 4s
231300K .......... .......... .......... .......... .......... 88% 18.2M 4s
231350K .......... .......... .......... .......... .......... 88% 15.6M 4s
231400K .......... .......... .......... .......... .......... 88% 13.4M 4s
231450K .......... .......... .......... .......... .......... 88% 11.4M 4s
231500K .......... .......... .......... .......... .......... 88% 22.9M 4s
231550K .......... .......... .......... .......... .......... 88% 13.4M 4s
231600K .......... .......... .......... .......... .......... 88% 56.5M 4s
231650K .......... .......... .......... .......... .......... 88% 12.1M 4s
231700K .......... .......... .......... .......... .......... 88% 6.69M 4s
231750K .......... .......... .......... .......... .......... 88% 90.2M 4s
231800K .......... .......... .......... .......... .......... 88% 34.8M 4s
231850K .......... .......... .......... .......... .......... 88% 16.2M 4s
231900K .......... .......... .......... .......... .......... 88% 11.0M 4s
231950K .......... .......... .......... .......... .......... 88% 12.6M 4s
232000K .......... .......... .......... .......... .......... 88% 15.0M 4s
232050K .......... .......... .......... .......... .......... 88% 11.6M 4s
232100K .......... .......... .......... .......... .......... 88% 9.00M 4s
232150K .......... .......... .......... .......... .......... 88% 11.5M 4s
232200K .......... .......... .......... .......... .......... 88% 7.67M 4s
232250K .......... .......... .......... .......... .......... 88% 9.70M 4s
232300K .......... .......... .......... .......... .......... 88% 5.44M 4s
232350K .......... .......... .......... .......... .......... 88% 3.62M 4s
232400K .......... .......... .......... .......... .......... 88% 3.81M 4s
232450K .......... .......... .......... .......... .......... 88% 3.34M 4s
232500K .......... .......... .......... .......... .......... 88% 8.36M 4s
232550K .......... .......... .......... .......... .......... 88% 15.8M 4s
232600K .......... .......... .......... .......... .......... 88% 9.13M 4s
232650K .......... .......... .......... .......... .......... 88% 13.2M 4s
232700K .......... .......... .......... .......... .......... 88% 8.32M 4s
232750K .......... .......... .......... .......... .......... 88% 12.6M 4s
232800K .......... .......... .......... .......... .......... 88% 9.32M 4s
232850K .......... .......... .......... .......... .......... 88% 6.72M 4s
232900K .......... .......... .......... .......... .......... 88% 11.4M 4s
232950K .......... .......... .......... .......... .......... 88% 6.28M 4s
233000K .......... .......... .......... .......... .......... 88% 10.8M 4s
233050K .......... .......... .......... .......... .......... 88% 10.0M 4s
233100K .......... .......... .......... .......... .......... 88% 5.97M 4s
233150K .......... .......... .......... .......... .......... 88% 19.9M 4s
233200K .......... .......... .......... .......... .......... 88% 10.6M 4s
233250K .......... .......... .......... .......... .......... 88% 12.8M 4s
233300K .......... .......... .......... .......... .......... 89% 67.2M 4s
233350K .......... .......... .......... .......... .......... 89% 16.4M 4s
233400K .......... .......... .......... .......... .......... 89% 11.9M 4s
233450K .......... .......... .......... .......... .......... 89% 29.4M 4s
233500K .......... .......... .......... .......... .......... 89% 16.2M 4s
233550K .......... .......... .......... .......... .......... 89% 25.0M 4s
233600K .......... .......... .......... .......... .......... 89% 12.6M 4s
233650K .......... .......... .......... .......... .......... 89% 15.0M 4s
233700K .......... .......... .......... .......... .......... 89% 15.9M 4s
233750K .......... .......... .......... .......... .......... 89% 11.2M 4s
233800K .......... .......... .......... .......... .......... 89% 6.80M 4s
233850K .......... .......... .......... .......... .......... 89% 7.67M 4s
233900K .......... .......... .......... .......... .......... 89% 9.63M 4s
233950K .......... .......... .......... .......... .......... 89% 9.35M 4s
234000K .......... .......... .......... .......... .......... 89% 10.9M 4s
234050K .......... .......... .......... .......... .......... 89% 8.35M 4s
234100K .......... .......... .......... .......... .......... 89% 5.11M 4s
234150K .......... .......... .......... .......... .......... 89% 5.90M 4s
234200K .......... .......... .......... .......... .......... 89% 6.19M 4s
234250K .......... .......... .......... .......... .......... 89% 13.3M 4s
234300K .......... .......... .......... .......... .......... 89% 11.6M 4s
234350K .......... .......... .......... .......... .......... 89% 11.9M 4s
234400K .......... .......... .......... .......... .......... 89% 15.6M 4s
234450K .......... .......... .......... .......... .......... 89% 9.30M 4s
234500K .......... .......... .......... .......... .......... 89% 13.8M 4s
234550K .......... .......... .......... .......... .......... 89% 13.9M 4s
234600K .......... .......... .......... .......... .......... 89% 14.5M 4s
234650K .......... .......... .......... .......... .......... 89% 15.1M 3s
234700K .......... .......... .......... .......... .......... 89% 13.5M 3s
234750K .......... .......... .......... .......... .......... 89% 11.0M 3s
234800K .......... .......... .......... .......... .......... 89% 9.69M 3s
234850K .......... .......... .......... .......... .......... 89% 5.89M 3s
234900K .......... .......... .......... .......... .......... 89% 8.37M 3s
234950K .......... .......... .......... .......... .......... 89% 9.54M 3s
235000K .......... .......... .......... .......... .......... 89% 11.1M 3s
235050K .......... .......... .......... .......... .......... 89% 11.2M 3s
235100K .......... .......... .......... .......... .......... 89% 8.74M 3s
235150K .......... .......... .......... .......... .......... 89% 18.0M 3s
235200K .......... .......... .......... .......... .......... 89% 12.4M 3s
235250K .......... .......... .......... .......... .......... 89% 12.0M 3s
235300K .......... .......... .......... .......... .......... 89% 11.1M 3s
235350K .......... .......... .......... .......... .......... 89% 6.75M 3s
235400K .......... .......... .......... .......... .......... 89% 15.4M 3s
235450K .......... .......... .......... .......... .......... 89% 14.6M 3s
235500K .......... .......... .......... .......... .......... 89% 12.0M 3s
235550K .......... .......... .......... .......... .......... 89% 20.2M 3s
235600K .......... .......... .......... .......... .......... 89% 20.7M 3s
235650K .......... .......... .......... .......... .......... 89% 21.8M 3s
235700K .......... .......... .......... .......... .......... 89% 20.2M 3s
235750K .......... .......... .......... .......... .......... 89% 19.0M 3s
235800K .......... .......... .......... .......... .......... 89% 21.1M 3s
235850K .......... .......... .......... .......... .......... 89% 18.1M 3s
235900K .......... .......... .......... .......... .......... 89% 25.0M 3s
235950K .......... .......... .......... .......... .......... 90% 17.8M 3s
236000K .......... .......... .......... .......... .......... 90% 21.3M 3s
236050K .......... .......... .......... .......... .......... 90% 10.1M 3s
236100K .......... .......... .......... .......... .......... 90% 7.36M 3s
236150K .......... .......... .......... .......... .......... 90% 10.7M 3s
236200K .......... .......... .......... .......... .......... 90% 8.82M 3s
236250K .......... .......... .......... .......... .......... 90% 7.11M 3s
236300K .......... .......... .......... .......... .......... 90% 7.29M 3s
236350K .......... .......... .......... .......... .......... 90% 6.03M 3s
236400K .......... .......... .......... .......... .......... 90% 7.65M 3s
236450K .......... .......... .......... .......... .......... 90% 7.58M 3s
236500K .......... .......... .......... .......... .......... 90% 6.75M 3s
236550K .......... .......... .......... .......... .......... 90% 13.9M 3s
236600K .......... .......... .......... .......... .......... 90% 5.97M 3s
236650K .......... .......... .......... .......... .......... 90% 14.1M 3s
236700K .......... .......... .......... .......... .......... 90% 7.31M 3s
236750K .......... .......... .......... .......... .......... 90% 9.94M 3s
236800K .......... .......... .......... .......... .......... 90% 9.03M 3s
236850K .......... .......... .......... .......... .......... 90% 7.09M 3s
236900K .......... .......... .......... .......... .......... 90% 10.8M 3s
236950K .......... .......... .......... .......... .......... 90% 7.73M 3s
237000K .......... .......... .......... .......... .......... 90% 14.1M 3s
237050K .......... .......... .......... .......... .......... 90% 10.5M 3s
237100K .......... .......... .......... .......... .......... 90% 7.59M 3s
237150K .......... .......... .......... .......... .......... 90% 11.9M 3s
237200K .......... .......... .......... .......... .......... 90% 10.3M 3s
237250K .......... .......... .......... .......... .......... 90% 10.4M 3s
237300K .......... .......... .......... .......... .......... 90% 9.82M 3s
237350K .......... .......... .......... .......... .......... 90% 5.83M 3s
237400K .......... .......... .......... .......... .......... 90% 4.81M 3s
237450K .......... .......... .......... .......... .......... 90% 3.99M 3s
237500K .......... .......... .......... .......... .......... 90% 5.06M 3s
237550K .......... .......... .......... .......... .......... 90% 5.01M 3s
237600K .......... .......... .......... .......... .......... 90% 7.67M 3s
237650K .......... .......... .......... .......... .......... 90% 6.27M 3s
237700K .......... .......... .......... .......... .......... 90% 5.73M 3s
237750K .......... .......... .......... .......... .......... 90% 7.07M 3s
237800K .......... .......... .......... .......... .......... 90% 7.53M 3s
237850K .......... .......... .......... .......... .......... 90% 7.11M 3s
237900K .......... .......... .......... .......... .......... 90% 8.39M 3s
237950K .......... .......... .......... .......... .......... 90% 9.07M 3s
238000K .......... .......... .......... .......... .......... 90% 14.4M 3s
238050K .......... .......... .......... .......... .......... 90% 16.1M 3s
238100K .......... .......... .......... .......... .......... 90% 13.7M 3s
238150K .......... .......... .......... .......... .......... 90% 16.1M 3s
238200K .......... .......... .......... .......... .......... 90% 15.5M 3s
238250K .......... .......... .......... .......... .......... 90% 12.3M 3s
238300K .......... .......... .......... .......... .......... 90% 14.0M 3s
238350K .......... .......... .......... .......... .......... 90% 11.9M 3s
238400K .......... .......... .......... .......... .......... 90% 13.3M 3s
238450K .......... .......... .......... .......... .......... 90% 7.73M 3s
238500K .......... .......... .......... .......... .......... 90% 7.20M 3s
238550K .......... .......... .......... .......... .......... 91% 9.34M 3s
238600K .......... .......... .......... .......... .......... 91% 7.86M 3s
238650K .......... .......... .......... .......... .......... 91% 11.5M 3s
238700K .......... .......... .......... .......... .......... 91% 8.37M 3s
238750K .......... .......... .......... .......... .......... 91% 11.1M 3s
238800K .......... .......... .......... .......... .......... 91% 10.2M 3s
238850K .......... .......... .......... .......... .......... 91% 6.64M 3s
238900K .......... .......... .......... .......... .......... 91% 9.99M 3s
238950K .......... .......... .......... .......... .......... 91% 5.51M 3s
239000K .......... .......... .......... .......... .......... 91% 8.70M 3s
239050K .......... .......... .......... .......... .......... 91% 6.82M 3s
239100K .......... .......... .......... .......... .......... 91% 5.51M 3s
239150K .......... .......... .......... .......... .......... 91% 18.6M 3s
239200K .......... .......... .......... .......... .......... 91% 15.5M 3s
239250K .......... .......... .......... .......... .......... 91% 16.8M 3s
239300K .......... .......... .......... .......... .......... 91% 20.0M 3s
239350K .......... .......... .......... .......... .......... 91% 11.2M 3s
239400K .......... .......... .......... .......... .......... 91% 15.2M 3s
239450K .......... .......... .......... .......... .......... 91% 16.5M 3s
239500K .......... .......... .......... .......... .......... 91% 24.3M 3s
239550K .......... .......... .......... .......... .......... 91% 19.6M 3s
239600K .......... .......... .......... .......... .......... 91% 11.1M 3s
239650K .......... .......... .......... .......... .......... 91% 14.1M 3s
239700K .......... .......... .......... .......... .......... 91% 10.9M 3s
239750K .......... .......... .......... .......... .......... 91% 14.4M 3s
239800K .......... .......... .......... .......... .......... 91% 15.3M 3s
239850K .......... .......... .......... .......... .......... 91% 12.3M 3s
239900K .......... .......... .......... .......... .......... 91% 14.3M 3s
239950K .......... .......... .......... .......... .......... 91% 15.6M 3s
240000K .......... .......... .......... .......... .......... 91% 37.1M 3s
240050K .......... .......... .......... .......... .......... 91% 31.8M 3s
240100K .......... .......... .......... .......... .......... 91% 29.9M 3s
240150K .......... .......... .......... .......... .......... 91% 18.6M 3s
240200K .......... .......... .......... .......... .......... 91% 39.5M 3s
240250K .......... .......... .......... .......... .......... 91% 36.1M 3s
240300K .......... .......... .......... .......... .......... 91% 32.5M 3s
240350K .......... .......... .......... .......... .......... 91% 19.1M 3s
240400K .......... .......... .......... .......... .......... 91% 61.6M 3s
240450K .......... .......... .......... .......... .......... 91% 20.5M 3s
240500K .......... .......... .......... .......... .......... 91% 17.7M 3s
240550K .......... .......... .......... .......... .......... 91% 23.8M 3s
240600K .......... .......... .......... .......... .......... 91% 14.1M 3s
240650K .......... .......... .......... .......... .......... 91% 8.23M 3s
240700K .......... .......... .......... .......... .......... 91% 6.43M 3s
240750K .......... .......... .......... .......... .......... 91% 11.1M 3s
240800K .......... .......... .......... .......... .......... 91% 7.15M 3s
240850K .......... .......... .......... .......... .......... 91% 4.95M 3s
240900K .......... .......... .......... .......... .......... 91% 7.33M 3s
240950K .......... .......... .......... .......... .......... 91% 6.04M 3s
241000K .......... .......... .......... .......... .......... 91% 7.41M 3s
241050K .......... .......... .......... .......... .......... 91% 5.58M 3s
241100K .......... .......... .......... .......... .......... 91% 8.32M 3s
241150K .......... .......... .......... .......... .......... 91% 10.4M 3s
241200K .......... .......... .......... .......... .......... 92% 9.31M 3s
241250K .......... .......... .......... .......... .......... 92% 9.98M 3s
241300K .......... .......... .......... .......... .......... 92% 9.96M 3s
241350K .......... .......... .......... .......... .......... 92% 7.45M 3s
241400K .......... .......... .......... .......... .......... 92% 8.98M 3s
241450K .......... .......... .......... .......... .......... 92% 7.64M 3s
241500K .......... .......... .......... .......... .......... 92% 8.74M 3s
241550K .......... .......... .......... .......... .......... 92% 20.8M 3s
241600K .......... .......... .......... .......... .......... 92% 30.5M 3s
241650K .......... .......... .......... .......... .......... 92% 17.5M 3s
241700K .......... .......... .......... .......... .......... 92% 38.5M 3s
241750K .......... .......... .......... .......... .......... 92% 38.2M 3s
241800K .......... .......... .......... .......... .......... 92% 24.5M 3s
241850K .......... .......... .......... .......... .......... 92% 55.1M 3s
241900K .......... .......... .......... .......... .......... 92% 48.0M 3s
241950K .......... .......... .......... .......... .......... 92% 14.6M 3s
242000K .......... .......... .......... .......... .......... 92% 32.7M 3s
242050K .......... .......... .......... .......... .......... 92% 13.1M 3s
242100K .......... .......... .......... .......... .......... 92% 27.8M 3s
242150K .......... .......... .......... .......... .......... 92% 14.9M 3s
242200K .......... .......... .......... .......... .......... 92% 10.5M 3s
242250K .......... .......... .......... .......... .......... 92% 10.9M 3s
242300K .......... .......... .......... .......... .......... 92% 9.65M 2s
242350K .......... .......... .......... .......... .......... 92% 19.2M 2s
242400K .......... .......... .......... .......... .......... 92% 15.6M 2s
242450K .......... .......... .......... .......... .......... 92% 10.4M 2s
242500K .......... .......... .......... .......... .......... 92% 9.01M 2s
242550K .......... .......... .......... .......... .......... 92% 8.51M 2s
242600K .......... .......... .......... .......... .......... 92% 6.19M 2s
242650K .......... .......... .......... .......... .......... 92% 4.70M 2s
242700K .......... .......... .......... .......... .......... 92% 5.54M 2s
242750K .......... .......... .......... .......... .......... 92% 6.66M 2s
242800K .......... .......... .......... .......... .......... 92% 7.30M 2s
242850K .......... .......... .......... .......... .......... 92% 12.6M 2s
242900K .......... .......... .......... .......... .......... 92% 22.4M 2s
242950K .......... .......... .......... .......... .......... 92% 13.3M 2s
243000K .......... .......... .......... .......... .......... 92% 16.1M 2s
243050K .......... .......... .......... .......... .......... 92% 18.5M 2s
243100K .......... .......... .......... .......... .......... 92% 18.6M 2s
243150K .......... .......... .......... .......... .......... 92% 23.8M 2s
243200K .......... .......... .......... .......... .......... 92% 12.8M 2s
243250K .......... .......... .......... .......... .......... 92% 13.7M 2s
243300K .......... .......... .......... .......... .......... 92% 13.4M 2s
243350K .......... .......... .......... .......... .......... 92% 10.6M 2s
243400K .......... .......... .......... .......... .......... 92% 7.50M 2s
243450K .......... .......... .......... .......... .......... 92% 12.1M 2s
243500K .......... .......... .......... .......... .......... 92% 9.64M 2s
243550K .......... .......... .......... .......... .......... 92% 10.4M 2s
243600K .......... .......... .......... .......... .......... 92% 13.1M 2s
243650K .......... .......... .......... .......... .......... 92% 23.4M 2s
243700K .......... .......... .......... .......... .......... 92% 12.7M 2s
243750K .......... .......... .......... .......... .......... 92% 13.9M 2s
243800K .......... .......... .......... .......... .......... 93% 13.3M 2s
243850K .......... .......... .......... .......... .......... 93% 18.8M 2s
243900K .......... .......... .......... .......... .......... 93% 24.7M 2s
243950K .......... .......... .......... .......... .......... 93% 23.4M 2s
244000K .......... .......... .......... .......... .......... 93% 20.0M 2s
244050K .......... .......... .......... .......... .......... 93% 22.2M 2s
244100K .......... .......... .......... .......... .......... 93% 12.8M 2s
244150K .......... .......... .......... .......... .......... 93% 10.9M 2s
244200K .......... .......... .......... .......... .......... 93% 11.9M 2s
244250K .......... .......... .......... .......... .......... 93% 12.6M 2s
244300K .......... .......... .......... .......... .......... 93% 8.84M 2s
244350K .......... .......... .......... .......... .......... 93% 8.79M 2s
244400K .......... .......... .......... .......... .......... 93% 7.57M 2s
244450K .......... .......... .......... .......... .......... 93% 9.70M 2s
244500K .......... .......... .......... .......... .......... 93% 6.48M 2s
244550K .......... .......... .......... .......... .......... 93% 7.51M 2s
244600K .......... .......... .......... .......... .......... 93% 7.40M 2s
244650K .......... .......... .......... .......... .......... 93% 15.6M 2s
244700K .......... .......... .......... .......... .......... 93% 19.4M 2s
244750K .......... .......... .......... .......... .......... 93% 19.8M 2s
244800K .......... .......... .......... .......... .......... 93% 15.2M 2s
244850K .......... .......... .......... .......... .......... 93% 11.3M 2s
244900K .......... .......... .......... .......... .......... 93% 9.99M 2s
244950K .......... .......... .......... .......... .......... 93% 11.3M 2s
245000K .......... .......... .......... .......... .......... 93% 12.7M 2s
245050K .......... .......... .......... .......... .......... 93% 12.9M 2s
245100K .......... .......... .......... .......... .......... 93% 9.92M 2s
245150K .......... .......... .......... .......... .......... 93% 7.49M 2s
245200K .......... .......... .......... .......... .......... 93% 9.78M 2s
245250K .......... .......... .......... .......... .......... 93% 14.0M 2s
245300K .......... .......... .......... .......... .......... 93% 14.3M 2s
245350K .......... .......... .......... .......... .......... 93% 10.9M 2s
245400K .......... .......... .......... .......... .......... 93% 8.13M 2s
245450K .......... .......... .......... .......... .......... 93% 7.93M 2s
245500K .......... .......... .......... .......... .......... 93% 9.28M 2s
245550K .......... .......... .......... .......... .......... 93% 9.51M 2s
245600K .......... .......... .......... .......... .......... 93% 11.2M 2s
245650K .......... .......... .......... .......... .......... 93% 12.5M 2s
245700K .......... .......... .......... .......... .......... 93% 9.51M 2s
245750K .......... .......... .......... .......... .......... 93% 9.84M 2s
245800K .......... .......... .......... .......... .......... 93% 12.6M 2s
245850K .......... .......... .......... .......... .......... 93% 11.0M 2s
245900K .......... .......... .......... .......... .......... 93% 11.9M 2s
245950K .......... .......... .......... .......... .......... 93% 9.33M 2s
246000K .......... .......... .......... .......... .......... 93% 12.7M 2s
246050K .......... .......... .......... .......... .......... 93% 18.0M 2s
246100K .......... .......... .......... .......... .......... 93% 17.5M 2s
246150K .......... .......... .......... .......... .......... 93% 12.3M 2s
246200K .......... .......... .......... .......... .......... 93% 16.3M 2s
246250K .......... .......... .......... .......... .......... 93% 19.0M 2s
246300K .......... .......... .......... .......... .......... 93% 23.2M 2s
246350K .......... .......... .......... .......... .......... 93% 18.4M 2s
246400K .......... .......... .......... .......... .......... 93% 20.0M 2s
246450K .......... .......... .......... .......... .......... 94% 14.5M 2s
246500K .......... .......... .......... .......... .......... 94% 13.1M 2s
246550K .......... .......... .......... .......... .......... 94% 18.3M 2s
246600K .......... .......... .......... .......... .......... 94% 19.6M 2s
246650K .......... .......... .......... .......... .......... 94% 21.3M 2s
246700K .......... .......... .......... .......... .......... 94% 20.2M 2s
246750K .......... .......... .......... .......... .......... 94% 19.2M 2s
246800K .......... .......... .......... .......... .......... 94% 20.6M 2s
246850K .......... .......... .......... .......... .......... 94% 20.9M 2s
246900K .......... .......... .......... .......... .......... 94% 21.5M 2s
246950K .......... .......... .......... .......... .......... 94% 13.6M 2s
247000K .......... .......... .......... .......... .......... 94% 14.7M 2s
247050K .......... .......... .......... .......... .......... 94% 16.4M 2s
247100K .......... .......... .......... .......... .......... 94% 10.8M 2s
247150K .......... .......... .......... .......... .......... 94% 9.08M 2s
247200K .......... .......... .......... .......... .......... 94% 8.21M 2s
247250K .......... .......... .......... .......... .......... 94% 7.91M 2s
247300K .......... .......... .......... .......... .......... 94% 7.99M 2s
247350K .......... .......... .......... .......... .......... 94% 19.7M 2s
247400K .......... .......... .......... .......... .......... 94% 13.1M 2s
247450K .......... .......... .......... .......... .......... 94% 29.4M 2s
247500K .......... .......... .......... .......... .......... 94% 19.9M 2s
247550K .......... .......... .......... .......... .......... 94% 23.5M 2s
247600K .......... .......... .......... .......... .......... 94% 13.5M 2s
247650K .......... .......... .......... .......... .......... 94% 14.6M 2s
247700K .......... .......... .......... .......... .......... 94% 11.9M 2s
247750K .......... .......... .......... .......... .......... 94% 37.0M 2s
247800K .......... .......... .......... .......... .......... 94% 20.5M 2s
247850K .......... .......... .......... .......... .......... 94% 15.9M 2s
247900K .......... .......... .......... .......... .......... 94% 21.5M 2s
247950K .......... .......... .......... .......... .......... 94% 16.7M 2s
248000K .......... .......... .......... .......... .......... 94% 18.3M 2s
248050K .......... .......... .......... .......... .......... 94% 21.3M 2s
248100K .......... .......... .......... .......... .......... 94% 18.6M 2s
248150K .......... .......... .......... .......... .......... 94% 15.9M 2s
248200K .......... .......... .......... .......... .......... 94% 12.2M 2s
248250K .......... .......... .......... .......... .......... 94% 10.2M 2s
248300K .......... .......... .......... .......... .......... 94% 10.3M 2s
248350K .......... .......... .......... .......... .......... 94% 8.72M 2s
248400K .......... .......... .......... .......... .......... 94% 11.3M 2s
248450K .......... .......... .......... .......... .......... 94% 11.5M 2s
248500K .......... .......... .......... .......... .......... 94% 12.4M 2s
248550K .......... .......... .......... .......... .......... 94% 14.1M 2s
248600K .......... .......... .......... .......... .......... 94% 11.0M 2s
248650K .......... .......... .......... .......... .......... 94% 11.7M 2s
248700K .......... .......... .......... .......... .......... 94% 9.94M 2s
248750K .......... .......... .......... .......... .......... 94% 9.52M 2s
248800K .......... .......... .......... .......... .......... 94% 14.0M 2s
248850K .......... .......... .......... .......... .......... 94% 15.6M 2s
248900K .......... .......... .......... .......... .......... 94% 14.0M 2s
248950K .......... .......... .......... .......... .......... 94% 18.0M 2s
249000K .......... .......... .......... .......... .......... 94% 13.6M 2s
249050K .......... .......... .......... .......... .......... 95% 11.8M 2s
249100K .......... .......... .......... .......... .......... 95% 9.27M 2s
249150K .......... .......... .......... .......... .......... 95%  908K 2s
249200K .......... .......... .......... .......... .......... 95% 12.6M 2s
249250K .......... .......... .......... .......... .......... 95% 14.0M 2s
249300K .......... .......... .......... .......... .......... 95% 13.4M 2s
249350K .......... .......... .......... .......... .......... 95% 10.5M 2s
249400K .......... .......... .......... .......... .......... 95% 14.3M 2s
249450K .......... .......... .......... .......... .......... 95% 8.45M 2s
249500K .......... .......... .......... .......... .......... 95% 14.8M 2s
249550K .......... .......... .......... .......... .......... 95% 15.9M 2s
249600K .......... .......... .......... .......... .......... 95% 13.4M 2s
249650K .......... .......... .......... .......... .......... 95% 10.8M 2s
249700K .......... .......... .......... .......... .......... 95% 5.75M 2s
249750K .......... .......... .......... .......... .......... 95% 5.96M 2s
249800K .......... .......... .......... .......... .......... 95% 7.41M 2s
249850K .......... .......... .......... .......... .......... 95% 6.78M 2s
249900K .......... .......... .......... .......... .......... 95% 10.2M 2s
249950K .......... .......... .......... .......... .......... 95% 26.1M 2s
250000K .......... .......... .......... .......... .......... 95% 16.8M 2s
250050K .......... .......... .......... .......... .......... 95% 69.9M 2s
250100K .......... .......... .......... .......... .......... 95% 44.8M 2s
250150K .......... .......... .......... .......... .......... 95% 35.6M 1s
250200K .......... .......... .......... .......... .......... 95% 33.5M 1s
250250K .......... .......... .......... .......... .......... 95% 25.7M 1s
250300K .......... .......... .......... .......... .......... 95% 47.2M 1s
250350K .......... .......... .......... .......... .......... 95% 31.5M 1s
250400K .......... .......... .......... .......... .......... 95% 42.0M 1s
250450K .......... .......... .......... .......... .......... 95% 17.3M 1s
250500K .......... .......... .......... .......... .......... 95% 21.8M 1s
250550K .......... .......... .......... .......... .......... 95% 29.2M 1s
250600K .......... .......... .......... .......... .......... 95% 33.3M 1s
250650K .......... .......... .......... .......... .......... 95% 27.5M 1s
250700K .......... .......... .......... .......... .......... 95% 30.2M 1s
250750K .......... .......... .......... .......... .......... 95% 16.7M 1s
250800K .......... .......... .......... .......... .......... 95% 19.8M 1s
250850K .......... .......... .......... .......... .......... 95% 11.0M 1s
250900K .......... .......... .......... .......... .......... 95% 12.5M 1s
250950K .......... .......... .......... .......... .......... 95% 7.10M 1s
251000K .......... .......... .......... .......... .......... 95% 6.13M 1s
251050K .......... .......... .......... .......... .......... 95% 6.06M 1s
251100K .......... .......... .......... .......... .......... 95% 6.00M 1s
251150K .......... .......... .......... .......... .......... 95% 7.25M 1s
251200K .......... .......... .......... .......... .......... 95% 6.71M 1s
251250K .......... .......... .......... .......... .......... 95% 14.3M 1s
251300K .......... .......... .......... .......... .......... 95% 11.0M 1s
251350K .......... .......... .......... .......... .......... 95% 6.79M 1s
251400K .......... .......... .......... .......... .......... 95% 11.4M 1s
251450K .......... .......... .......... .......... .......... 95% 9.43M 1s
251500K .......... .......... .......... .......... .......... 95% 10.4M 1s
251550K .......... .......... .......... .......... .......... 95% 8.24M 1s
251600K .......... .......... .......... .......... .......... 95% 8.72M 1s
251650K .......... .......... .......... .......... .......... 95% 8.29M 1s
251700K .......... .......... .......... .......... .......... 96% 8.85M 1s
251750K .......... .......... .......... .......... .......... 96% 7.04M 1s
251800K .......... .......... .......... .......... .......... 96% 6.93M 1s
251850K .......... .......... .......... .......... .......... 96% 3.69M 1s
251900K .......... .......... .......... .......... .......... 96% 7.06M 1s
251950K .......... .......... .......... .......... .......... 96% 4.55M 1s
252000K .......... .......... .......... .......... .......... 96% 5.51M 1s
252050K .......... .......... .......... .......... .......... 96% 6.50M 1s
252100K .......... .......... .......... .......... .......... 96% 8.72M 1s
252150K .......... .......... .......... .......... .......... 96% 6.97M 1s
252200K .......... .......... .......... .......... .......... 96% 6.84M 1s
252250K .......... .......... .......... .......... .......... 96% 9.88M 1s
252300K .......... .......... .......... .......... .......... 96% 12.5M 1s
252350K .......... .......... .......... .......... .......... 96% 8.37M 1s
252400K .......... .......... .......... .......... .......... 96% 10.3M 1s
252450K .......... .......... .......... .......... .......... 96% 7.44M 1s
252500K .......... .......... .......... .......... .......... 96% 5.70M 1s
252550K .......... .......... .......... .......... .......... 96% 9.85M 1s
252600K .......... .......... .......... .......... .......... 96% 7.23M 1s
252650K .......... .......... .......... .......... .......... 96% 9.43M 1s
252700K .......... .......... .......... .......... .......... 96% 7.73M 1s
252750K .......... .......... .......... .......... .......... 96% 9.53M 1s
252800K .......... .......... .......... .......... .......... 96% 9.16M 1s
252850K .......... .......... .......... .......... .......... 96% 10.5M 1s
252900K .......... .......... .......... .......... .......... 96% 21.4M 1s
252950K .......... .......... .......... .......... .......... 96% 16.2M 1s
253000K .......... .......... .......... .......... .......... 96% 18.5M 1s
253050K .......... .......... .......... .......... .......... 96% 16.0M 1s
253100K .......... .......... .......... .......... .......... 96% 13.0M 1s
253150K .......... .......... .......... .......... .......... 96% 13.3M 1s
253200K .......... .......... .......... .......... .......... 96% 12.5M 1s
253250K .......... .......... .......... .......... .......... 96% 15.2M 1s
253300K .......... .......... .......... .......... .......... 96% 13.3M 1s
253350K .......... .......... .......... .......... .......... 96% 6.29M 1s
253400K .......... .......... .......... .......... .......... 96% 7.96M 1s
253450K .......... .......... .......... .......... .......... 96% 5.27M 1s
253500K .......... .......... .......... .......... .......... 96% 6.54M 1s
253550K .......... .......... .......... .......... .......... 96% 5.81M 1s
253600K .......... .......... .......... .......... .......... 96% 12.7M 1s
253650K .......... .......... .......... .......... .......... 96% 21.3M 1s
253700K .......... .......... .......... .......... .......... 96% 13.1M 1s
253750K .......... .......... .......... .......... .......... 96% 14.5M 1s
253800K .......... .......... .......... .......... .......... 96% 17.5M 1s
253850K .......... .......... .......... .......... .......... 96% 8.59M 1s
253900K .......... .......... .......... .......... .......... 96% 32.0M 1s
253950K .......... .......... .......... .......... .......... 96% 14.3M 1s
254000K .......... .......... .......... .......... .......... 96% 12.8M 1s
254050K .......... .......... .......... .......... .......... 96% 11.8M 1s
254100K .......... .......... .......... .......... .......... 96% 8.69M 1s
254150K .......... .......... .......... .......... .......... 96% 12.3M 1s
254200K .......... .......... .......... .......... .......... 96% 10.0M 1s
254250K .......... .......... .......... .......... .......... 96% 13.2M 1s
254300K .......... .......... .......... .......... .......... 97% 13.3M 1s
254350K .......... .......... .......... .......... .......... 97% 17.7M 1s
254400K .......... .......... .......... .......... .......... 97% 14.8M 1s
254450K .......... .......... .......... .......... .......... 97% 32.2M 1s
254500K .......... .......... .......... .......... .......... 97% 12.4M 1s
254550K .......... .......... .......... .......... .......... 97% 19.4M 1s
254600K .......... .......... .......... .......... .......... 97% 12.6M 1s
254650K .......... .......... .......... .......... .......... 97% 11.1M 1s
254700K .......... .......... .......... .......... .......... 97% 12.5M 1s
254750K .......... .......... .......... .......... .......... 97% 17.0M 1s
254800K .......... .......... .......... .......... .......... 97% 9.87M 1s
254850K .......... .......... .......... .......... .......... 97% 15.4M 1s
254900K .......... .......... .......... .......... .......... 97% 13.5M 1s
254950K .......... .......... .......... .......... .......... 97% 13.2M 1s
255000K .......... .......... .......... .......... .......... 97% 14.7M 1s
255050K .......... .......... .......... .......... .......... 97% 17.6M 1s
255100K .......... .......... .......... .......... .......... 97% 15.6M 1s
255150K .......... .......... .......... .......... .......... 97% 18.5M 1s
255200K .......... .......... .......... .......... .......... 97% 17.6M 1s
255250K .......... .......... .......... .......... .......... 97% 18.3M 1s
255300K .......... .......... .......... .......... .......... 97% 17.8M 1s
255350K .......... .......... .......... .......... .......... 97% 24.5M 1s
255400K .......... .......... .......... .......... .......... 97% 16.6M 1s
255450K .......... .......... .......... .......... .......... 97% 14.3M 1s
255500K .......... .......... .......... .......... .......... 97% 22.7M 1s
255550K .......... .......... .......... .......... .......... 97% 20.2M 1s
255600K .......... .......... .......... .......... .......... 97% 17.9M 1s
255650K .......... .......... .......... .......... .......... 97% 24.2M 1s
255700K .......... .......... .......... .......... .......... 97% 15.7M 1s
255750K .......... .......... .......... .......... .......... 97% 18.4M 1s
255800K .......... .......... .......... .......... .......... 97% 19.4M 1s
255850K .......... .......... .......... .......... .......... 97% 9.74M 1s
255900K .......... .......... .......... .......... .......... 97% 17.7M 1s
255950K .......... .......... .......... .......... .......... 97% 17.7M 1s
256000K .......... .......... .......... .......... .......... 97% 48.7M 1s
256050K .......... .......... .......... .......... .......... 97% 29.8M 1s
256100K .......... .......... .......... .......... .......... 97% 24.1M 1s
256150K .......... .......... .......... .......... .......... 97% 46.0M 1s
256200K .......... .......... .......... .......... .......... 97% 60.3M 1s
256250K .......... .......... .......... .......... .......... 97% 59.5M 1s
256300K .......... .......... .......... .......... .......... 97% 34.8M 1s
256350K .......... .......... .......... .......... .......... 97% 8.91M 1s
256400K .......... .......... .......... .......... .......... 97% 9.64M 1s
256450K .......... .......... .......... .......... .......... 97% 10.8M 1s
256500K .......... .......... .......... .......... .......... 97% 10.6M 1s
256550K .......... .......... .......... .......... .......... 97% 13.3M 1s
256600K .......... .......... .......... .......... .......... 97% 7.26M 1s
256650K .......... .......... .......... .......... .......... 97% 18.1M 1s
256700K .......... .......... .......... .......... .......... 97% 11.3M 1s
256750K .......... .......... .......... .......... .......... 97% 11.5M 1s
256800K .......... .......... .......... .......... .......... 97% 12.7M 1s
256850K .......... .......... .......... .......... .......... 97% 10.8M 1s
256900K .......... .......... .......... .......... .......... 98% 11.1M 1s
256950K .......... .......... .......... .......... .......... 98% 13.6M 1s
257000K .......... .......... .......... .......... .......... 98% 19.5M 1s
257050K .......... .......... .......... .......... .......... 98% 13.3M 1s
257100K .......... .......... .......... .......... .......... 98% 20.6M 1s
257150K .......... .......... .......... .......... .......... 98% 25.5M 1s
257200K .......... .......... .......... .......... .......... 98% 15.2M 1s
257250K .......... .......... .......... .......... .......... 98% 30.3M 1s
257300K .......... .......... .......... .......... .......... 98% 12.6M 1s
257350K .......... .......... .......... .......... .......... 98% 12.2M 1s
257400K .......... .......... .......... .......... .......... 98% 15.2M 1s
257450K .......... .......... .......... .......... .......... 98% 15.5M 1s
257500K .......... .......... .......... .......... .......... 98% 16.7M 1s
257550K .......... .......... .......... .......... .......... 98% 15.2M 1s
257600K .......... .......... .......... .......... .......... 98% 12.5M 1s
257650K .......... .......... .......... .......... .......... 98% 15.9M 1s
257700K .......... .......... .......... .......... .......... 98% 15.6M 1s
257750K .......... .......... .......... .......... .......... 98% 17.7M 1s
257800K .......... .......... .......... .......... .......... 98% 26.0M 1s
257850K .......... .......... .......... .......... .......... 98% 19.3M 1s
257900K .......... .......... .......... .......... .......... 98% 25.0M 1s
257950K .......... .......... .......... .......... .......... 98% 12.5M 1s
258000K .......... .......... .......... .......... .......... 98% 12.3M 1s
258050K .......... .......... .......... .......... .......... 98% 13.3M 1s
258100K .......... .......... .......... .......... .......... 98% 8.97M 0s
258150K .......... .......... .......... .......... .......... 98% 13.8M 0s
258200K .......... .......... .......... .......... .......... 98% 9.46M 0s
258250K .......... .......... .......... .......... .......... 98% 17.3M 0s
258300K .......... .......... .......... .......... .......... 98% 35.1M 0s
258350K .......... .......... .......... .......... .......... 98% 10.8M 0s
258400K .......... .......... .......... .......... .......... 98% 89.7M 0s
258450K .......... .......... .......... .......... .......... 98% 22.4M 0s
258500K .......... .......... .......... .......... .......... 98% 15.8M 0s
258550K .......... .......... .......... .......... .......... 98% 12.5M 0s
258600K .......... .......... .......... .......... .......... 98% 11.2M 0s
258650K .......... .......... .......... .......... .......... 98% 14.0M 0s
258700K .......... .......... .......... .......... .......... 98% 12.0M 0s
258750K .......... .......... .......... .......... .......... 98% 13.0M 0s
258800K .......... .......... .......... .......... .......... 98% 15.4M 0s
258850K .......... .......... .......... .......... .......... 98% 12.3M 0s
258900K .......... .......... .......... .......... .......... 98% 18.2M 0s
258950K .......... .......... .......... .......... .......... 98% 16.4M 0s
259000K .......... .......... .......... .......... .......... 98% 12.5M 0s
259050K .......... .......... .......... .......... .......... 98% 17.7M 0s
259100K .......... .......... .......... .......... .......... 98% 16.4M 0s
259150K .......... .......... .......... .......... .......... 98% 17.5M 0s
259200K .......... .......... .......... .......... .......... 98% 12.7M 0s
259250K .......... .......... .......... .......... .......... 98% 17.0M 0s
259300K .......... .......... .......... .......... .......... 98% 18.7M 0s
259350K .......... .......... .......... .......... .......... 98% 15.3M 0s
259400K .......... .......... .......... .......... .......... 98% 12.8M 0s
259450K .......... .......... .......... .......... .......... 98% 21.0M 0s
259500K .......... .......... .......... .......... .......... 98% 14.8M 0s
259550K .......... .......... .......... .......... .......... 99% 12.4M 0s
259600K .......... .......... .......... .......... .......... 99% 10.8M 0s
259650K .......... .......... .......... .......... .......... 99% 13.0M 0s
259700K .......... .......... .......... .......... .......... 99% 12.4M 0s
259750K .......... .......... .......... .......... .......... 99% 13.0M 0s
259800K .......... .......... .......... .......... .......... 99% 16.9M 0s
259850K .......... .......... .......... .......... .......... 99% 10.5M 0s
259900K .......... .......... .......... .......... .......... 99% 16.6M 0s
259950K .......... .......... .......... .......... .......... 99% 19.2M 0s
260000K .......... .......... .......... .......... .......... 99% 93.6M 0s
260050K .......... .......... .......... .......... .......... 99% 18.2M 0s
260100K .......... .......... .......... .......... .......... 99% 32.7M 0s
260150K .......... .......... .......... .......... .......... 99%  237M 0s
260200K .......... .......... .......... .......... .......... 99% 47.1M 0s
260250K .......... .......... .......... .......... .......... 99% 65.4M 0s
260300K .......... .......... .......... .......... .......... 99% 32.6M 0s
260350K .......... .......... .......... .......... .......... 99% 14.8M 0s
260400K .......... .......... .......... .......... .......... 99% 20.8M 0s
260450K .......... .......... .......... .......... .......... 99% 12.9M 0s
260500K .......... .......... .......... .......... .......... 99% 14.7M 0s
260550K .......... .......... .......... .......... .......... 99% 11.0M 0s
260600K .......... .......... .......... .......... .......... 99% 9.93M 0s
260650K .......... .......... .......... .......... .......... 99% 10.4M 0s
260700K .......... .......... .......... .......... .......... 99% 12.7M 0s
260750K .......... .......... .......... .......... .......... 99% 10.6M 0s
260800K .......... .......... .......... .......... .......... 99% 14.5M 0s
260850K .......... .......... .......... .......... .......... 99% 13.7M 0s
260900K .......... .......... .......... .......... .......... 99% 16.5M 0s
260950K .......... .......... .......... .......... .......... 99% 12.9M 0s
261000K .......... .......... .......... .......... .......... 99% 26.7M 0s
261050K .......... .......... .......... .......... .......... 99% 16.9M 0s
261100K .......... .......... .......... .......... .......... 99% 16.0M 0s
261150K .......... .......... .......... .......... .......... 99% 17.2M 0s
261200K .......... .......... .......... .......... .......... 99% 11.3M 0s
261250K .......... .......... .......... .......... .......... 99% 12.4M 0s
261300K .......... .......... .......... .......... .......... 99% 10.6M 0s
261350K .......... .......... .......... .......... .......... 99% 8.26M 0s
261400K .......... .......... .......... .......... .......... 99% 24.1M 0s
261450K .......... .......... .......... .......... .......... 99% 10.8M 0s
261500K .......... .......... .......... .......... .......... 99% 13.1M 0s
261550K .......... .......... .......... .......... .......... 99% 13.4M 0s
261600K .......... .......... .......... .......... .......... 99% 13.2M 0s
261650K .......... .......... .......... .......... .......... 99% 14.3M 0s
261700K .......... .......... .......... .......... .......... 99% 16.5M 0s
261750K .......... .......... .......... .......... .......... 99% 18.9M 0s
261800K .......... .......... .......... .......... .......... 99% 14.7M 0s
261850K .......... .......... .......... .......... .......... 99% 11.3M 0s
261900K .......... .......... .......... .......... .......... 99% 24.0M 0s
261950K .......... .......... .......... .......... .......... 99% 13.6M 0s
262000K .......... .......... .......... .......... .......... 99% 14.3M 0s
262050K .......... .......... .......... .......... .......... 99% 15.6M 0s
262100K .......... .......... .......... .......... .......... 99% 13.4M 0s
262150K .......... .......... .......... ..........           100% 10.3M=32s

2024-04-28 10:17:34 (7.97 MB/s) - ‘ESPbeta.tgz’ saved [268483520/268483520]

+ tar -xf ESPbeta.tgz
+ rm -rf EngSketchPad/data/Slugs
+ python --version
Python 3.11.9
+ [[ '' == *\.\i\f\o\r\t ]]
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/config/
+ ./makeEnv

ESP runtime AutoConfigurator

CASROOT = /home/jenkins/util/ESP/OpenCASCADE-7.8.0  with contents:
bin
include
lib
share


Info: Python exec /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python found!
Info: Python header /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11/Python.h found!
Info: Python library /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/libpython3.11.so found!

ESP_ARCH = LINUX64
ESP_ROOT = /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad
EFCOMP   = gfortran

CARCH    = LINUX64
CASROOT  = /home/jenkins/util/ESP/OpenCASCADE-7.8.0
CASARCH  = .
CASREV   = 7.8

PYTHONINC= /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
PYTHONLIB= -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11

+ source /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=LINUX64
++ ESP_ARCH=LINUX64
++ export ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad
++ ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASARCH=.
++ CASARCH=.
++ export CASREV=7.8
++ CASREV=7.8
++ export PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONINC=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
++ PYTHONINC=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
++ export 'PYTHONLIB=-L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11'
++ PYTHONLIB='-L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11'
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ export AFLR_ARCH=Linux-x86-64
++ AFLR_ARCH=Linux-x86-64
++ '[' -z /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib: ']'
++ export LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ export CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ export TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ export 'SLUGS_START=firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/SLUGS/Slugs.html &'
++ SLUGS_START='firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/SLUGS/Slugs.html &'
++ export 'ESP_START=firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/ESP/ESP.html &'
++ ESP_START='firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/ESP/ESP.html &'
++ export 'WV_START=firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/wvClient/wv.html &'
++ WV_START='firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/wvClient/wv.html &'
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src
+ make
(cd EGADS/src; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/src'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/LINUX64
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/LINUX64
cp -p ../include/LINUX64 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/LINUX64
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/STANALYZER.make
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/STANALYZER.make
cp -p ../include/STANALYZER.make /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/STANALYZER.make
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.h
cp -p ../include/egads.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads_dot.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads_dot.h
cp -p ../include/egads_dot.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads_dot.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.inc
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.inc
cp -p ../include/egads.inc /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.inc
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsErrors.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsErrors.h
cp -p ../include/egadsErrors.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsErrors.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTypes.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTypes.h
cp -p ../include/egadsTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTypes.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/emp.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/emp.h
cp -p ../include/emp.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/emp.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/prm.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/prm.h
cp -p ../include/prm.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/prm.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.h
cp -p ../include/wsserver.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.inc
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.inc
cp -p ../include/wsserver.inc /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.inc
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsss.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsss.h
cp -p ../include/wsss.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsss.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTris.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTris.h
cp -p egadsTris.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTris.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineFit.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineFit.h
cp -p egadsSplineFit.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineFit.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineVels.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineVels.h
cp -p egadsSplineVels.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineVels.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsf90.inc
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsf90.inc
cp -p ../include/egadsf90.inc /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsf90.inc
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealD.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Lazy.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealD_Lazy.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Trad.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealD_Trad.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealS.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Lazy.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealS_Lazy.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Trad.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealS_Trad.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/always_inline.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/always_inline.h
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsGeom.cpp -o ./egadsGeom.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsHLevel.cpp -o ./egadsHLevel.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsTopo.cpp -o ./egadsTopo.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsCopy.cpp -o ./egadsCopy.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsSpline.cpp -o ./egadsSpline.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsIO.cpp -o ./egadsIO.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsSplineFit.cpp -o ./egadsSplineFit.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsSkinning.cpp -o ./egadsSkinning.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsTessSens.cpp -o ./egadsTessSens.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 OCC/BRepLib_FuseEdges.cpp -o ./BRepLib_FuseEdges.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsBase.c -o ./egadsBase.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsMemory.c -o ./egadsMemory.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsAttrs.c -o ./egadsAttrs.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsTess.c -o ./egadsTess.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsTessInp.c -o ./egadsTessInp.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsTris.c -o ./egadsTris.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsQuads.c -o ./egadsQuads.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsFit.c -o ./egadsFit.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsRobust.c -o ./egadsRobust.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsSBO.c -o ./egadsSBO.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap prmCfit.c -o ./prmCfit.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap prmGrid.c -o ./prmGrid.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap prmUV.c -o ./prmUV.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsExport.c -o ./egadsExport.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsEffect.c -o ./egadsEffect.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsSolids.c -o ./egadsSolids.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include ../util/emp.c \
	-o ./emp.o
g++ -g  -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \
	../util/evaluate.c -o ./evaluate.o
g++ -g  -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \
	../util/rational.c -o ./rational.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include -I../util \
	../util/regQuads.c -o ./regQuads.o
g++ -g  -o ./SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp
./SurrealD1

SurrealD1_test_suite Complete!

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

SurrealD4_test_suite Complete!

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

SurrealS1_test_suite Complete!

g++ -g  -o ./SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp
../util/SurrealS4_btest.cpp: In function ‘void multiply_deriv2()’:
../util/SurrealS4_btest.cpp:1265:23: note: variable tracking size limit exceeded with -fvar-tracking-assignments, retrying without
 BOOST_AUTO_TEST_CASE( multiply_deriv2 )
                       ^
../util/SurrealS4_btest.cpp:19:42: note: in definition of macro ‘BOOST_AUTO_TEST_CASE’
 #define BOOST_AUTO_TEST_CASE( fun ) void fun()
                                          ^
./SurrealS4

SurrealS4_test_suite Complete!

make -C ../util
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/util'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 uvmap/main/uvmap.c -Iuvmap \
	-o ./uvmap.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_bnd_adj.c -o ./uvmap_bnd_adj.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibfibf.c -o ./uvmap_ibfibf.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_message.c -o ./uvmap_message.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibfin.c -o ./uvmap_ibfin.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_read.c -o ./uvmap_read.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_iccin.c -o ./uvmap_iccin.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_add.c -o ./uvmap_add.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_cpu_message.c -o ./uvmap_cpu_message.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapFindUV.c -o ./EG_uvmapFindUV.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapTest.c -o ./EG_uvmapTest.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_inibe.c -o ./uvmap_inibe.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_version.c -o ./uvmap_version.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_inl_uv_bnd.c -o ./uvmap_inl_uv_bnd.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_chk_edge_ratio.c -o ./uvmap_chk_edge_ratio.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_struct_tasks.c -o ./uvmap_struct_tasks.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmap_Read.c -o ./EG_uvmap_Read.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_idibe.c -o ./uvmap_idibe.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapStructFree.c -o ./EG_uvmapStructFree.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapGen.c -o ./EG_uvmapGen.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_write.c -o ./uvmap_write.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibeibe.c -o ./uvmap_ibeibe.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_chk_area_uv.c -o ./uvmap_chk_area_uv.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_norm_uv.c -o ./uvmap_norm_uv.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_iccibe.c -o ./uvmap_iccibe.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_malloc.c -o ./uvmap_malloc.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_gen_uv.c -o ./uvmap_gen_uv.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_to_egads.c -o ./uvmap_to_egads.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmap_Write.c -o ./EG_uvmap_Write.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_test.c -o ./uvmap_test.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_mben_disc.c -o ./uvmap_mben_disc.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_find_uv.c -o ./uvmap_find_uv.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_gen.c -o ./uvmap_gen.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_solve.c -o ./uvmap_solve.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_from_egads.c -o ./uvmap_from_egads.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 egadsUVmap.c -Iuvmap \
	-o ./egadsUVmap.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a ./egadsUVmap.o uvmap_cpu_message.o uvmap_ibfibf.o uvmap_message.o uvmap_version.o uvmap_gen_uv.o uvmap_inl_uv_bnd.o EG_uvmap_Read.o uvmap_chk_edge_ratio.o uvmap_idibe.o uvmap_write.o uvmap_ibeibe.o uvmap_chk_area_uv.o uvmap_gen.o uvmap_malloc.o uvmap_to_egads.o EG_uvmap_Write.o uvmap_iccibe.o EG_uvmapGen.o EG_uvmapTest.o uvmap_read.o uvmap_ibfin.o uvmap_iccin.o uvmap_add.o EG_uvmapFindUV.o uvmap_struct_tasks.o uvmap_bnd_adj.o EG_uvmapStructFree.o uvmap_inibe.o uvmap_norm_uv.o uvmap_test.o uvmap_mben_disc.o uvmap_find_uv.o uvmap_solve.o uvmap_from_egads.o;  )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a
gcc -g  -o ./uvmap.exe ./uvmap.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -luvmap -lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/util'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegads.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegads.so
(cd .; gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegads.so \
	egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o   egadsSplineFit.o egadsSkinning.o egadsTessSens.o  BRepLib_FuseEdges.o  egadsBase.o egadsMemory.o egadsAttrs.o  egadsTess.o   egadsTessInp.o egadsTris.o egadsQuads.o  egadsFit.o    egadsRobust.o egadsSBO.o prmCfit.o   prmGrid.o     prmUV.o       egadsExport.o egadsEffect.o egadsSolids.o emp.o evaluate.o rational.o regQuads.o \
	-L/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -pthread -lm -lstdc++ -lrt )
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a
cp /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a
(cd .; \
	ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a egadsBase.o egadsMemory.o egadsAttrs.o  egadsTess.o   egadsTessInp.o egadsTris.o egadsQuads.o  egadsFit.o    egadsRobust.o egadsSBO.o prmCfit.o   prmGrid.o     prmUV.o       egadsExport.o egadsEffect.o egadsSolids.o egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o   egadsSplineFit.o egadsSkinning.o egadsTessSens.o  BRepLib_FuseEdges.o  emp.o \
	evaluate.o rational.o regQuads.o;  )
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsBase.c -o ./fgadsBase.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsMemory.c -o ./fgadsMemory.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsAttrs.c -o ./fgadsAttrs.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsTess.c -o ./fgadsTess.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsHLevel.c -o ./fgadsHLevel.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsGeom.c -o ./fgadsGeom.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsTopo.c -o ./fgadsTopo.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o  fgadsTess.o   fgadsHLevel.o fgadsGeom.o fgadsTopo.o;  )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a emp.o;  )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a
 *** EGADS Build Complete! ***
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/src'
(cd EGADS/lite; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/lite'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteBase.c -o ./liteBase.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteMemory.c -o ./liteMemory.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteGeom.c -o ./liteGeom.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteTopo.c -o ./liteTopo.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteAttrs.c -o ./liteAttrs.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteImport.c -o ./liteImport.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteString.c -o ./liteString.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                ../src/egadsTess.c -o ./liteTess.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                ../src/egadsTris.c -o ./liteTris.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src \
                ../src/egadsQuads.c -o ./liteQuads.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                -I../util ../src/egadsTessInp.c -o ./liteTessInp.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 ../src/egadsRobust.c \
	-o ./egadsRobust.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLINUX64 -I../include ../util/emp.c \
	-o ./emp.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
	../util/evaluate.c -o ./evaLite.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE ../util/rational.c \
	-o ./ratLite.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I../util \
	../util/regQuads.c -o ./liteRegQuads.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                ../src/egadsEffect.c -o ./liteEffect.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                -I../util/uvmap liteUVmap.c -o ./liteUVmap.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslite.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslite.so
(cd .; gcc -g  -shared -Wl,-no-undefined \
	-o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslite.so liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o liteTess.o liteTris.o \
	liteQuads.o liteTessInp.o egadsRobust.o emp.o evaLite.o \
	ratLite.o liteRegQuads.o liteEffect.o liteUVmap.o \
	-lpthread -lm )
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o \
                liteTess.o liteTris.o liteQuads.o liteTessInp.o egadsRobust.o \
	emp.o evaLite.o ratLite.o liteRegQuads.o liteEffect.o \
	liteUVmap.o ;  )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/lite'
(cd wvServer; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/wvServer'
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 map.cpp -o ./map.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include base64-decode.c -o ./base64-decode.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include handshake.c -o ./handshake.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include client-handshake.c -o ./client-handshake.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include libwebsockets.c -o ./libwebsockets.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include extension-deflate-stream.c -o ./extension-deflate-stream.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include md5.c -o ./md5.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include extension-x-google-mux.c -o ./extension-x-google-mux.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include parsers.c -o ./parsers.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include extension.c -o ./extension.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include sha-1.c -o ./sha-1.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include server.c -o ./server.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include wv.c -o ./wv.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include browserMessage.c -o ./browserMessage.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fwv.c -o ./fwv.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a map.o base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o \
	./fwv.o;  )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -DSTANDALONE server.c \
	-I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -o ./servertest.o
g++ -g  -o ./server ./servertest.o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a  \
	-lpthread -lz -lm
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.so
(cd .; g++ -g  -shared -Wl,-no-undefined \
	-o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.so base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o map.o -lz -lpthread)
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/wvServer'
(cd EGADS/examples; make -f egads2cart.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include egads2cart.c \
	-o ./egads2cart.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads \
	-lrt -lm
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vCurvature.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vCurvature.c -o ./vCurvature.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vCurvature ./vCurvature.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads -lrt
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vGeom.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vGeom.c -o ./vGeom.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vGeom ./vGeom.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads \
	-lrt
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vTess.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vTess.c -o ./vTess.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include ../util/retessFaces.c \
	-o ./retessFaces.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legadstatic -L/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -pthread -lm \
	-lpthread -lz -lrt -lm
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads -lrt
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
(cd OpenCSM; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. serveCSM.c -o ./serveCSM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. OpenCSM.c -o ./OpenCSM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udp.c -o ./udp.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. tim.c -o ./tim.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libocsm.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libocsm.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libocsm.so ./OpenCSM.o ./udp.o ./tim.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads -lwsserver -ldl -lrt -lm
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/serveESP ./serveESP.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o
gcc -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lrt -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bezier.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bezier.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/biconvex.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/biconvex.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/box.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/box.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/box.so ./udpBox.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bspline.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bspline.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/catmull.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/catmull.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/compare.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/compare.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/compare.so ./udfCompare.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createBEM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createBEM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createPoly.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createPoly.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/csm.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/csm.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/csm.so ./udpCsm.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/deform.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/deform.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/deform.so ./udfDeform.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/droop.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/droop.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/droop.so ./udfDroop.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/dumpPmtrs.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/dumpPmtrs.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/editAttr.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/editAttr.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ellipse.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ellipse.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/eqn2body.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/eqn2body.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fitcurve.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fitcurve.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flend.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flend.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flend.so ./udfFlend.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/freeform.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/freeform.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ganged.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ganged.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/guide.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/guide.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/guide.so ./udfGuide.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hex.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hex.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hex.so ./udpHex.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/import.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/import.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/import.so ./udpImport.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/kulfan.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/kulfan.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/linalg.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/linalg.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/matchBodys.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/matchBodys.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mechanism.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mechanism.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca.so ./udpNaca.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca6mc.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca6mc.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nacelle.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nacelle.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nurbbody.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nurbbody.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nuscale.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nuscale.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/offset.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/offset.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/offset.so ./udfOffset.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parabaloid.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parabaloid.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parsec.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parsec.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pod.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pod.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pod.so ./udpPod.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/poly.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/poly.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/poly.so ./udpPoly.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBbox.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBbox.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBrep.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBrep.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printEgo.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printEgo.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/prop.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/prop.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/prop.so ./udpProp.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/radwaf.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/radwaf.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sample.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sample.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sample.so ./udpSample.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sew.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sew.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sew.so ./udpSew.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/shadow.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/shadow.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slices.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slices.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slices.so ./udfSlices.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stag.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stag.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stag.so ./udpStag.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stiffener.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stiffener.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/supell.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/supell.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/supell.so ./udpSupell.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester1.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester1.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester2.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester2.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vsp3.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vsp3.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/waffle.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/waffle.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpWarp.c -o ./udpWarp.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/warp.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/warp.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/warp.so ./udpWarp.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/PDT2.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/PDT2.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpNaca456.c -o ./udpNaca456.o
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer naca456.f90 -o ./naca456.o -J .
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca456.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca456.so
gfortran -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -legads -lm 
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ereped.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ereped.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ereped.so ./timEreped.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mitten.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mitten.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mitten.so ./timMitten.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plotter.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plotter.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plugs.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plugs.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slugs.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slugs.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vspSetup.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vspSetup.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/OpenCSM.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/OpenCSM.h
cp -p OpenCSM.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/OpenCSM.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/common.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/common.h
cp -p common.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/common.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udp.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udp.h
cp -p udp.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udp.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/esp.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/esp.h
cp -p esp.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/esp.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/tim.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/tim.h
cp -p tim.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/tim.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egg.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egg.h
cp -p egg.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egg.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.h
cp -p udpUtilities.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.c
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.c
cp -p udpUtilities.c /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.c
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM'
(cd Slugs; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/Slugs'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. Slugs.c -o ./Slugs.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. Fitter.c \
	-o ./Fitter.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. RedBlackTree.c \
	-o ./RedBlackTree.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. Tessellate.c \
	-o ./Tessellate.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \
	./Tessellate.o -lrt -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads \
	-lpthread -lz -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -lrt -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads \
	-lpthread -lz -lm
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/Slugs'
(cd CAPS; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS'
/bin/cp Cart3D/X86_64_GCC/libc3dio.a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libc3dio.a
/bin/cp Cart3D/X86_64_GCC/libCart3D.a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libCart3D.a
/bin/cp Executables/LINUX64/avl /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/avl
/bin/cp Executables/LINUX64/pplot /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/pplot
/bin/cp Executables/LINUX64/pxplot /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/pxplot
/bin/cp Executables/LINUX64/xfoil /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/xfoil
/bin/cp Executables/LINUX64/mastros.exe /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/mastros.exe
/bin/cp Executables/LINUX64/ASTRO.D01 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/ASTRO.D01
/bin/cp Executables/LINUX64/ASTRO.IDX /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/ASTRO.IDX
/bin/cp Executables/LINUX64/mses /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/mses
/bin/cp Executables/LINUX64/mset /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/mset
/bin/cp Libraries/LINUX64/aflr2AIM.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/aflr2AIM.so
/bin/cp Libraries/LINUX64/aflr3AIM.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/aflr3AIM.so
/bin/cp Libraries/LINUX64/aflr4AIM.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/aflr4AIM.so
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS'
(cd CAPS/src; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/src'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/caps.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/caps.h
cp -p ../include/caps.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/caps.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsErrors.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsErrors.h
cp -p ../include/capsErrors.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsErrors.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsTypes.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsTypes.h
cp -p ../include/capsTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsTypes.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimUtil.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimUtil.h
cp -p ../include/aimUtil.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimUtil.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimMesh.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimMesh.h
cp -p ../include/aimMesh.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimMesh.h
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../include \
	-I/usr/include/udunits2 aimUtil.c -o ./aimUtil.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include \
	-I/usr/include/udunits2 aimTransferUtil.c \
	-o ./aimTransferUtil.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../include \
	aimMesh.c -o ./aimMesh.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a
ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \
	./aimTransferUtil.o 
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsBase.c -o ./capsBase.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsAnalysis.c -o ./capsAnalysis.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsApprox.c -o ./capsApprox.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsAttr.c -o ./capsAttr.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsAIM.c -o ./capsAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsBound.c -o ./capsBound.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsProblem.c -o ./capsProblem.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsValue.c -o ./capsValue.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsUnits.c -o ./capsUnits.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 conjGrad.c -o ./conjGrad.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsFunIDs.c -o ./capsFunIDs.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsChkInpt.c -o ./capsChkInpt.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
	-I/usr/include/udunits2 printObject.c -o ./printObject.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcaps.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcaps.so
(cd .; gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcaps.so \
		capsBase.o   capsAnalysis.o capsApprox.o capsAttr.o  capsAIM.o capsBound.o  capsProblem.o  capsValue.o  capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o  printObject.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -ludunits2 -locsm -legads -ldl \
		-lrt -lm )
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a capsBase.o   capsAnalysis.o capsApprox.o capsAttr.o  capsAIM.o capsBound.o  capsProblem.o  capsValue.o  capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o  printObject.o )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include testingAIM.c \
	-o ./testingAIM.o
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so
rm: cannot remove ‘/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so’: No such file or directory
make[1]: [/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored)
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include testingWriter.c \
	-o ./testingWriter.o
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so
rm: cannot remove ‘/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so’: No such file or directory
make[1]: [/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored)
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -ldl -lrt -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include phaseUtil.c \
	-o ./phaseUtil.o
gcc -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -lrt -lm
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/src'
(cd ../CAPSexamples; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples'
(make -C cCAPS -f aeroelastic_SU2.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o
gcc -g  -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include avlTest.c -o ./avlTest.o
gcc -g  -o ./avlTest ./avlTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include awaveTest.c -o ./awaveTest.o
gcc -g  -o ./awaveTest ./awaveTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include frictionTest.c -o ./frictionTest.o
gcc -g  -o ./frictionTest ./frictionTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o
gcc -g  -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o
gcc -g  -o ./fun3dTetgenTest ./fun3dTetgenTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o
gcc -g  -o ./aeroelasticTest ./aeroelasticTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f hsm.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmTest.c -o ./hsmTest.o   
gcc -g  -o ./hsmTest ./hsmTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o  
gcc -g  -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o  
gcc -g  -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o  
gcc -g  -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include interferenceTest.c \
	-o ./interferenceTest.o   
gcc -g  -o ./interferenceTest ./interferenceTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include msesTest.c -o ./msesTest.o
gcc -g  -o ./msesTest ./msesTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f mystran.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include mystranTest.c -o ./mystranTest.o   
gcc -g  -o ./mystranTest ./mystranTest.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o
gcc -g  -o ./pointwiseTest ./pointwiseTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples'
(cd CAPS/aim; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim'
make -C utils
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/utils'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython attrUtils.c -o ./attrUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython meshUtils.c -o ./meshUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cfdUtils.c -o ./cfdUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython miscUtils.c -o ./miscUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython feaUtils.c -o ./feaUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython vlmUtils.c -o ./vlmUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranUtils.c -o ./nastranUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython tecplotUtils.c -o ./tecplotUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython arrayUtils.c -o ./arrayUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython deprecateUtils.c -o ./deprecateUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cardUtils.c -o ./cardUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranCards.c -o ./nastranCards.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython jsonUtils.c -o ./jsonUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cython/nastranOP2Reader.c -o ./nastranOP2Reader.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a attrUtils.o meshUtils.o cfdUtils.o miscUtils.o feaUtils.o vlmUtils.o nastranUtils.o tecplotUtils.o arrayUtils.o deprecateUtils.o cardUtils.o nastranCards.o jsonUtils.o nastranOP2Reader.o vlmSpanSpace.o )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils
cp -p -f attrUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/attrUtils.h
cp -p -f nastranCards.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/nastranCards.h
cp -p -f cfdTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cfdTypes.h
cp -p -f arrayUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/arrayUtils.h
cp -p -f meshUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/meshUtils.h
cp -p -f feaTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/feaTypes.h
cp -p -f miscUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/miscUtils.h
cp -p -f meshTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/meshTypes.h
cp -p -f attrTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/attrTypes.h
cp -p -f vlmTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/vlmTypes.h
cp -p -f feaUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/feaUtils.h
cp -p -f cfdUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cfdUtils.h
cp -p -f vlmUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/vlmUtils.h
cp -p -f cardTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cardTypes.h
cp -p -f jsonUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/jsonUtils.h
cp -p -f nastranUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/nastranUtils.h
cp -p -f deprecateUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/deprecateUtils.h
cp -p -f miscTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/miscTypes.h
cp -p -f tecplotUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/tecplotUtils.h
cp -p -f vlmSpanSpace.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/vlmSpanSpace.h
cp -p -f cardUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cardUtils.h
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/utils'
make -C friction 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/friction'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -Wno-format -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils frictionAIM.c \
	-o ./frictionAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer friction_eja_mod.f -o ./friction.o
gfortran -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/friction ./friction.o 
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/friction'
make -C tetgen 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tetgen'
g++ -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils tetgenAIM.cpp \
	-o ./tetgenAIM.o
g++ -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I/home/jenkins/util/tetgen/tetgen1.6.0 -I../utils \
	-DTETLIBRARY tetgen_Interface.cpp -o ./tetgen_Interface.o
g++ -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DTETLIBRARY -w /home/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o ./tetgen.o
g++ -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -O0 -w /home/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o ./predicates.o
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \
	./tetgen_Interface.o ./tetgen.o \
	./predicates.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
	-legads -ludunits2 -ldl -lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tetgen'
make -C tacs 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tacs'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils tacsAIM.c \
	-o ./tacsAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tacs'
make -C astros 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/astros'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils astrosAIM.c \
	-o ./astrosAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils astrosUtils.c \
	-o ./astrosUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils astrosCards.c \
        -o ./astrosCards.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o  ./astrosUtils.o ./astrosCards.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/astros'
make -C pointwise 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils pointwiseAIM.c \
	-o ./pointwiseAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hashElement.c \
	-o ./hashElement.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pointwiseAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pointwiseAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
	-lrt -lm -lpthread
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise'
make -C xfoil 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/xfoil'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
	xfoilAIM.c -o ./xfoilAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/xfoil'
make -C aflr2 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr2'
Not compiling aflr2AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr2'
make -C aflr4 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr4'
Not compiling aflr4AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr4'
make -C su2 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/su2'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../meshWriter/su2Writer -I../utils su2AIM.c \
	-o ./su2AIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2Utils.c \
	-o ./su2Utils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_4_Cardinal.c \
	-o ./su2_4_Cardinal.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_5_Raven.c \
	-o ./su2_5_Raven.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_6_Falcon.c \
	-o ./su2_6_Falcon.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_7_Blackbird.c \
	-o ./su2_7_Blackbird.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils su2_801_Harrier.c \
	-o ./su2_801_Harrier.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/su2AIM.so ./su2AIM.o ./su2Utils.o ./su2_4_Cardinal.o ./su2_5_Raven.o ./su2_6_Falcon.o ./su2_7_Blackbird.o ./su2_801_Harrier.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/su2'
make -C cgt 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cgt'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include egads2cgt.c \
	-o ./egads2cgt.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include aflr4egads.c \
	-o ./aflr4egads.o
g++ -g  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads -lcaps -locsm -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cgt'
make -C mses 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mses'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils msesAIM.c -o msesAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mses'
make -C egadsTess 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/egadsTess'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils egadsTessAIM.c \
	-o ./egadsTessAIM.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/egadsTessAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/egadsTessAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
	-lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/egadsTess'
make -C sierraSD 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSD'
Not compiling sierraSDAIM: SEACAS must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSD'
make -C masstran 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/masstran'
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils masstranAIM.cpp \
	-o ./masstranAIM.o
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/masstran'
make -C plato 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/plato'
Not compiling platoAIM: SEACAS must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/plato'
make -C refine 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/refine'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \
	-o ./refineAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 \
	-I../meshWriter/libmeshbWriter/libMeshb/sources \
	../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \
	-o ./libmeshb7.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/refineAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/refineAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
	-lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/refine'
make -C awave 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/awave'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils awaveAIM.c \
	-o ./awaveAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/awave'
make -C tsfoil 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tsfoil'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
	tsfoilAIM.c -o ./tsfoilAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tsfoil'
make -C delaundo 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/delaundo'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils delaundoAIM.c \
	-o ./delaundoAIM.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/delaundoAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/delaundoAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
	-lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/delaundo'
make -C abaqus 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/abaqus'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
	abaqusAIM.c -o ./abaqusAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
	abaqusUtils.c -o ./abaqusUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
	-I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/abaqusFILReader.c -o ./abaqusFILReader.o
echo "Building Abaqus with Python"
Building Abaqus with Python
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -ldl -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/abaqus'
make -C fun3d 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/fun3d'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
	-I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
	-I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython fun3dAIM.c -o ./fun3dAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
	fun3dUtils.c -o ./fun3dUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
	-I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
	-I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/fun3dNamelist.c -o ./fun3dNamelist.o
Building FUN3D with Python
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \
	./fun3dNamelist.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
	-legads -ludunits2 -ldl -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/fun3d'
make -C cbaero 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cbaero'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o cbaeroAIM.o
gcc -g  -shared -Wl,-no-undefined  cbaeroAIM.o -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/cbaeroAIM.so -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cbaero'
make -C interference 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/interference'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include interferenceAIM.c \
	-o ./interferenceAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. cloudFns.c \
	-o ./cloudFns.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/interferenceAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/interferenceAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/interferenceAIM.so \
	./interferenceAIM.o ./cloudFns.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib \
	-laimUtil -locsm -legads -ludunits2 -ldl -lstdc++ -lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/interference'
make -C meshWriter 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter'
make -C libmeshbWriter 
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/libmeshbWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include libmeshbWriter.c \
	-o ./libmeshbWriter.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -IlibMeshb/sources -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include libMeshb/sources/libmeshb7.c \
	-o ./libmeshb7.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/libmeshbWriter'
make -C fastWriter 
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/fastWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fastWriter.c \
	-o ./fastWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/fastWriter'
make -C tecplotWriter 
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/tecplotWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include tecplotWriter.c \
	-o ./tecplotWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/tecplotWriter'
make -C vtkWriter 
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/vtkWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vtkWriter.c \
	-o ./vtkWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/vtkWriter'
make -C bstlWriter 
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bstlWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include bstlWriter.c \
	-o ./bstlWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bstlWriter'
make -C bvtkWriter 
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bvtkWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include bvtkWriter.c \
	-o ./bvtkWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bvtkWriter'
make -C su2Writer 
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/su2Writer'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include su2Writer.c \
	-o ./su2Writer.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/su2Writer'
make -C stlWriter 
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/stlWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include stlWriter.c \
	-o ./stlWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/stlWriter'
make -C ugridWriter 
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/ugridWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include ugridWriter.c \
	-o ./ugridWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/ugridWriter'
make -C exodusWriter 
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter'
make[3]: Nothing to be done for `default'.
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter'
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter'
make -C cart3d 
make[2]: xml2-config: Command not found
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cart3d'
XML developer libarary missing. Not compiling cart3dAIM.
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cart3d'
make -C nastran 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/nastran'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils nastranAIM.c \
	-o ./nastranAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/nastran'
make -C spinnaker 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/spinnaker'
make[2]: Nothing to be done for `default'.
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/spinnaker'
make -C aflr3 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr3'
Not compiling aflr3AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr3'
make -C sierraSM 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSM'
Not compiling sierraSMAIM: SEACAS must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSM'
make -C hsm 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hsmAIM.c \
	-o src/hsmAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hsmUtils.c \
	-o src/hsmUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hsmAdj.c \
	-o src/hsmAdj.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -Wno-comment rcm/rcm.cpp -DREVISION=7.8 \
	-o src/rcm.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 rcm/genrcmi.cpp -DREVISION=7.8 \
	-o src/genrcmi.o
make -C src hsmglr.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmglr.f -o ./hsmglr.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmbc.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmbc.f -o ./hsmbc.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmbb2.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmbb2.f -o ./hsmbb2.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmre1.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmre1.f -o ./hsmre1.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmdep.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmdep.f -o ./hsmdep.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmrfm.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmrfm.f -o ./hsmrfm.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmout.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmout.f -o ./hsmout.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmren.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmren.f -o ./hsmren.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmprj.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmprj.f -o ./hsmprj.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src atanc.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  atanc.f -o ./atanc.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src cross.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  cross.f -o ./cross.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src ludcmp.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  ludcmp.f -o ./ludcmp.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmabd.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmabd.f -o ./hsmabd.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src bmdump.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  bmdump.f -o ./bmdump.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmrun.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o ./hsmrun.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmeqn.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmeqn.f -o ./hsmeqn.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmsol.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmsol.f -o ./hsmsol.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmgeo.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  hsmgeo.f -o ./hsmgeo.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src sbsolve.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g  -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero  sbsolve.f -o ./sbsolve.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a hsmsol.o hsmdep.o hsmout.o hsmgeo.o hsmabd.o hsmeqn.o hsmbc.o hsmprj.o hsmren.o hsmre1.o hsmrfm.o hsmbb2.o hsmglr.o ludcmp.o sbsolve.o atanc.o bmdump.o cross.o )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hsmAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hsmAIM.so
gfortran -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hsmAIM.so \
	src/hsmAIM.o src/hsmUtils.o src/hsmAdj.o \
	src/rcm.o src/genrcmi.o \
	 -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
	-legads -ludunits2 -lhsm -ldl  -lstdc++ 
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm'
make -C avl 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/avl'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils avlAIM.c -o ./avlAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o avlRead_ELE.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o avlRead_DERMATB.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o avlRead_HINGE.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o avlRead_BODY.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o avlRead_CNC.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o avlRead_TOT.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o avlRead_DERMATS.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o avlRead_STRP.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o avlRead_VM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o avlRead_CPOML.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o avlRead_DERMATM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o avlRead_SURF.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/avlAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/avlAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/avlAIM.so ./avlAIM.o ./avlRead_ELE.o ./avlRead_DERMATB.o ./avlRead_HINGE.o ./avlRead_BODY.o ./avlRead_CNC.o ./avlRead_TOT.o ./avlRead_DERMATS.o ./avlRead_STRP.o ./avlRead_VM.o ./avlRead_CPOML.o ./avlRead_DERMATM.o ./avlRead_SURF.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \
	-lstdc++ -lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/avl'
make -C custom 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/custom'
make[2]: Nothing to be done for `default'.
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/custom'
make -C skeleton 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/skeleton'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils skeletonAIM.c \
	-o ./skeletonAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/skeleton'
make -C unitTest 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest'
make[2]: Nothing to be done for `all'.
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest'
make -C mystran 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mystran'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils mystranAIM.c \
	-o ./mystranAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils mystranUtils.c \
	-o ./mystranUtils.o
gcc -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \
	-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mystran'
make -C zaero 
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/zaero'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroAIM.c -o zaeroAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroUtils.c -o zaeroUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroLinearFlutter.c -o zaeroLinearFlutter.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroTrim.c -o zaeroTrim.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroTypes.c -o zaeroTypes.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroCards.c -o zaeroCards.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroGeneral.c -o zaeroGeneral.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o
gcc -g  -shared -Wl,-no-undefined   -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/zaeroAIM.so ./zaeroAIM.o ./zaeroUtils.o ./zaeroLinearFlutter.o ./zaeroTrim.o ./zaeroTypes.o ./zaeroCards.o ./zaeroGeneral.o ./zaeroGraphical.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/zaero'
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim'
(cd OpenCSM; make -f serveESP.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/capsMode.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/capsMode.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flowchart.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flowchart.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/viewer.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/viewer.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/viewer.so ./timViewer.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 timPyscript.c -o ./timPyscript.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pyscript.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pyscript.so
g++ -g  -shared -Wl,-no-undefined  -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pyscript.so ./timPyscript.o -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lrt -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM'
 
 *** Build Completed! ***
+ export CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data
+ CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin
++ uname -a
+ [[ Linux reynolds-centOS7 3.10.0-1160.108.1.el7.x86_64 #1 SMP Thu Jan 25 16:17:31 UTC 2024 x86_64 x86_64 x86_64 GNU/Linux == *\D\a\r\w\i\n* ]]
+ sed -i 's/.*capsExamples.*/#&/' /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/Verification.sh
+ bash -ex /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/Verification.sh
+ expectSuccess 01 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions.csm:1914]]
        signal 1 thrown by user
    --> catching signal 1 (UNKNOWN)
ERROR:: (illegal_value) in Branch Brch_001813 at [[/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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	0m0.084s
user	0m0.070s
sys	0m0.014s
+ set +x

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

+ expectSuccess 02 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/demo2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.341s
user	0m0.426s
sys	0m0.028s
+ set +x

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

+ expectSuccess 03 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/verify_7.8.0/tutorial1_whole.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m2.618s
user	0m3.968s
sys	0m0.097s
+ set +x

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

+ expectSuccess 04 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/design2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/design2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.605s
user	0m0.744s
sys	0m0.027s
+ set +x

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

+ expectSuccess 05 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/design3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/design3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.578s
user	0m0.843s
sys	0m0.033s
+ set +x

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

+ expectSuccess 06 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/verify_7.8.0/tutorial2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.522s
user	0m0.758s
sys	0m0.026s
+ set +x

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

+ expectSuccess 07 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/verify_7.8.0/tutorial3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m3.804s
user	0m5.184s
sys	0m0.140s
+ set +x

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

+ expectSuccess 08 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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	0m29.174s
user	0m46.176s
sys	0m0.621s
+ set +x

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

+ expectSuccess 09 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/bottle
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/verify_7.8.0/bottle.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m1.395s
user	0m0.830s
sys	0m0.020s
+ set +x

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

+ expectSuccess 10 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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	0m37.593s
user	1m1.127s
sys	0m0.837s
+ set +x

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

+ expectSuccess 11 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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	0m0.512s
user	0m0.295s
sys	0m0.026s
+ set +x

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

+ expectSuccess 12 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/connect5.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.806s
user	0m0.812s
sys	0m0.020s
+ set +x

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

+ expectSuccess 13 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/group2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/group2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.304s
user	0m0.170s
sys	0m0.022s
+ set +x

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

+ expectSuccess 14 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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	0m0.373s
user	0m0.480s
sys	0m0.026s
+ set +x

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

+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/testEGADS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
....................................................   PCurve Map: 48 (alloc 48)!
   Surface Map: 12 (alloc 24)!
   Curve Map: 28 (alloc 28)!
 Writing PCurves...
 Writing Curves...
 Writing Surfaces...
 Writing 16 Nodes...
 Writing 28 Edges...
 Writing 12 Loops...
 Writing 12 Faces...
 Writing 1 Shells...
 EGADS Info: 0 Objects, 0 Reference in Use (of 972) at Close!
...................
----------------------------------------------------------------------
Ran 71 tests in 2.048s

OK
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/testOCSM
+ source /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp

real	0m6.015s
user	0m10.328s
sys	0m0.159s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/testCAPS
+ make test
python --version
Python 3.11.9
python -u -m unittest discover
..Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing1, index = 1
	Name = Wing2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 143
	Number of elements = 282
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 282
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 140
	Number of elements = 276
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 276
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 283
	Combined Number of elements = 558
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 558
	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 12.001s

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 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/
+ make test
python --version
Python 3.11.9
python -u -m unittest discover --verbose
Please set the environment variable ASTROS_ROOT
test_journal (test_aflr2.TestAFLR2.test_journal) ... Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2    : Compile Date   04/23/24 @ 12:17PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2244      2244
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       450       902
AFLR2 IG : Nodes, Faces      =       900      1802
AFLR2 IG : Nodes, Faces      =      1145      2292
AFLR2 IG : Nodes, Faces      =      1260      2522
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1360      2722
AFLR2 IG : Nodes, Faces      =      1460      2922
AFLR2 IG : Nodes, Faces      =      1560      3122
AFLR2 IG : Nodes, Faces      =      1660      3322
AFLR2 IG : Nodes, Faces      =      1760      3522
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1860      3722
AFLR2 IG : Nodes, Faces      =      1960      3922
AFLR2 IG : Nodes, Faces      =      2060      4122
AFLR2 IG : Nodes, Faces      =      2085      4172
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.040   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4283      6322
AFLR2 GG : Nodes, Faces      =      6128     10012
AFLR2 GG : Nodes, Faces      =      7863     13482
AFLR2 GG : Nodes, Faces      =      9464     16684
AFLR2 GG : Nodes, Faces      =     10948     19652
AFLR2 GG : Nodes, Faces      =     12322     22400
AFLR2 GG : Nodes, Faces      =     13619     24994
AFLR2 GG : Nodes, Faces      =     14829     27414
AFLR2 GG : Nodes, Faces      =     15981     29718
AFLR2 GG : Nodes, Faces      =     17082     31920
AFLR2 GG : Nodes, Faces      =     18110     33976
AFLR2 GG : Nodes, Faces      =     19081     35918
AFLR2 GG : Nodes, Faces      =     20014     37784
AFLR2 GG : Nodes, Faces      =     20924     39604
AFLR2 GG : Nodes, Faces      =     21782     41320
AFLR2 GG : Nodes, Faces      =     22595     42946
AFLR2 GG : Nodes, Faces      =     23377     44510
AFLR2 GG : Nodes, Faces      =     24129     46014
AFLR2 GG : Nodes, Faces      =     24840     47436
AFLR2 GG : Nodes, Faces      =     25522     48800
AFLR2 GG : Nodes, Faces      =     26170     50096
AFLR2 GG : Nodes, Faces      =     26793     51342
AFLR2 GG : Nodes, Faces      =     27346     52448
AFLR2 GG : Nodes, Faces      =     27846     53448
AFLR2 GG : Nodes, Faces      =     28280     54316
AFLR2 GG : Nodes, Faces      =     28652     55060
AFLR2 GG : Nodes, Faces      =     28920     55596
AFLR2 GG : Nodes, Faces      =     29143     56042
AFLR2 GG : Nodes, Faces      =     29358     56472
AFLR2 GG : Nodes, Faces      =     29550     56856
AFLR2 GG : Nodes, Faces      =     29693     57142
AFLR2 GG : Nodes, Faces      =     29805     57366
AFLR2 GG : Nodes, Faces      =     29875     57506
AFLR2 GG : Nodes, Faces      =     29895     57546
AFLR2 GG : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.127   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.009   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
Getting 2D mesh for body 1 (of 1)
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2224         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2224      2224
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       446       894
AFLR2 IG : Nodes, Faces      =       892      1786
AFLR2 IG : Nodes, Faces      =       918      1838
AFLR2 IG : Nodes, Faces      =      1033      2068
AFLR2 IG : Nodes, Faces      =      1133      2268
AFLR2 IG : Nodes, Faces      =      1233      2468
AFLR2 IG : Nodes, Faces      =      1333      2668
AFLR2 IG : Nodes, Faces      =      1338      2678
AFLR2 IG : Nodes, Faces      =      1433      2868
AFLR2 IG : Nodes, Faces      =      1533      3068
AFLR2 IG : Nodes, Faces      =      1633      3268
AFLR2 IG : Nodes, Faces      =      1733      3468
AFLR2 IG : Nodes, Faces      =      1784      3570
AFLR2 IG : Nodes, Faces      =      1833      3668
AFLR2 IG : Nodes, Faces      =      1858      3718
AFLR2 IG : Nodes, Faces      =      2224      4450
AFLR2 IG : Nodes, Faces      =      2228      4450
AFLR2 IG : Nodes, Faces      =      2224      2224
 
AFLR2    : CPU Time          =     0.029   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4122      6020
AFLR2 GG : Nodes, Faces      =      5812      9400
AFLR2 GG : Nodes, Faces      =      7299     12374
AFLR2 GG : Nodes, Faces      =      8574     14924
AFLR2 GG : Nodes, Faces      =      9729     17234
AFLR2 GG : Nodes, Faces      =     10787     19350
AFLR2 GG : Nodes, Faces      =     11767     21310
AFLR2 GG : Nodes, Faces      =     12683     23142
AFLR2 GG : Nodes, Faces      =     13516     24808
AFLR2 GG : Nodes, Faces      =     14278     26332
AFLR2 GG : Nodes, Faces      =     14999     27774
AFLR2 GG : Nodes, Faces      =     15682     29140
AFLR2 GG : Nodes, Faces      =     16312     30400
AFLR2 GG : Nodes, Faces      =     16899     31574
AFLR2 GG : Nodes, Faces      =     17451     32678
AFLR2 GG : Nodes, Faces      =     17959     33694
AFLR2 GG : Nodes, Faces      =     18443     34662
AFLR2 GG : Nodes, Faces      =     18877     35530
AFLR2 GG : Nodes, Faces      =     19283     36342
AFLR2 GG : Nodes, Faces      =     19650     37076
AFLR2 GG : Nodes, Faces      =     19994     37764
AFLR2 GG : Nodes, Faces      =     20325     38426
AFLR2 GG : Nodes, Faces      =     20638     39052
AFLR2 GG : Nodes, Faces      =     20940     39656
AFLR2 GG : Nodes, Faces      =     21240     40256
AFLR2 GG : Nodes, Faces      =     21523     40822
AFLR2 GG : Nodes, Faces      =     21792     41360
AFLR2 GG : Nodes, Faces      =     22053     41882
AFLR2 GG : Nodes, Faces      =     22305     42386
AFLR2 GG : Nodes, Faces      =     22521     42818
AFLR2 GG : Nodes, Faces      =     22696     43168
AFLR2 GG : Nodes, Faces      =     22829     43434
AFLR2 GG : Nodes, Faces      =     22953     43682
AFLR2 GG : Nodes, Faces      =     23050     43876
AFLR2 GG : Nodes, Faces      =     23110     43996
AFLR2 GG : Nodes, Faces      =     23139     44054
AFLR2 GG : Nodes, Faces      =     23157     44090
AFLR2 GG : Nodes, Faces      =     23175     44126
AFLR2 GG : Nodes, Faces      =     23183     44142
AFLR2 GG : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.102   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.006   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2244      2244
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       450       902
AFLR2 IG : Nodes, Faces      =       900      1802
AFLR2 IG : Nodes, Faces      =      1145      2292
AFLR2 IG : Nodes, Faces      =      1260      2522
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1360      2722
AFLR2 IG : Nodes, Faces      =      1460      2922
AFLR2 IG : Nodes, Faces      =      1560      3122
AFLR2 IG : Nodes, Faces      =      1660      3322
AFLR2 IG : Nodes, Faces      =      1760      3522
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1860      3722
AFLR2 IG : Nodes, Faces      =      1960      3922
AFLR2 IG : Nodes, Faces      =      2060      4122
AFLR2 IG : Nodes, Faces      =      2085      4172
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.037   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4283      6322
AFLR2 GG : Nodes, Faces      =      6128     10012
AFLR2 GG : Nodes, Faces      =      7863     13482
AFLR2 GG : Nodes, Faces      =      9464     16684
AFLR2 GG : Nodes, Faces      =     10948     19652
AFLR2 GG : Nodes, Faces      =     12322     22400
AFLR2 GG : Nodes, Faces      =     13619     24994
AFLR2 GG : Nodes, Faces      =     14829     27414
AFLR2 GG : Nodes, Faces      =     15981     29718
AFLR2 GG : Nodes, Faces      =     17082     31920
AFLR2 GG : Nodes, Faces      =     18110     33976
AFLR2 GG : Nodes, Faces      =     19081     35918
AFLR2 GG : Nodes, Faces      =     20014     37784
AFLR2 GG : Nodes, Faces      =     20924     39604
AFLR2 GG : Nodes, Faces      =     21782     41320
AFLR2 GG : Nodes, Faces      =     22595     42946
AFLR2 GG : Nodes, Faces      =     23377     44510
AFLR2 GG : Nodes, Faces      =     24129     46014
AFLR2 GG : Nodes, Faces      =     24840     47436
AFLR2 GG : Nodes, Faces      =     25522     48800
AFLR2 GG : Nodes, Faces      =     26170     50096
AFLR2 GG : Nodes, Faces      =     26793     51342
AFLR2 GG : Nodes, Faces      =     27346     52448
AFLR2 GG : Nodes, Faces      =     27846     53448
AFLR2 GG : Nodes, Faces      =     28280     54316
AFLR2 GG : Nodes, Faces      =     28652     55060
AFLR2 GG : Nodes, Faces      =     28920     55596
AFLR2 GG : Nodes, Faces      =     29143     56042
AFLR2 GG : Nodes, Faces      =     29358     56472
AFLR2 GG : Nodes, Faces      =     29550     56856
AFLR2 GG : Nodes, Faces      =     29693     57142
AFLR2 GG : Nodes, Faces      =     29805     57366
AFLR2 GG : Nodes, Faces      =     29875     57506
AFLR2 GG : Nodes, Faces      =     29895     57546
AFLR2 GG : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.099   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.007   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
 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 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2224         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2224      2224
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       446       894
AFLR2 IG : Nodes, Faces      =       892      1786
AFLR2 IG : Nodes, Faces      =       918      1838
AFLR2 IG : Nodes, Faces      =      1033      2068
AFLR2 IG : Nodes, Faces      =      1133      2268
AFLR2 IG : Nodes, Faces      =      1233      2468
AFLR2 IG : Nodes, Faces      =      1333      2668
AFLR2 IG : Nodes, Faces      =      1338      2678
AFLR2 IG : Nodes, Faces      =      1433      2868
AFLR2 IG : Nodes, Faces      =      1533      3068
AFLR2 IG : Nodes, Faces      =      1633      3268
AFLR2 IG : Nodes, Faces      =      1733      3468
AFLR2 IG : Nodes, Faces      =      1784      3570
AFLR2 IG : Nodes, Faces      =      1833      3668
AFLR2 IG : Nodes, Faces      =      1858      3718
AFLR2 IG : Nodes, Faces      =      2224      4450
AFLR2 IG : Nodes, Faces      =      2228      4450
AFLR2 IG : Nodes, Faces      =      2224      2224
 
AFLR2    : CPU Time          =     0.034   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4122      6020
AFLR2 GG : Nodes, Faces      =      5812      9400
AFLR2 GG : Nodes, Faces      =      7299     12374
AFLR2 GG : Nodes, Faces      =      8574     14924
AFLR2 GG : Nodes, Faces      =      9729     17234
AFLR2 GG : Nodes, Faces      =     10787     19350
AFLR2 GG : Nodes, Faces      =     11767     21310
AFLR2 GG : Nodes, Faces      =     12683     23142
AFLR2 GG : Nodes, Faces      =     13516     24808
AFLR2 GG : Nodes, Faces      =     14278     26332
AFLR2 GG : Nodes, Faces      =     14999     27774
AFLR2 GG : Nodes, Faces      =     15682     29140
AFLR2 GG : Nodes, Faces      =     16312     30400
AFLR2 GG : Nodes, Faces      =     16899     31574
AFLR2 GG : Nodes, Faces      =     17451     32678
AFLR2 GG : Nodes, Faces      =     17959     33694
AFLR2 GG : Nodes, Faces      =     18443     34662
AFLR2 GG : Nodes, Faces      =     18877     35530
AFLR2 GG : Nodes, Faces      =     19283     36342
AFLR2 GG : Nodes, Faces      =     19650     37076
AFLR2 GG : Nodes, Faces      =     19994     37764
AFLR2 GG : Nodes, Faces      =     20325     38426
AFLR2 GG : Nodes, Faces      =     20638     39052
AFLR2 GG : Nodes, Faces      =     20940     39656
AFLR2 GG : Nodes, Faces      =     21240     40256
AFLR2 GG : Nodes, Faces      =     21523     40822
AFLR2 GG : Nodes, Faces      =     21792     41360
AFLR2 GG : Nodes, Faces      =     22053     41882
AFLR2 GG : Nodes, Faces      =     22305     42386
AFLR2 GG : Nodes, Faces      =     22521     42818
AFLR2 GG : Nodes, Faces      =     22696     43168
AFLR2 GG : Nodes, Faces      =     22829     43434
AFLR2 GG : Nodes, Faces      =     22953     43682
AFLR2 GG : Nodes, Faces      =     23050     43876
AFLR2 GG : Nodes, Faces      =     23110     43996
AFLR2 GG : Nodes, Faces      =     23139     44054
AFLR2 GG : Nodes, Faces      =     23157     44090
AFLR2 GG : Nodes, Faces      =     23175     44126
AFLR2 GG : Nodes, Faces      =     23183     44142
AFLR2 GG : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.106   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.031   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
ok
test_phase (test_aflr2.TestAFLR2.test_phase) ... Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2244         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2244      2244
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       450       902
AFLR2 IG : Nodes, Faces      =       900      1802
AFLR2 IG : Nodes, Faces      =      1145      2292
AFLR2 IG : Nodes, Faces      =      1260      2522
AFLR2 IG : Nodes, Faces      =      1350      2702
AFLR2 IG : Nodes, Faces      =      1360      2722
AFLR2 IG : Nodes, Faces      =      1460      2922
AFLR2 IG : Nodes, Faces      =      1560      3122
AFLR2 IG : Nodes, Faces      =      1660      3322
AFLR2 IG : Nodes, Faces      =      1760      3522
AFLR2 IG : Nodes, Faces      =      1800      3602
AFLR2 IG : Nodes, Faces      =      1860      3722
AFLR2 IG : Nodes, Faces      =      1960      3922
AFLR2 IG : Nodes, Faces      =      2060      4122
AFLR2 IG : Nodes, Faces      =      2085      4172
AFLR2 IG : Nodes, Faces      =      2244      4490
AFLR2 IG : Nodes, Faces      =      2248      4490
AFLR2 IG : Nodes, Faces      =      2244      2244
 
AFLR2    : CPU Time          =     0.032   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4283      6322
AFLR2 GG : Nodes, Faces      =      6128     10012
AFLR2 GG : Nodes, Faces      =      7863     13482
AFLR2 GG : Nodes, Faces      =      9464     16684
AFLR2 GG : Nodes, Faces      =     10948     19652
AFLR2 GG : Nodes, Faces      =     12322     22400
AFLR2 GG : Nodes, Faces      =     13619     24994
AFLR2 GG : Nodes, Faces      =     14829     27414
AFLR2 GG : Nodes, Faces      =     15981     29718
AFLR2 GG : Nodes, Faces      =     17082     31920
AFLR2 GG : Nodes, Faces      =     18110     33976
AFLR2 GG : Nodes, Faces      =     19081     35918
AFLR2 GG : Nodes, Faces      =     20014     37784
AFLR2 GG : Nodes, Faces      =     20924     39604
AFLR2 GG : Nodes, Faces      =     21782     41320
AFLR2 GG : Nodes, Faces      =     22595     42946
AFLR2 GG : Nodes, Faces      =     23377     44510
AFLR2 GG : Nodes, Faces      =     24129     46014
AFLR2 GG : Nodes, Faces      =     24840     47436
AFLR2 GG : Nodes, Faces      =     25522     48800
AFLR2 GG : Nodes, Faces      =     26170     50096
AFLR2 GG : Nodes, Faces      =     26793     51342
AFLR2 GG : Nodes, Faces      =     27346     52448
AFLR2 GG : Nodes, Faces      =     27846     53448
AFLR2 GG : Nodes, Faces      =     28280     54316
AFLR2 GG : Nodes, Faces      =     28652     55060
AFLR2 GG : Nodes, Faces      =     28920     55596
AFLR2 GG : Nodes, Faces      =     29143     56042
AFLR2 GG : Nodes, Faces      =     29358     56472
AFLR2 GG : Nodes, Faces      =     29550     56856
AFLR2 GG : Nodes, Faces      =     29693     57142
AFLR2 GG : Nodes, Faces      =     29805     57366
AFLR2 GG : Nodes, Faces      =     29875     57506
AFLR2 GG : Nodes, Faces      =     29895     57546
AFLR2 GG : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.103   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.008   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
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 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =        48         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =        48        48
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        10        22
AFLR2 IG : Nodes, Faces      =        20        42
AFLR2 IG : Nodes, Faces      =        30        62
AFLR2 IG : Nodes, Faces      =        40        82
AFLR2 IG : Nodes, Faces      =        45        92
AFLR2 IG : Nodes, Faces      =        46        94
AFLR2 IG : Nodes, Faces      =        48        98
AFLR2 IG : Nodes, Faces      =        52        98
AFLR2 IG : Nodes, Faces      =        48        48
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =        48        48
AFLR2 GG : Nodes, Faces      =        88       128
AFLR2 GG : Nodes, Faces      =       109       170
AFLR2 GG : Nodes, Faces      =       124       200
AFLR2 GG : Nodes, Faces      =       136       224
AFLR2 GG : Nodes, Faces      =       148       248
AFLR2 GG : Nodes, Faces      =       161       274
AFLR2 GG : Nodes, Faces      =       171       294
AFLR2 GG : Nodes, Faces      =       181       314
AFLR2 GG : Nodes, Faces      =       187       326
AFLR2 GG : Nodes, Faces      =       190       332
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =       190       332
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

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

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       339       680
AFLR2 IG : Nodes, Faces      =       340       682
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =       344       344
AFLR2 GG : Nodes, Faces      =       679      1014
AFLR2 GG : Nodes, Faces      =      1006      1668
AFLR2 GG : Nodes, Faces      =      1321      2298
AFLR2 GG : Nodes, Faces      =      1604      2864
AFLR2 GG : Nodes, Faces      =      1886      3428
AFLR2 GG : Nodes, Faces      =      2155      3966
AFLR2 GG : Nodes, Faces      =      2409      4474
AFLR2 GG : Nodes, Faces      =      2649      4954
AFLR2 GG : Nodes, Faces      =      2867      5390
AFLR2 GG : Nodes, Faces      =      3063      5782
AFLR2 GG : Nodes, Faces      =      3243      6142
AFLR2 GG : Nodes, Faces      =      3400      6456
AFLR2 GG : Nodes, Faces      =      3540      6736
AFLR2 GG : Nodes, Faces      =      3665      6986
AFLR2 GG : Nodes, Faces      =      3786      7228
AFLR2 GG : Nodes, Faces      =      3900      7456
AFLR2 GG : Nodes, Faces      =      4010      7676
AFLR2 GG : Nodes, Faces      =      4114      7884
AFLR2 GG : Nodes, Faces      =      4209      8074
AFLR2 GG : Nodes, Faces      =      4292      8240
AFLR2 GG : Nodes, Faces      =      4368      8392
AFLR2 GG : Nodes, Faces      =      4439      8534
AFLR2 GG : Nodes, Faces      =      4503      8662
AFLR2 GG : Nodes, Faces      =      4560      8776
AFLR2 GG : Nodes, Faces      =      4611      8878
AFLR2 GG : Nodes, Faces      =      4650      8956
AFLR2 GG : Nodes, Faces      =      4677      9010
AFLR2 GG : Nodes, Faces      =      4695      9046
AFLR2 GG : Nodes, Faces      =      4705      9066
 
AFLR2    : CPU Time          =     0.011   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4705      9066
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 4705
Number of elements = 9410
Number of tris = 9066
Number of quad = 0

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


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

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


Writing vtk file ....

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


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


Writing FAST file ....
Finished writing FAST file


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


Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       339       680
AFLR2 IG : Nodes, Faces      =       340       682
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       682      1020
AFLR2 GGp: Nodes, Faces      =      1010      1676
AFLR2 GGp: Nodes, Faces      =      1316      2288
AFLR2 GGp: Nodes, Faces      =      1592      2840
AFLR2 GGp: Nodes, Faces      =      1855      3366
AFLR2 GGp: Nodes, Faces      =      2106      3868
AFLR2 GGp: Nodes, Faces      =      2341      4338
AFLR2 GGp: Nodes, Faces      =      2551      4758
AFLR2 GGp: Nodes, Faces      =      2741      5138
AFLR2 GGp: Nodes, Faces      =      2917      5490
AFLR2 GGp: Nodes, Faces      =      3082      5820
AFLR2 GGp: Nodes, Faces      =      3240      6136
AFLR2 GGp: Nodes, Faces      =      3379      6414
AFLR2 GGp: Nodes, Faces      =      3513      6682
AFLR2 GGp: Nodes, Faces      =      3642      6940
AFLR2 GGp: Nodes, Faces      =      3748      7152
AFLR2 GGp: Nodes, Faces      =      3846      7348
AFLR2 GGp: Nodes, Faces      =      3931      7518
AFLR2 GGp: Nodes, Faces      =      3999      7654
AFLR2 GGp: Nodes, Faces      =      4044      7744
AFLR2 GGp: Nodes, Faces      =      4058      7772
 
AFLR2    : CPU Time          =     0.018   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4058      7772
AFLR2 QI : Nodes, Faces      =      4057       364
AFLR2 QI : Nodes, Faces      =      4057      3703
AFLR2 QI : Nodes, Faces      =      4057      7770
AFLR2 QI : Nodes, Faces      =      4056       344
AFLR2 QI : Nodes, Faces      =      4056      3712
AFLR2 QI : Nodes, Faces      =      4056      7768
AFLR2 QI : Nodes, Faces      =      4055       348
AFLR2 QI : Nodes, Faces      =      4055      3709
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       392
AFLR2 QI : Nodes, Faces      =      4055      3687
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
 
AFLR2    : CPU Time          =     0.011   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

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

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


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

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


Writing vtk file ....

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


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


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

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 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       339       680
AFLR2 IG : Nodes, Faces      =       340       682
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       682      1020
AFLR2 GGp: Nodes, Faces      =      1010      1676
AFLR2 GGp: Nodes, Faces      =      1316      2288
AFLR2 GGp: Nodes, Faces      =      1592      2840
AFLR2 GGp: Nodes, Faces      =      1855      3366
AFLR2 GGp: Nodes, Faces      =      2106      3868
AFLR2 GGp: Nodes, Faces      =      2341      4338
AFLR2 GGp: Nodes, Faces      =      2551      4758
AFLR2 GGp: Nodes, Faces      =      2741      5138
AFLR2 GGp: Nodes, Faces      =      2917      5490
AFLR2 GGp: Nodes, Faces      =      3082      5820
AFLR2 GGp: Nodes, Faces      =      3240      6136
AFLR2 GGp: Nodes, Faces      =      3379      6414
AFLR2 GGp: Nodes, Faces      =      3513      6682
AFLR2 GGp: Nodes, Faces      =      3642      6940
AFLR2 GGp: Nodes, Faces      =      3748      7152
AFLR2 GGp: Nodes, Faces      =      3846      7348
AFLR2 GGp: Nodes, Faces      =      3931      7518
AFLR2 GGp: Nodes, Faces      =      3999      7654
AFLR2 GGp: Nodes, Faces      =      4044      7744
AFLR2 GGp: Nodes, Faces      =      4058      7772
 
AFLR2    : CPU Time          =     0.013   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4058      7772
AFLR2 QI : Nodes, Faces      =      4057       364
AFLR2 QI : Nodes, Faces      =      4057      3703
AFLR2 QI : Nodes, Faces      =      4057      7770
AFLR2 QI : Nodes, Faces      =      4056       344
AFLR2 QI : Nodes, Faces      =      4056      3712
AFLR2 QI : Nodes, Faces      =      4056      7768
AFLR2 QI : Nodes, Faces      =      4055       348
AFLR2 QI : Nodes, Faces      =      4055      3709
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       392
AFLR2 QI : Nodes, Faces      =      4055      3687
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
 
AFLR2    : CPU Time          =     0.007   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

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

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box, index = 1
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2    : Compile Date   04/23/24 @ 12:17PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR4    : Compile Date   04/23/24 @ 12:17PM
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          = 6092
	Number of elements       = 33723
	Number of triangles      = 4434
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 29289
	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          = 13578
	Number of elements       = 76165
	Number of triangles      = 8144
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 68021
	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          = 42341
	Number of elements       = 240656
	Number of triangles      = 19890
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 220766
	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          = 4356
	Number of elements       = 24173
	Number of triangles      = 3018
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 21155
	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          = 10984
	Number of elements       = 60667
	Number of triangles      = 8628
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 52039
	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          = 10678
	Number of elements       = 59894
	Number of triangles      = 6366
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 53528
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Getting volume mesh for body 1 (of 7)

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

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

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

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

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

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

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

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

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

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 89218
	Number of elements       = 501527
	Number of triangles      = 51812
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 449715
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_all (test_aflr3.TestAFLR3.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = farfield, index = 8
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = farfield, index = 8
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 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          = 16488
	Number of elements       = 93795
	Number of triangles      = 7926
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 85869
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 3649
	Number of elements       = 19777
	Number of triangles      = 3394
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 16383
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5514
	Number of elements       = 30658
	Number of triangles      = 3656
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 27002
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5092
	Number of elements       = 27888
	Number of triangles      = 4070
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 23818
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5238
	Number of elements       = 28440
	Number of triangles      = 4622
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 23818
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 4902
	Number of elements       = 26933
	Number of triangles      = 4038
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 22895
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 336
	Number of elements       = 1507
	Number of triangles      = 584
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 923
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 33106
	Number of elements       = 191761
	Number of triangles      = 8496
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 183265
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

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

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

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 36447
	Number of elements       = 205093
	Number of triangles      = 21828
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 183265
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 5):
	Number of nodes          = 28882
	Number of elements       = 164134
	Number of triangles      = 15162
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 148972
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 5):
	Number of nodes          = 1415
	Number of elements       = 7515
	Number of triangles      = 1456
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6059
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 3 (of 5):
	Number of nodes          = 4186
	Number of elements       = 23181
	Number of triangles      = 2942
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 20239
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 5 (of 5):
	Number of nodes          = 1253
	Number of elements       = 6578
	Number of triangles      = 1424
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5154
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 16786
	Number of elements       = 95215
	Number of triangles      = 8798
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 86417
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

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

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 18710
	Number of elements       = 102591
	Number of triangles      = 16174
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 86417
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 1 (of 2):
	Number of nodes          = 12124
	Number of elements       = 68112
	Number of triangles      = 7138
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 60974
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh for body 2 (of 2):
	Number of nodes          = 6586
	Number of elements       = 34479
	Number of triangles      = 9036
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 25443
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_journal (test_aflr3.TestAFLR3.test_journal) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2940
	Number of elements       = 12771
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7319
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2497
	Number of elements       = 10947
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6395
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2940
	Number of elements       = 12771
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7319
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2497
	Number of elements       = 10947
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6395
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
ok
test_phase (test_aflr3.TestAFLR3.test_phase) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2940
	Number of elements       = 12771
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7319
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2497
	Number of elements       = 10947
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6395
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_reenter (test_aflr3.TestAFLR3.test_reenter) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 2940
	Number of elements       = 12771
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7319
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

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


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


Writing Tecplot file ....
Finished writing Tecplot file


Writing vtk file ....

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


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


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 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          = 2497
	Number of elements       = 10947
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6395
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

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


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


Writing Tecplot file ....
Finished writing Tecplot file


Writing vtk file ....

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


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


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 5047
	Number of elements       = 27987
	Number of triangles      = 3464
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 24523
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 6342
	Number of elements       = 35410
	Number of triangles      = 4052
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 31358
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_transp (test_aflr3.TestAFLR3.test_transp) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file

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

Getting mesh sizing parameters
	Mesh sizing name - Wake
	Done getting mesh sizing parameters
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 60311
	Number of elements       = 351913
	Number of triangles      = 12928
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 338985
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Getting mesh sizing parameters
	Mesh sizing name - Wake
	Done getting mesh sizing parameters
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 59175
	Number of elements       = 344623
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 332195
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Getting mesh sizing parameters
	Mesh sizing name - Wake
	Done getting mesh sizing parameters
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 60311
	Number of elements       = 351413
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 338985
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
ok
test_SingleBody_output (test_aflr4.TestAFLR4.test_SingleBody_output) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - trailingEdge
	Done getting mesh sizing parameters
ok
test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = farfield, index = 8
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ok
test_box (test_aflr4.TestAFLR4.test_box) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ok
test_boxhole (test_aflr4.TestAFLR4.test_boxhole) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = boxhole, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_bullet (test_aflr4.TestAFLR4.test_bullet) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = bullet, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_cone (test_aflr4.TestAFLR4.test_cone) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cone, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_cylinder (test_aflr4.TestAFLR4.test_cylinder) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_faceMatch (test_aflr4.TestAFLR4.test_faceMatch) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_faceMatch_MultiDomain (test_aflr4.TestAFLR4.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file

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

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

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

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


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


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


Writing vtk file ....

Writing vtk surface file ....

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


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


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file


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


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


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


Writing vtk file ....

Writing vtk surface file ....

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


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


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file

ok
test_setInput (test_aflr4.TestAFLR4.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = sphere, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_torus (test_aflr4.TestAFLR4.test_torus) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = torus, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_Aeroelastic (test_astros.TestAstros.test_Aeroelastic) ... skipped 'No astros.exe executable'
test_Plate (test_astros.TestAstros.test_Plate) ... skipped 'No astros.exe executable'
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
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
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
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_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) ... skipped 'No flowCart executable'
test_outputs (test_cart3d.TestCart3D.test_outputs) ... skipped 'No flowCart executable'
test_reenter (test_cart3d.TestCart3D.test_reenter) ... skipped 'No flowCart executable'
test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... skipped 'No flowCart executable'
test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... skipped 'No flowCart executable'
test_Output (test_cbaero.TestCBAERO.test_Output) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing1, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = Wing1, index = 1
	Name = trailingEdge, index = 2

Writing FAST file ....
Finished writing FAST file

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

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

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
ok
test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 9
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = nodeBody, index = 8
	Name = farfield, index = 9
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
 7F48774EE700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F48774EE700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F48A5C26740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F48A5C26740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 9
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = nodeBody, index = 8
	Name = farfield, index = 9
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
 7F48A5C26740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F48A5C26740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F4876CED700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F4876CED700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 9
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = nodeBody, index = 8
	Name = farfield, index = 9
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
 7F48A5C26740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F48A5C26740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F48A5C26740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F48A5C26740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
ok
test_box (test_egadsTess.TestEGADS.test_box) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
ok
test_boxhole (test_egadsTess.TestEGADS.test_boxhole) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = boxhole, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
 7F48A5C26740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F48A5C26740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F48774EE700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F48774EE700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
ok
test_bullet (test_egadsTess.TestEGADS.test_bullet) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = bullet, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_cone (test_egadsTess.TestEGADS.test_cone) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cone, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_cylinder (test_egadsTess.TestEGADS.test_cylinder) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
ok
test_invalid_Mesh_Lenght_Scale (test_egadsTess.TestEGADS.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3
ok
test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1

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

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

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

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

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

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

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

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

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

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

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

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

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


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


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


Writing vtk file ....

Writing vtk surface file ....

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


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


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file

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

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

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


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


Writing Tecplot file ....
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


Writing vtk file ....

Writing vtk surface file ....

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


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


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file

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

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 7766
Number of elements = 15528
Number of triangle elements      = 15528
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5870
Number of elements = 11736
Number of triangle elements      = 11736
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 488
Number of elements = 972
Number of triangle elements      = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14124
Total number of elements = 28236
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 - 14124, elements - 28236
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.15
Creating surface mesh ...
Surface mesh seconds:  0.04
Recovering boundaries...
Boundary recovery seconds:  0.15
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.07
Recovering Delaunayness...
Delaunay recovery seconds:  0.07
Refining mesh...
  18827 insertions, added 13420 points, 721721 tetrahedra in queue.
  6269 insertions, added 2485 points, 625204 tetrahedra in queue.
  8356 insertions, added 2101 points, 168215 tetrahedra in queue.
Refinement seconds:  3.39
Smoothing vertices...
Mesh smoothing seconds:  3.32
Improving mesh...
Mesh improvement seconds:  0.08

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

Output seconds:  0.02
Total running seconds:  7.29

Statistics:

  Input points: 14124
  Input facets: 28236
  Input segments: 42354
  Input holes: 2
  Input regions: 0

  Mesh points: 33059
  Mesh tetrahedra: 159851
  Mesh faces: 333820
  Mesh faces on exterior boundary: 28236
  Mesh faces on input facets: 28236
  Mesh edges on input segments: 42354
  Steiner points inside domain: 18935

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    = 7766
Number of elements = 15528
Number of triangle elements      = 15528
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5870
Number of elements = 11736
Number of triangle elements      = 11736
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 488
Number of elements = 972
Number of triangle elements      = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14124
Total number of elements = 28236
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 - 14124, elements - 28236
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.14
Creating surface mesh ...
Surface mesh seconds:  0.04
Recovering boundaries...
Boundary recovery seconds:  0.14
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.06
Recovering Delaunayness...
Delaunay recovery seconds:  0.06
Refining mesh...
  18827 insertions, added 13420 points, 721721 tetrahedra in queue.
  6269 insertions, added 2485 points, 625204 tetrahedra in queue.
  8356 insertions, added 2101 points, 168215 tetrahedra in queue.
Refinement seconds:  3.13
Smoothing vertices...
Mesh smoothing seconds:  3.18
Improving mesh...
Mesh improvement seconds:  0.07

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

Output seconds:  0.02
Total running seconds:  6.84

Statistics:

  Input points: 14124
  Input facets: 28236
  Input segments: 42354
  Input holes: 2
  Input regions: 0

  Mesh points: 33059
  Mesh tetrahedra: 159851
  Mesh faces: 333820
  Mesh faces on exterior boundary: 28236
  Mesh faces on input facets: 28236
  Mesh edges on input segments: 42354
  Steiner points inside domain: 18935

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 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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)
	/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 - 5043, elements - 10074
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 - 5043, elements - 10074
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 - 14124, elements - 28236
Getting volume mesh

Generating volume mesh using TetGen.....

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

Writing MAPBC file ....
Finished writing MAPBC file

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

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

Writing MAPBC file ....
Finished writing MAPBC file

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

Writing MAPBC file ....
Finished writing MAPBC file

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

Writing MAPBC file ....
Finished writing MAPBC file

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

Writing MAPBC file ....
Finished writing MAPBC file

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
ok
test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable'
test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable'
test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable'
test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable'
test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable'
test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable'
test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable'
test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable'
test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable'
test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable'
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_Area_Mesh (test_refine.TestREFINE.test_Area_Mesh) ... skipped "No 'ref' executable"
test_all (test_refine.TestREFINE.test_all) ... skipped "No 'ref' executable"
test_box_volume (test_refine.TestREFINE.test_box_volume) ... skipped "No 'ref' executable"
test_boxhole (test_refine.TestREFINE.test_boxhole) ... skipped "No 'ref' executable"
test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... skipped "No 'ref' executable"
test_fun3d (test_refine.TestREFINE.test_fun3d) ... skipped "No 'ref' executable"
test_inputs (test_refine.TestREFINE.test_inputs) ... skipped "No 'ref' executable"
test_phase (test_refine.TestREFINE.test_phase) ... skipped "No 'ref' executable"
test_sphere (test_refine.TestREFINE.test_sphere) ... skipped "No 'ref' executable"
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
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         

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

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 3 Active Bodies

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

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

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

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

EGADS    : Face Edges Information

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

EGADS    : Face Loops Information

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

EGADS    : Loop Edges Information

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

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

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

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

EGADS    : Node Information

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

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

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

AFLR4    : Geometry Definition Information

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

AFLR4    : Case has 2 Proximity Checking Components

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

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
AFLR4    : Define CAD surface definition 17
AFLR4    : Define CAD surface definition 18
 
AFLR43   : INPUT SURFACE MESH FROM TESS
 
AFLR43   : Quad Surface Faces=         0
AFLR43   : Tria Surface Faces=     12428
AFLR43   : Nodes             =      6220
 
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR3    : ---------------------------------------
AFLR3    : AFLR3 LIBRARY
AFLR3    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3    : TETRAHEDRAL GRID GENERATOR
AFLR3    : Version Number 16.32.50
AFLR3    : Version Date   10/31/23 @ 06:31PM
AFLR3    : Compile OS     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR3    : Compile Date   03/08/24 @ 01:03AM
AFLR3    : Copyright 1994-2021, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =      6220         0

UG3      : Boundary Conditions

UG3      :  B-Face ID            Boundary Condition
UG3      :          1                         Solid
UG3      :          2                         Solid
UG3      :          3                         Solid
UG3      :          4                         Solid
UG3      :          5                         Solid
UG3      :          6                         Solid
UG3      :          7                         Solid
UG3      :          8                         Solid
UG3      :          9                         Solid
UG3      :         10                         Solid
UG3      :         11                         Solid
UG3      :         12                         Solid
UG3      :         13                         Solid
UG3      :         14                         Solid
UG3      :         15                         Solid
UG3      :         16                         Solid
UG3      :         17                      FarField
UG3      :         18                      FarField
 
AFLR3    : CPU Time          =     0.014   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =      6220         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =      1246      7333
AFLR3 IG : Nodes, Elements   =      2492     16261
AFLR3 IG : Nodes, Elements   =      3738     25021
AFLR3 IG : Nodes, Elements   =      4984     34304
AFLR3 IG : Nodes, Elements   =      6227     43518
AFLR3 IG : Nodes, Elements   =      6227     43440
AFLR3 IG : Nodes, Elements   =      6227     43475
AFLR3 IG : Nodes, Elements   =      6227     43439
AFLR3 IG : Nodes, Elements   =      6220     26110
AFLR3 IG : Nodes, Elements   =      6220     26133
AFLR3 IG : Nodes, Elements   =      6220     21488
AFLR3 IG : Nodes, Elements   =      6220     19195
 
AFLR3    : CPU Time          =     0.266   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =      6220     19195
AFLR3 GG : Nodes, Elements   =      9104     28052
AFLR3 GG : Nodes, Elements   =      9104     39102
AFLR3 GG : Nodes, Elements   =      9104     36335
AFLR3 GG : Nodes, Elements   =      9104     34880
AFLR3 GG : Nodes, Elements   =     11662     42890
AFLR3 GG : Nodes, Elements   =     11662     54004
AFLR3 GG : Nodes, Elements   =     11662     50843
AFLR3 GG : Nodes, Elements   =     11662     49925
AFLR3 GG : Nodes, Elements   =     14498     58736
AFLR3 GG : Nodes, Elements   =     14498     71038
AFLR3 GG : Nodes, Elements   =     14498     67638
AFLR3 GG : Nodes, Elements   =     14498     66762
AFLR3 GG : Nodes, Elements   =     17480     75922
AFLR3 GG : Nodes, Elements   =     17480     88720
AFLR3 GG : Nodes, Elements   =     17480     85188
AFLR3 GG : Nodes, Elements   =     17480     84349
AFLR3 GG : Nodes, Elements   =     20711     94213
AFLR3 GG : Nodes, Elements   =     20711    107855
AFLR3 GG : Nodes, Elements   =     20711    104214
AFLR3 GG : Nodes, Elements   =     20711    103375
AFLR3 GG : Nodes, Elements   =     24093    113678
AFLR3 GG : Nodes, Elements   =     24093    128254
AFLR3 GG : Nodes, Elements   =     24093    124257
AFLR3 GG : Nodes, Elements   =     24093    123406
AFLR3 GG : Nodes, Elements   =     27618    134141
AFLR3 GG : Nodes, Elements   =     27618    149080
AFLR3 GG : Nodes, Elements   =     27618    145168
AFLR3 GG : Nodes, Elements   =     27618    144374
AFLR3 GG : Nodes, Elements   =     31189    155227
AFLR3 GG : Nodes, Elements   =     31189    170286
AFLR3 GG : Nodes, Elements   =     31189    166309
AFLR3 GG : Nodes, Elements   =     31189    165453
AFLR3 GG : Nodes, Elements   =     34751    176284
AFLR3 GG : Nodes, Elements   =     34751    191463
AFLR3 GG : Nodes, Elements   =     34751    187411
AFLR3 GG : Nodes, Elements   =     34751    186588
AFLR3 GG : Nodes, Elements   =     38283    197293
AFLR3 GG : Nodes, Elements   =     38283    212453
AFLR3 GG : Nodes, Elements   =     38283    208438
AFLR3 GG : Nodes, Elements   =     38283    207716
AFLR3 GG : Nodes, Elements   =     41833    218438
AFLR3 GG : Nodes, Elements   =     41833    233399
AFLR3 GG : Nodes, Elements   =     41833    229556
AFLR3 GG : Nodes, Elements   =     41833    228802
AFLR3 GG : Nodes, Elements   =     45233    239061
AFLR3 GG : Nodes, Elements   =     45233    253453
AFLR3 GG : Nodes, Elements   =     45233    249686
AFLR3 GG : Nodes, Elements   =     45233    248980
AFLR3 GG : Nodes, Elements   =     48547    258960
AFLR3 GG : Nodes, Elements   =     48547    273037
AFLR3 GG : Nodes, Elements   =     48547    269340
AFLR3 GG : Nodes, Elements   =     48547    268660
AFLR3 GG : Nodes, Elements   =     51788    278411
AFLR3 GG : Nodes, Elements   =     51788    292195
AFLR3 GG : Nodes, Elements   =     51788    288655
AFLR3 GG : Nodes, Elements   =     51788    288020
AFLR3 GG : Nodes, Elements   =     54897    297367
AFLR3 GG : Nodes, Elements   =     54897    310536
AFLR3 GG : Nodes, Elements   =     54897    307175
AFLR3 GG : Nodes, Elements   =     54897    306599
AFLR3 GG : Nodes, Elements   =     57861    315502
AFLR3 GG : Nodes, Elements   =     57861    327967
AFLR3 GG : Nodes, Elements   =     57861    324838
AFLR3 GG : Nodes, Elements   =     57861    324290
AFLR3 GG : Nodes, Elements   =     60791    333083
AFLR3 GG : Nodes, Elements   =     60791    345364
AFLR3 GG : Nodes, Elements   =     60791    342206
AFLR3 GG : Nodes, Elements   =     60791    341750
AFLR3 GG : Nodes, Elements   =     63489    349850
AFLR3 GG : Nodes, Elements   =     63489    361174
AFLR3 GG : Nodes, Elements   =     63489    358324
AFLR3 GG : Nodes, Elements   =     63489    357881
AFLR3 GG : Nodes, Elements   =     65986    365375
AFLR3 GG : Nodes, Elements   =     65986    375877
AFLR3 GG : Nodes, Elements   =     65986    373150
AFLR3 GG : Nodes, Elements   =     65986    372801
AFLR3 GG : Nodes, Elements   =     68262    379634
AFLR3 GG : Nodes, Elements   =     68262    389039
AFLR3 GG : Nodes, Elements   =     68262    386682
AFLR3 GG : Nodes, Elements   =     68262    386428
AFLR3 GG : Nodes, Elements   =     70242    392370
AFLR3 GG : Nodes, Elements   =     70242    400574
AFLR3 GG : Nodes, Elements   =     70242    398524
AFLR3 GG : Nodes, Elements   =     70242    398290
AFLR3 GG : Nodes, Elements   =     71834    403067
AFLR3 GG : Nodes, Elements   =     71834    409901
AFLR3 GG : Nodes, Elements   =     71834    408035
AFLR3 GG : Nodes, Elements   =     71834    407840
AFLR3 GG : Nodes, Elements   =     73096    411631
AFLR3 GG : Nodes, Elements   =     73096    416942
AFLR3 GG : Nodes, Elements   =     73096    415543
AFLR3 GG : Nodes, Elements   =     73096    415387
AFLR3 GG : Nodes, Elements   =     74042    418225
AFLR3 GG : Nodes, Elements   =     74042    422196
AFLR3 GG : Nodes, Elements   =     74042    421120
AFLR3 GG : Nodes, Elements   =     74042    421030
AFLR3 GG : Nodes, Elements   =     74697    422995
AFLR3 GG : Nodes, Elements   =     74697    425691
AFLR3 GG : Nodes, Elements   =     74697    424979
AFLR3 GG : Nodes, Elements   =     74697    424921
AFLR3 GG : Nodes, Elements   =     75147    426271
AFLR3 GG : Nodes, Elements   =     75147    428179
AFLR3 GG : Nodes, Elements   =     75147    427658
AFLR3 GG : Nodes, Elements   =     75147    427613
AFLR3 GG : Nodes, Elements   =     75442    428499
AFLR3 GG : Nodes, Elements   =     75442    429739
AFLR3 GG : Nodes, Elements   =     75442    429380
AFLR3 GG : Nodes, Elements   =     75442    429354
AFLR3 GG : Nodes, Elements   =     75634    429930
AFLR3 GG : Nodes, Elements   =     75634    430753
AFLR3 GG : Nodes, Elements   =     75634    430521
AFLR3 GG : Nodes, Elements   =     75634    430497
AFLR3 GG : Nodes, Elements   =     75743    430824
AFLR3 GG : Nodes, Elements   =     75743    431284
AFLR3 GG : Nodes, Elements   =     75743    431147
AFLR3 GG : Nodes, Elements   =     75743    431140
AFLR3 GG : Nodes, Elements   =     75813    431351
AFLR3 GG : Nodes, Elements   =     75813    431632
AFLR3 GG : Nodes, Elements   =     75813    431554
AFLR3 GG : Nodes, Elements   =     75813    431549
AFLR3 GG : Nodes, Elements   =     75854    431672
AFLR3 GG : Nodes, Elements   =     75854    431830
AFLR3 GG : Nodes, Elements   =     75854    431793
AFLR3 GG : Nodes, Elements   =     75854    431785
AFLR3 GG : Nodes, Elements   =     75878    431857
AFLR3 GG : Nodes, Elements   =     75878    431960
AFLR3 GG : Nodes, Elements   =     75878    431923
AFLR3 GG : Nodes, Elements   =     75878    431919
AFLR3 GG : Nodes, Elements   =     75896    431973
AFLR3 GG : Nodes, Elements   =     75896    432050
AFLR3 GG : Nodes, Elements   =     75896    432029
AFLR3 GG : Nodes, Elements   =     75896    432027
AFLR3 GG : Nodes, Elements   =     75911    432072
AFLR3 GG : Nodes, Elements   =     75911    432140
AFLR3 GG : Nodes, Elements   =     75911    432115
AFLR3 GG : Nodes, Elements   =     75911    432113
AFLR3 GG : Nodes, Elements   =     75917    432131
AFLR3 GG : Nodes, Elements   =     75917    432161
AFLR3 GG : Nodes, Elements   =     75917    432148
AFLR3 GG : Nodes, Elements   =     75917    432146
AFLR3 GG : Nodes, Elements   =     75922    432161
AFLR3 GG : Nodes, Elements   =     75922    432186
AFLR3 GG : Nodes, Elements   =     75922    432175
AFLR3 GG : Nodes, Elements   =     75925    432184
AFLR3 GG : Nodes, Elements   =     75925    432192
AFLR3 GG : Nodes, Elements   =     75925    432191
AFLR3 GG : Nodes, Elements   =     75927    432197
AFLR3 GG : Nodes, Elements   =     75927    432207
AFLR3 GG : Nodes, Elements   =     75927    432204
AFLR3 GG : Nodes, Elements   =     75929    432210
AFLR3 GG : Nodes, Elements   =     75929    432216
AFLR3 GG : Nodes, Elements   =     75929    432215
AFLR3 GG : Nodes, Elements   =     75932    432224
AFLR3 GG : Nodes, Elements   =     75932    432240
AFLR3 GG : Nodes, Elements   =     75932    432234
AFLR3 GG : Nodes, Elements   =     75932    432233
AFLR3 GG : Nodes, Elements   =     75933    432236
AFLR3 GG : Nodes, Elements   =     75933    432244
AFLR3 GG : Nodes, Elements   =     75933    432241
AFLR3 GG : Nodes, Elements   =     75933    432240
AFLR3 GG : Nodes, Elements   =     75962    432327
AFLR3 GG : Nodes, Elements   =     75962    432440
AFLR3 GG : Nodes, Elements   =     75962    432401
AFLR3 GG : Nodes, Elements   =     75962    432400
AFLR3 GG : Nodes, Elements   =     75964    432406
AFLR3 GG : Nodes, Elements   =     75964    432411
AFLR3 GG : Nodes, Elements   =     75964    432408
 
AFLR3    : CPU Time          =     6.841   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =     75964    432408
AFLR3 QI : Nodes, Elements   =     74464    423905
AFLR3 QI : Nodes, Elements   =     74236    422620
AFLR3 QI : Nodes, Elements   =     74218    422515
AFLR3 QI : Nodes, Elements   =     74218    426676
AFLR3 QI : Nodes, Elements   =     74218    422354
AFLR3 QI : Nodes, Elements   =     74218    421937
AFLR3 QI : Nodes, Elements   =     74218    422317
AFLR3 QI : Nodes, Elements   =     74218    421673
AFLR3 QI : Nodes, Elements   =     74218    421449
AFLR3 QI : Nodes, Elements   =     74218    421720
AFLR3 QI : Nodes, Elements   =     74218    421413
AFLR3 QI : Nodes, Elements   =     74218    421313
AFLR3 QI : Nodes, Elements   =     74218    421535
AFLR3 QI : Nodes, Elements   =     74218    421304
AFLR3 QI : Nodes, Elements   =     74218    421266
AFLR3 QI : Nodes, Elements   =     74218    421471
AFLR3 QI : Nodes, Elements   =     74218    421263
AFLR3 QI : Nodes, Elements   =     74218    421232
AFLR3 QI : Nodes, Elements   =     74223    421255
AFLR3 QI : Nodes, Elements   =     74223    421470
AFLR3 QI : Nodes, Elements   =     74223    421272
AFLR3 QI : Nodes, Elements   =     74223    421260
AFLR3 QI : Nodes, Elements   =     74223    421451
AFLR3 QI : Nodes, Elements   =     74223    421266
AFLR3 QI : Nodes, Elements   =     74223    421234
 
AFLR3    : CPU Time          =     1.870   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =     74223    421234
AFLR3 QRG: Nodes, Elements   =     74223    421233
AFLR3 QRG: Nodes, Elements   =     74223    421232
AFLR3 QRG: Nodes, Elements   =     74225    421243
AFLR3 QRG: Nodes, Elements   =     74230    421269
AFLR3 QRG: Nodes, Elements   =     74239    421316
 
AFLR3    : CPU Time          =     0.135   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    421316
UG3      : Min, Max Ang      =     1.064     171.4
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        62
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.12e+06

UG3      : No. Tet Elems     =    421316
UG3      : Min Vol           =  6.77e-10
UG3      : Average Vol       =      5.04
UG3      : Total-Tet-Vol     =  2.12e+06
UG3      : No. Vol<TOL       =         0

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

UG3      : No. Tet Elems     =    421316
UG3      : Min, Max Q        =    0.0787         1
UG3      : Average Q         =     0.894
UG3      : No. Q<       0.1  =        24
UG3      : No. Q<      0.01  =         0

OVERALL  : CPU Time          =     9.591   seconds

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    421316
UG3      : Min, Max Ang      =     1.064     171.4
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        62
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.12e+06

UG3      : No. Tet Elems     =    421316
UG3      : Min Vol           =  6.77e-10
UG3      : Average Vol       =      5.04
UG3      : Total-Tet-Vol     =  2.12e+06
UG3      : No. Vol<TOL       =         0

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

UG3      : No. Tet Elems     =    421316
UG3      : Min, Max Q        =     0.188         1
UG3      : Average Q         =     0.854
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          = 74239
	Number of elements       = 433744
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 421316
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Cardinal"
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Raven"
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Falcon"
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... Getting CFD boundary conditions
	Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - X
ok
test_journal (test_su2.TestSU2.test_journal) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 74239
	Number of elements       = 433744
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 421316
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 1
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 2
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 2
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 74239
	Number of elements       = 433744
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 421316
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
 CAPS Info: Hit last success -- going live!
Running SU2 1
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 2
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
 CAPS Info: Hit last success -- going live!
Running SU2 2
 CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
ok
test_phase (test_su2.TestSU2.test_phase) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh

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

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.25
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------
Volume mesh:
	Number of nodes          = 74239
	Number of elements       = 433744
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 421316
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_reenter (test_su2.TestSU2.test_reenter) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 2
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_units (test_su2.TestSU2.test_units) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
ok
test_PlateSensFile (test_tacs.TestTACS.test_PlateSensFile) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of triangle elements      = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes    = 25
Total number of elements = 16
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
	Face 1 TFI quading disabled with attribute .qParams
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 25
Number of elements = 16
Number of triangle elements      = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes    = 25
Total number of elements = 16
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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

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

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

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

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

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

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

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

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 2
	Design_Variable name - plateLength
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Projecting tessellation 1 (of 1) on to new body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - plateWidth
	Number of design variable relations - 0
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = plateEdge, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 1
	Name = plate, index = 1
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
	Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
	Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 25
	Number of elements = 16
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 16

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Getting FEA design variables.......
	Number of design variables          - 1
	Design_Variable name - thick1
	Design_Variable_Relation name - thick1
	Number of design variable relations - 1
	Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Writing subElement types (if any) - appending mesh file

Writing TACS instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint ADD cards
	Writing load cards
	Writing constraint cards
	Writing material cards
	Writing property cards
	Writing design variable cards
	Writing design variable relation cards
ok
test_Multiple_Mesh (test_tetgen.TestTETGEN.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Getting surface mesh for body 1 (of 7)
Getting surface mesh for body 2 (of 7)
Getting surface mesh for body 3 (of 7)
Getting surface mesh for body 4 (of 7)
Getting surface mesh for body 5 (of 7)
Getting surface mesh for body 6 (of 7)
 7F48A5C26740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F48A5C26740 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F48764EC700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F48764EC700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Getting surface mesh for body 7 (of 7)
Body 1 (of 7)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 2 (of 7)
Number of nodes    = 296
Number of elements = 588
Number of triangle elements      = 588
Number of quadrilateral elements = 0
Body 3 (of 7)
Number of nodes    = 487
Number of elements = 970
Number of triangle elements      = 970
Number of quadrilateral elements = 0
Body 4 (of 7)
Number of nodes    = 2048
Number of elements = 4096
Number of triangle elements      = 4096
Number of quadrilateral elements = 0
Body 5 (of 7)
Number of nodes    = 152
Number of elements = 300
Number of triangle elements      = 300
Number of quadrilateral elements = 0
Body 6 (of 7)
Number of nodes    = 624
Number of elements = 1248
Number of triangle elements      = 1248
Number of quadrilateral elements = 0
Body 7 (of 7)
Number of nodes    = 488
Number of elements = 972
Number of triangle elements      = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4193
Total number of elements = 8366
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 - 296, elements - 588
Body 3 number of surface: nodes - 487, elements - 970
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cylinder, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cone, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = torus, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = sphere, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = boxhole, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = bullet, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 296, elements - 588
Body 3 number of surface: nodes - 487, elements - 970
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Number of surface: nodes - 4193, elements - 8366
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 374
Number of elements = 744
Number of triangle elements      = 744
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 472
Total number of elements = 936
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 386
Number of elements = 768
Number of triangle elements      = 768
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 582
Total number of elements = 1152
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 351
Number of elements = 698
Number of triangle elements      = 698
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 491
Total number of elements = 970
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 376
Number of elements = 748
Number of triangle elements      = 748
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 98
Number of elements = 192
Number of triangle elements      = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 516
Total number of elements = 1020
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 370
Number of elements = 736
Number of triangle elements      = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 42
Number of elements = 80
Number of triangle elements      = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 454
Total number of elements = 896
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 370
Number of elements = 736
Number of triangle elements      = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 126
Number of elements = 252
Number of triangle elements      = 252
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 20
Number of elements = 36
Number of triangle elements      = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 516
Total number of elements = 1024
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 109
Number of elements = 214
Number of triangle elements      = 214
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 48
Number of elements = 96
Number of triangle elements      = 96
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 12
Number of elements = 20
Number of triangle elements      = 20
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 169
Total number of elements = 330
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 536
Number of elements = 1072
Number of triangle elements      = 1072
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 544
Number of elements = 1084
Number of triangle elements      = 1084
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1080
Total number of elements = 2156
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 5)
Getting surface mesh for body 2 (of 5)
Getting surface mesh for body 3 (of 5)
Getting surface mesh for body 4 (of 5)
Getting surface mesh for body 5 (of 5)
Body 1 (of 5)
Number of nodes    = 1352
Number of elements = 2684
Number of triangle elements      = 2684
Number of quadrilateral elements = 0
Body 2 (of 5)
Number of nodes    = 288
Number of elements = 572
Number of triangle elements      = 572
Number of quadrilateral elements = 0
Body 3 (of 5)
Number of nodes    = 173
Number of elements = 342
Number of triangle elements      = 342
Number of quadrilateral elements = 0
Body 4 (of 5)
Number of nodes    = 26
Number of elements = 48
Number of triangle elements      = 48
Number of quadrilateral elements = 0
Body 5 (of 5)
Number of nodes    = 482
Number of elements = 960
Number of triangle elements      = 960
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 2321
Total number of elements = 4606
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1352, elements - 2684
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 173, elements - 342
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1352, elements - 2684
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 173, elements - 342
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 440
Number of elements = 876
Number of triangle elements      = 876
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 522
Number of elements = 1044
Number of triangle elements      = 1044
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 962
Total number of elements = 1920
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 440, elements - 876
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 440, elements - 876
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_journal (test_tetgen.TestTETGEN.test_journal) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
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 - 9626, elements - 19244
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 - 9626, elements - 19244
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 - 9626, elements - 19244
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 - 9626, elements - 19244
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 7130, elements - 14252
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_reenter (test_tetgen.TestTETGEN.test_reenter) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Farfield, index = 1
	Name = Wing1, index = 2
	Name = trailingEdge, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 9626
Number of elements = 19244
Number of triangle elements      = 19244
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9626
Total number of elements = 19244
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!

Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary STL file ....
Finished writing Binary STL file


Writing Tecplot file ....
Finished writing Tecplot file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing Binary VTK file ....
Finished writing Binary VTK file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!

Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary STL file ....
Finished writing Binary STL file


Writing Tecplot file ....
Finished writing Tecplot file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing Binary VTK file ....
Finished writing Binary VTK file


Writing FAST file ....
Finished writing FAST file


Writing SU2 file ....
Finished writing SU2 file

ok
test_setInput (test_tetgen.TestTETGEN.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment) ... ok
test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment) ... ok
test_Cl (test_xfoil.Testxfoil_NACA.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment) ... ok
test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement) ... ok
test_append (test_xfoil.Testxfoil_NACA.test_append) ... ok
test_normalize (test_xfoil.Testxfoil_NACA.test_normalize) ... ok
test_phase (test_xfoil.Testxfoil_NACA.test_phase) ... ok
test_Output (test_zaero.TestZAERO.test_Output) ... ok
test_inputs (test_zaero.TestZAERO.test_inputs) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 1220
Number of elements = 2680
Number of triangle elements      = 2680
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1221
Total number of elements = 2680
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1220
	Number of elements = 2680
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 2680
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 1221
	Combined Number of elements = 2681
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 2680
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 6
	Property name - Rib_Root
	Property name - Rib_Root_Point
	Property name - Ribs
	Property name - Skin
	Property name - Spar1
	Property name - Spar2
	Done getting FEA properties
Updating mesh element types based on properties input

'Smart_Restart' is ON
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data
Getting vortex lattice control surface data
	VLM control surface name - CntrlLE
	VLM control surface name - CntrlTE
	Done getting vortex lattice control surface data

Getting FEA vortex lattice mesh

Getting ZAERO UAIC Configurations.......
	Number of UAIC Configurations - 2

	UAIC Configuration: climb, id = 1
	- Mach Number : 0.200000
	- Reduced Freq: [0.020000, ... , 0.250000]

	UAIC Configuration: cruise, id = 2
	- Mach Number : 0.700000
	- Reduced Freq: [0.040000, ... , 0.350000]

Getting ZAERO Analysis Subcases.......
	Number of Analysis Subcases - 2

	Analysis Subcase: FlutterCruise, id = 1
	- Discipline : flutter
	- UAIC       : cruise

	Analysis Subcase: Trim, id = 2
	- Discipline : Trim
	- UAIC       : climb

Getting ZAERO Trim Variables.......
	Number of Trim Variables - 2

	Trim Variable: ANGLEA
	- Label : ALPHA
	- Value : free

	Trim Variable: URDD3
	- Label : NZ
	- Value : 1.0

	Updating StaticAeroelastic subcase: Trim
	- vectorToCG -> [0.345898, 1.652951, -0.041403]
	- weight -> 476456.149985
	- weightMomentOfInertia -> [304902.643270, 98963.803820, 69822.813292, 6179.981375, 19723.152207, 370546.335524]
ok

----------------------------------------------------------------------
Ran 143 tests in 533.923s

OK (skipped=26)
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/
+ make test TYPE=MINIMAL
(make -C cCAPS -f aeroelastic_SU2.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `avlTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `awaveTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `frictionTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: Nothing to be done for `fun3d'.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f hsm.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `hsm' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `interferenceTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `msesTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f mystran.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `mystranTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `pointwiseTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(cd ./regressionTest; ./execute_CTestRegression.sh MINIMAL)
Running.... MINIMAL c-Tests

All tests pass!

(cd ./regressionTest; ./execute_PyTestRegression.sh MINIMAL)

=================================================
Using python : /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python
=================================================

Running.... MINIMAL PyTests

=================================================
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ echo 'avl_PyTest.py test;'
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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   0.0006119078685746836
CYtot   -6.288067668554914e-15
CZtot   -0.3012861394886091
Cltot   -4.782099331324466e-14
Cmtot   -0.1945055953450467
Cntot   -2.339543963831951e-15
Cl'tot  -4.785454061647156e-14
Cn'tot  -1.504596228417061e-15
CLtot   0.3012509314150772
CDtot   0.004646353488232841
CDvis   0.0
CLff    0.3009503023520527
CYff    -7.718708857566269e-15
CDind   0.004646353488232841
CDff    0.004968969500908292
e       0.9669902146157957
StripForces 
Wing  cl =  [0.02994790451347, 0.08555545178934, 0.1329003532588, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.310122128419, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805665, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996428, 0.2453427152623, 0.2100182422922, 0.1733025192801, 0.1329003532723, 0.08555545180788, 0.0299479045408]
Wing  cd =  [-0.004234137763162, -0.004494543653191, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946402, 0.0005114598078397, 0.0021191472861, 0.004145189908974, 0.006609094404182, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.00660909440444, 0.004145189909261, 0.002119147286385, 0.0005114598080999, -0.000738653894407, -0.001762021024095, -0.002739626801367, -0.003752887372445, -0.004494543653161, -0.004234137764545]

real	0m0.653s
user	0m0.502s
sys	0m0.356s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  [1.05475230552567, 1.36488869373635, 1.56607214272105, 2.03059709344862, 1.97271083121169, 1.87307153172386, 1.76050475760117]
Cd =  [0.0131991208675727, 0.0166540240605751, 0.0200551482562831, 0.0458671341969345, 0.0754256009394856, 0.0994469174477522, 0.127479430989037]
Alpha =  [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location =  [0.4960441144043, 0.461377732041502, 0.44237656820185, 0.361251636355465, 0.276104140853559, 0.214381239321467, 0.132988264746661]

real	0m5.667s
user	0m4.875s
sys	0m0.231s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  0.37837910855492407
Cd =  0.007775858417210143
Cm =  0.005262636995811319

real	0m5.173s
user	0m4.799s
sys	0m0.243s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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	0m0.500s
user	0m0.354s
sys	0m0.255s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'tsfoil_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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 =  0.933329
Cd =  0.000283
Cd Wave =  0.0
Cm =  -0.203433
Cp _Critcal =  -1.303869

real	0m0.496s
user	0m0.427s
sys	0m0.245s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================


=================================================
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ echo 'delaundo_PyTest.py test;'
delaundo_PyTest.py test;
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u delaundo_PyTest.py -outLevel=0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6

Getting mesh sizing parameters
	Mesh sizing name - Airfoil
	Mesh sizing name - AirfoilTE
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting edge discretization for body 1
	Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
	Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
	Writing out *.pts file
Reading delaundo mesh file - delaundo_CAPS.mesh
	Swapping y and z coordinates!

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file


Writing ugrid file ....
Finished writing ugrid file


real	0m0.554s
user	0m0.478s
sys	0m0.309s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'egadsTess_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
	Name = Wing, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2

Getting mesh sizing parameters
	Mesh sizing name - LeadingEdge
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes    = 3793
Number of elements = 4001
Number of triangle elements      = 0
Number of quadrilateral elements = 4001
Body 2 (of 4)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes    = 76
Number of elements = 55
Number of triangle elements      = 0
Number of quadrilateral elements = 55
Body 4 (of 4)
Number of nodes    = 100
Number of elements = 73
Number of triangle elements      = 0
Number of quadrilateral elements = 73
----------------------------
Total number of nodes    = 3970
Total number of elements = 4129

Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing ugrid file ....
Finished writing ugrid file


real	0m7.323s
user	0m12.890s
sys	0m0.702s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr2_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2    : Compile Date   04/23/24 @ 12:17PM
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          =     0.023   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          =     0.010   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 6031
Number of elements = 6448
Number of tris = 488
Number of quad = 5616
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file


real	0m0.770s
user	0m0.652s
sys	0m0.287s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'aflr4_and_aflr3_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing ugrid file ....
Finished writing ugrid file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4

Getting mesh sizing parameters
	Mesh sizing name - Wing1
	Mesh sizing name - Wing2
	Done getting mesh sizing parameters
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2    : Compile Date   04/23/24 @ 12:17PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR4    : Compile Date   04/23/24 @ 12:17PM
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          = 151604
	Number of elements       = 458324
	Number of triangles      = 14380
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 222892
	Number of pyramids       = 425
	Number of prisms         = 220627
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


real	0m17.389s
user	0m16.169s
sys	0m0.404s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 2236
Number of elements = 4468
Number of triangle elements      = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 636
Number of elements = 1268
Number of triangle elements      = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 267
Number of elements = 530
Number of triangle elements      = 530
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 3139
Total number of elements = 6266

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 3139, elements - 6266
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.02
Creating surface mesh ...
Surface mesh seconds:  0.01
Recovering boundaries...
Boundary recovery seconds:  0.05
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0
Suppressing Steiner points ...
Steiner suppression seconds:  0
Recovering Delaunayness...
Delaunay recovery seconds:  0.01
Refining mesh...
  4190 insertions, added 2180 points, 134280 tetrahedra in queue.
  1395 insertions, added 459 points, 138994 tetrahedra in queue.
  1859 insertions, added 487 points, 137112 tetrahedra in queue.
  2478 insertions, added 498 points, 120303 tetrahedra in queue.
  3304 insertions, added 499 points, 74342 tetrahedra in queue.
  4404 insertions, added 474 points, 460 tetrahedra in queue.
Refinement seconds:  0.64
Smoothing vertices...
Mesh smoothing seconds:  0.44
Improving mesh...
Mesh improvement seconds:  0.01
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0
Total running seconds:  1.18

Statistics:

  Input points: 3139
  Input facets: 6266
  Input segments: 9399
  Input holes: 2
  Input regions: 0

  Mesh points: 8309
  Mesh tetrahedra: 41161
  Mesh faces: 85455
  Mesh faces on exterior boundary: 6266
  Mesh faces on input facets: 6266
  Mesh edges on input segments: 9399
  Steiner points inside domain: 5170

Done meshing using TetGen!

Writing Tecplot file ....
Finished writing Tecplot file


real	0m2.646s
user	0m2.766s
sys	0m0.329s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Saving geometry
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2    : Compile Date   04/23/24 @ 12:17PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       545         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       545       545
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       110       222
AFLR2 IG : Nodes, Faces      =       220       442
AFLR2 IG : Nodes, Faces      =       330       662
AFLR2 IG : Nodes, Faces      =       440       882
AFLR2 IG : Nodes, Faces      =       517      1036
AFLR2 IG : Nodes, Faces      =       545      1092
AFLR2 IG : Nodes, Faces      =       549      1092
AFLR2 IG : Nodes, Faces      =       545       545
 
AFLR2    : CPU Time          =     0.002   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       545       545
AFLR2 GGp: Nodes, Faces      =      1083      1621
AFLR2 GGp: Nodes, Faces      =      1616      2687
AFLR2 GGp: Nodes, Faces      =      2144      3743
AFLR2 GGp: Nodes, Faces      =      2661      4777
AFLR2 GGp: Nodes, Faces      =      3171      5797
AFLR2 GGp: Nodes, Faces      =      3672      6799
AFLR2 GGp: Nodes, Faces      =      4158      7771
AFLR2 GGp: Nodes, Faces      =      4653      8761
AFLR2 GGp: Nodes, Faces      =      5142      9739
AFLR2 GGp: Nodes, Faces      =      5608     10671
AFLR2 GGp: Nodes, Faces      =      6055     11565
AFLR2 GGp: Nodes, Faces      =      6482     12419
AFLR2 GGp: Nodes, Faces      =      6880     13215
AFLR2 GGp: Nodes, Faces      =      7257     13969
AFLR2 GGp: Nodes, Faces      =      7614     14683
AFLR2 GGp: Nodes, Faces      =      7947     15349
AFLR2 GGp: Nodes, Faces      =      8276     16007
AFLR2 GGp: Nodes, Faces      =      8575     16605
AFLR2 GGp: Nodes, Faces      =      8869     17193
AFLR2 GGp: Nodes, Faces      =      9140     17735
AFLR2 GGp: Nodes, Faces      =      9401     18257
AFLR2 GGp: Nodes, Faces      =      9654     18763
AFLR2 GGp: Nodes, Faces      =      9887     19229
AFLR2 GGp: Nodes, Faces      =     10110     19675
AFLR2 GGp: Nodes, Faces      =     10315     20085
AFLR2 GGp: Nodes, Faces      =     10497     20449
AFLR2 GGp: Nodes, Faces      =     10656     20767
AFLR2 GGp: Nodes, Faces      =     10791     21037
AFLR2 GGp: Nodes, Faces      =     10919     21293
AFLR2 GGp: Nodes, Faces      =     11022     21499
AFLR2 GGp: Nodes, Faces      =     11092     21639
AFLR2 GGp: Nodes, Faces      =     11145     21745
AFLR2 GGp: Nodes, Faces      =     11156     21767
 
AFLR2    : CPU Time          =     0.044   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          =     0.019   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 11153
Number of elements = 11885
Number of tris = 917
Number of quad = 10423
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!

Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file


Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Airfoil
	Boundary condition name - InFlow
	Boundary condition name - OutFlow
	Boundary condition name - TunnelWall
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.

Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../aflr2/aflr2_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_su2_aflr2.
Volume file name: flow_pyCAPS_su2_aflr2.
Restart file name: restart_flow_pyCAPS_su2_aflr2.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_5|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                     Inlet boundary|                               BC_4|
+-----------------------------------------------------------------------+
|                    Outlet boundary|                               BC_3|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
11153 grid points.
11340 volume elements.
4 surface markers.
98 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_4).
399 boundary elements in index 3 (Marker = BC_5).
917 triangles.
10423 quadrilaterals.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 917 TRIANGLE volume elements.
There has been a re-orientation of 10423 QUADRILATERAL volume elements.
There has been a re-orientation of 73 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.878.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        49.3184|             90|
|     CV Face Area Aspect Ratio|        1.00035|        33.4982|
|           CV Sub-Volume Ratio|        1.00001|        7.89914|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11153|    1/1.00|        10|
|         1|      2702|    1/4.13|   7.38309|
|         2|       549|    1/4.92|   4.99198|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06265 m.
Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m.
Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is NOT a single straight.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        216054|             1|   m^2/s^2|        216054|
|            Velocity-X|       136.119|             1|       m/s|       136.119|
|            Velocity-Y|             0|             1|       m/s|             0|
|    Velocity Magnitude|       136.119|             1|       m/s|       136.119|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.3958e-01|    0.071067|    2.739763|    1.616077|    5.599701|    0.055267|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.2675e-01|   -0.447576|    2.193837|    1.571349|    5.070382|    0.046028|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.1852e-01|   -0.561159|    2.074597|    1.490746|    4.953698|    0.033910|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.2335e-01|   -0.723326|    1.921155|    1.390756|    4.790278|    0.049695|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.1949e-01|   -0.876572|    1.825653|    1.275093|    4.637161|    0.133976|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.1694e-01|   -1.029177|    1.759196|    1.156078|    4.482282|    0.368542|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.1496e-01|   -1.215334|    1.704909|    1.114966|    4.286060|    0.974759|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.1349e-01|   -1.329970|    1.644937|    1.145030|    4.116982|    2.716332|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.1243e-01|   -1.270672|    1.570739|    1.155400|    4.139480|   16.569216|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.1151e-01|   -1.221243|    1.499646|    1.130319|    4.189559|   -6.277653|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.22124|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_su2_aflr2.dat  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|CSV file                           |surface_flow_pyCAPS_su2_aflr2.csv  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary                     |flow_pyCAPS_su2_aflr2.szplt        |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary surface             |surface_flow_pyCAPS_su2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 994 more values.0: Error finishing Tecplot file output.

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

Total Force - Pressure + Viscous
Cl =  0.072253 Cd =  -0.01151
Cmz =  0.070975
Cx =  -0.01151 Cy =  0.072253
Pressure Contribution
Cl_p =  0.072253 Cd_p =  -0.01151
Cmz_p =  0.070975
Cx_p =  -0.01151 Cy_p =  0.072253
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0

real	0m2.304s
user	0m2.128s
sys	0m0.391s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results mass properties.....

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 1159
Number of elements = 798
Number of triangle elements      = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes    = 1159
Total number of elements = 798
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Constraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1159
	Number of elements = 798
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 798

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - Ribs_and_Spars
	No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input
Area      3.428666259747
Mass      5383.006027803
Centroid  [1.222256036874, 0.1634981473778, -4.234505810751e-11]
CG        [1.222256036874, 0.1634981473778, -4.234637807833e-11]
Ixx       22133.97306033
Iyy       23448.30046709
Izz       1389.213122582
Ixy       164.2055275657
Ixz       -7.45484669011e-06
Iyz       1.707686795832e-06
I         [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.45484669011e-06, 1.707686795832e-06]
II        [[22133.97306033, -164.2055275657, 7.45484669011e-06], [-164.2055275657, 23448.30046709, -1.707686795832e-06], [7.45484669011e-06, -1.707686795832e-06, 1389.213122582]]

real	0m4.508s
user	0m6.264s
sys	0m0.936s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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	0m1.765s
user	0m1.644s
sys	0m0.235s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo '../corsairlite/qp.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
../corsairlite/qp.py test;
+ python -u ../corsairlite/qp.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/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	0m2.611s
user	0m2.524s
sys	0m0.436s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case ../corsairlite/qp.py passed (as expected)
=================================================


*************************************************
*************************************************

=================================================
Did not run examples for:

abaqus
awave
Cart3D
Astros
Mystran
=================================================

All tests pass!

+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64
+ mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/test/plugs
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/test/plugs
+ find /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/Plugs -name 'plugs0*.csm'
+ sort -f
find: ‘/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/Plugs’: No such file or directory
+ awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/data/plugs/plugsFailure.txt
+ cp /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/data/plugs/plugsIgnore.txt .
+ set +x
Testing CSM files:
total 28M
-rw-rw-r--. 1 jenkins jenkins 1.3M Apr 28 10:21 ASTRO.D01
-rw-rw-r--. 1 jenkins jenkins 316K Apr 28 10:21 ASTRO.IDX
-rwxrwxr-x. 1 jenkins jenkins 1.1M Apr 28 10:21 avl
-rwxrwxr-x. 1 jenkins jenkins  29K Apr 28 10:20 egads2cart
-rwxrwxr-x. 1 jenkins jenkins 114K Apr 28 10:22 egads2cgt
-rwxrwxr-x. 1 jenkins jenkins  46K Apr 28 10:21 friction
-rwxrwxr-x. 1 jenkins jenkins 8.2M Apr 28 10:21 mastros.exe
-rwxrwxr-x. 1 jenkins jenkins 727K Apr 28 10:21 mses
-rwxrwxr-x. 1 jenkins jenkins 536K Apr 28 10:21 mset
-rwxrwxr-x. 1 jenkins jenkins  39K Apr 28 10:21 phaseUtil
-rw-rw-r--. 1 jenkins jenkins 1.6K Apr 28 10:24 pod.egads
-rw-rw-r--. 1 jenkins jenkins    0 Apr 28 10:24 port7681.jrnl
-rwxrwxr-x. 1 jenkins jenkins 451K Apr 28 10:21 pplot
-rwxrwxr-x. 1 jenkins jenkins 405K Apr 28 10:21 pxplot
-rwxrwxr-x. 1 jenkins jenkins 115K Apr 28 10:20 sensCSM
-rwxrwxr-x. 1 jenkins jenkins 507K Apr 28 10:20 serveCSM
-rwxrwxr-x. 1 jenkins jenkins 443K Apr 28 10:20 serveESP
-rwxrwxr-x. 1 jenkins jenkins 568K Apr 28 10:21 Slugs
-rwxrwxr-x. 1 jenkins jenkins 169K Apr 28 10:21 TestFit
-rwxrwxr-x. 1 jenkins jenkins  62K Apr 28 10:20 vCurvature
-rwxrwxr-x. 1 jenkins jenkins  36K Apr 28 10:20 vGeom
-rwxrwxr-x. 1 jenkins jenkins  63K Apr 28 10:20 vTess
-rwxrwxr-x. 1 jenkins jenkins  12M Apr 28 10:20 vTesstatic
-rw-rw-r--. 1 jenkins jenkins 195K Apr 28 10:24 wingMultiModel.bdf
-rwxrwxr-x. 1 jenkins jenkins 1.1M Apr 28 10:21 xfoil
[Execution node] check if [reynolds-centOS7] is in [[viggen]]
Run condition [Execution node ] preventing perform for step [Execute shell]
[Execution node] check if [reynolds-centOS7] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[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: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[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: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[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: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_Beta/CASREV=7.8,ESP_ARCH=LINUX64,buildnode=reynolds-centOS7 #711'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS